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41#
发表于 2008-12-25 20:05:33 |只看该作者
ELPRS Enhanced Position Location Reporting System. 1 d+ ~ J; A' W5 ~ELS Earth Limb Sensor. ) d) w. _4 E: lELSEC Electronics Security. 0 o& S( A4 N8 n M# fELSI Enhanced Longwave Spectrometer Imager.9 c8 V) f+ F* ? ELV Expendable Launch Vehicle. / T/ R. [, Y8 ~' c1 |* ]6 [5 MEmanations / {+ [: U8 J5 ^1 ySecurity ' \* }8 X- t8 c; b; J9 J5 z(EMSEC) * {; |" l/ x9 M& x: W) ^( I8 s+ f: ]The protection that results from all measures designed to deny unauthorized9 n- t5 r8 @" w5 t persons information of value that might be derived from intercept and analysis of$ K' o/ J# E7 z: n compromising emanations. ! f# i3 o: P9 XEMC (1) Electromagnetic Compatibility. (2) Early Midcourse.. ^/ C$ O& d3 \3 x EMCON Emission Control/ t# K6 R$ s& C% e. R EMD Engineering and Manufacturing Development (previously referred to as FSD). $ Q6 x' B6 R2 K# k/ b# ^9 mEMDCT Expanded Memory DCT. # Y/ y" T0 u' Y, W9 nEME Electromagnetic Environment.% u9 ~5 J3 v2 E" x4 U( A/ ~, `0 M MDA GLOSSARY, VER. 4.0 E; f' B( r* O, ?. ~ 93 + D9 n F8 d+ z, r& B3 B eEmergency _. w, o0 e8 z* w- `' ^8 m D. g Capability $ A9 g$ L& `2 `3 k(replaces* o* o* p: V [ Contingency9 \4 L( g! h' h9 A$ S4 c8 ?/ _ Capability)& X: c6 A) A4 A) V4 y3 ? BMDS elements or components that are still in development or testing that1 }6 @1 n8 z2 @. @8 C3 m& B6 ~9 l provide limited ballistic missile defense capabilities. MDA, working with the) e3 E( h" C# }% |) A8 e+ V5 n Services, will develop plans, which cover the potential use of prototypes and test$ @8 \) {2 ]& @" y! G. | assets for contingency deployment should the SECDEF determine that an - {: f$ X/ x: s) a3 i7 _2 pemerging BMD threat requires emergency fielding of a BMDS capability.: D6 u" Z4 t0 C) f EMF Electromagnetic Field.# l+ K& E" P/ l9 L0 I. A. L! S% D EMG Electromagnetic Gun. % |2 t' r3 [5 H7 M$ G WEMI Electromagnetic Interference." Q0 [1 W( k& m+ U7 A( a8 w& z, W4 W EMIP See Exoatmospheric Midcourse Interceptor Program.4 f# D9 D; n" p7 e! _8 q2 t Emission Control 7 O. i; ~: j* ](EMCON)( J) p2 ^4 q" {9 J The selective and controlled use of electromagnetic, acoustic, or other emitters5 ^- P5 \' F/ y5 E8 g, \, U to optimize command and control capabilities while minimizing: a) detection by + w% W) p' C. K! Y$ \9 s, W7 Ienemy sensors, and b) mutual interference among friendly systems. EMCON. u/ W* e3 U( x3 t- @ can also be involved in military deception plans. Also called EMCON.3 ]2 w( l5 r# R, X* g2 B EML Electromagnetic Launcher. A device used to launch hypervelocity particles. ' n, b4 `5 e% ~! {, u* ]# l: k9 {EMP Electromagnetic Pulse.2 N2 a$ a5 C1 M3 Y, Y( z EMPSKD Employment Scheduling (USN term). , {* S. v! Z. L; A8 s7 j" R: AEMR Electromagnetic Radiation. 1 Z6 s& z2 M9 N* IEMRLD Excimer Moderate Power Raman-Shifted Laser Device. 4 a9 | E6 X _3 n. }EMSEC Emanations Security./ m" R4 _* v; k( _- p# n p* W+ L EMSP Enhanced Modular Signal Processor. ) w' p3 P/ k) e1 O5 u8 aEMT Engineering Management Team.) V$ v/ m- z. I+ M EMV Electromagnetic Vulnerability.4 W& S1 E0 V5 r0 t# \' ] ENA Engineering: Architecture and Analysis. 0 t3 y$ Z# v; X3 \' M3 C# lENCATT Engineer CATT (US Army term). / B7 l9 ]) k& R P* [Enclave Isolated resource – an SDS asset that has lost connectivity with other SDS 6 [% M, d3 @/ ]) cassets with which it normally has connectivity, but is still capable of coordinating 5 l& Z0 k( P1 B4 M1 ~8 W Twith SDS assets to conduct ballistic missile defense. Various combinations of. K; R6 l( f* ? connectivity losses are possible; for example, (1) an operations center has lost. T! n; H. H, ]6 o% ~4 l connectivity with Higher Authority, yet can still provide sufficient C2 and can still- i( Y; b$ K( j4 x+ } connect with sufficient weapons and sensors to conduct an engagement and (2); _( @6 }$ W+ {5 L5 K an operations center has loss of connectivity with another operations center with 8 H: ~' \$ B2 {/ Y1 \3 k! M3 P: dwhich it normally shares data, but can still conduct an engagement.6 I3 k' o$ l# f2 k7 B4 ^% I# m V Endgame FOV The field of view of the interceptor’s sensor during its final maneuvers after target6 i; I0 G3 j2 `) h% w acquisition to intercept the target. May be less than the acquisition FOV. 6 x: n9 [* @ {8 V1 }End Item The final production product when assembled, or completed, and ready for" Y9 m+ L6 }0 N& Q' l) j; { issue/deployment. 7 [# O$ f: w- v. j/ D1 A1 I O& d( AMDA GLOSSARY, VER. 4.0 E) J2 @% ` b# U r, H6 ` 94' x8 D- i9 S4 X7 C Endoatmospheric Within the earth’s atmosphere; generally considered to be altitudes below 100 % D. M$ }" A3 P2 L8 r8 xkm. An endoatmospheric interceptor reaches its target within the atmosphere. : U7 J/ J+ }+ o2 XEndo- 9 }4 Q% o1 q- }Exoatmospheric8 L6 O/ U3 D6 y9 F: _) D5 T# i Interceptor (E2 I) . K3 n) P3 y" KA ground-based interceptor capable of engaging RVs either endoatmospheric or ' n9 g( H. d0 f! ^5 L* rexoatmospheric. (Successor to High Endoatmospheric Defense Interceptor& |/ `$ ]" Y {0 ?( @ (HEDI).) & Y2 g4 _4 ^$ N6 p# m9 G$ X/ XENDOSIM Endoatmospheric Simulation. / ?) j6 Z: a5 Z/ @% s) I( ^) v8 QEndurance The time an aircraft can continue flying, or a ground vehicle or ship can continue- a n$ o6 f1 t, O9 {) T9 _ P operating, under specified conditions, e.g. without refueling.3 X' j/ \# L* v( {$ ?" }) U& t ENG Engineering.) u6 p% q4 ~0 j& u" V ENGAG’T Engagement.6 B* n! s$ S |0 d9 f. r Engage (1) In air defense, a fire control order used to direct or authorize units and/or 0 F+ w) x% ]7 a- I% pweapon systems to fire on a designated target.) W4 P4 ~5 r' a% Q( b1 p2 R" R) f (2) In air intercept, a code meaning, “Attack designated contact.” * e* ^# a: N. Z4 \- @3 L, B. d! YEngagement (1) A period of hostilities beginning when the first ballistic missile target * x9 j" L$ F7 I' J7 rundergoes fire from the first defensive weapon. ! _: X1 f: u1 P9 t r0 ]3 Z(2) A period beginning whenever any hostile object is identified (designated)+ q" f, z, Z5 F" ]* a as hostile and ending after the last hostile object has been attacked./ ~6 G/ u$ M/ f1 N; ~) b (3) In air defense, an attack with guns or air-to-air missiles by an interceptor % Z, z& T( z1 Q7 e8 g+ ^) Xaircraft, or the launch of an air defense missile by air defense artillery and9 F; y; ^. `: E7 l5 E the missile’s subsequent travel to intercept. 1 A# T5 n4 k$ J) sEngagement $ o( G- M0 o# S* H* D/ y) C, @Authorization ( v8 d+ F% e# H4 j* L3 E0 W6 l8 `" BThe authorization given to USSPACECOM to use weapon and sensor systems 0 @! o( Z5 `/ ?$ n Z8 Ounder previously coordinated and authorized rules, procedures, and conditions. / s, i2 R6 v7 F5 G' jEngagement - f2 j+ x& U1 a! f5 m. C- n0 bControl ) g* s+ A- y7 Z4 @3 \(1) That set of coordination, assessment, decision, and direction functions ( m! A/ t1 R5 gnormally implemented automatically to execute the selected battle plan,8 c- G' F: a1 _6 q military strategy and tactics within partitioned battle spaces (i.e., a1 I4 S$ O T+ [; S5 B, G0 m8 |) | spatial/functional subdivision of battle management). Includes the ! B0 g' B+ l3 D: S3 I, b. ~" Odetermination of: what specific objects to intercept in order to implement + X9 @% R* _% j; e* O, ~the selected military strategy, and which specific interceptors to assign to2 G. C6 X: Q. k6 g7 O5 W each attacker to implement the selected tactics within the rules of 6 J6 J* y' _0 R" Gengagement. a# x. G1 {# v5 R0 {+ X(2) In air defense, that degree of control exercised over the operational5 f* z1 }$ P9 C2 s; |) F9 o3 O functions of an air defense unit that are related to detection, " j/ P/ C V, Q! `identification, engagement, and destruction of hostile targets.

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发表于 2008-12-25 20:05:49 |只看该作者
Engagement7 | f! L. b$ i1 [( N" c Planning8 P! Z4 J6 \+ i' g a' T- _ A set of rules and parameters to be used in developing weapon-target 5 E; g! @: S5 ^: {& Gassignments and for sensor resource management. (USSPACECOM)* ^0 a7 Y+ y9 q: Q- G' ~+ x, H Engagement$ ~1 F K2 o$ C+ s8 S! { Surveillance, P- W! ]8 {% a- Y& Z* ~6 ` The surveillance required to support RV negation in the midcourse tier.( Z/ B1 l7 }, |7 n% P Engagement 3 \" T X: c- I, d9 cTime ! F% y/ C, @( A' ~# CThe time that a weapon takes while engaging a given target. This includes not 4 A+ w- _+ y6 J1 _! e, tonly firing at the target but all other necessary weapon functions involved that 0 r: Z1 b9 }1 B7 e/ e$ Care unique to that particular target. 4 L D) ~: A/ W" G* p! F. uMDA GLOSSARY, VER. 4.0 E6 Y$ y- X0 W( |, m 950 `6 q/ [; u0 P Engineering and3 _/ ]+ G3 [3 V/ ~8 P5 m Y Manufacturing # v& \: ]- k+ W5 @ X4 }- |Development * V* q& w: p9 L0 k. s5 h8 Z0 F(EMD) * C" J+ f2 Q) ~" ]5 p: vThe third phase in the acquisition process, following Milestone II. The system6 [0 {! a) c: a and its supporting items are fully developed, engineered, designed, fabricated,2 r9 E; T, D- J7 v- f3 R' y tested, and evaluated. The intended output is a pre-production system that # Y+ p, I8 v, j3 Q$ [$ Yclosely approximates the final product; the documentation necessary to enter the / p. @/ t# {# z# Rproduction phase, and the test results demonstrating that the production product 2 i: W% D+ A, t+ e+ U3 D, L( j( Uwill meet stated requirements.1 W0 V" _9 o9 n* x8 s. |; v% U. c Engineering " F' J* `; l. H7 m+ fChange Proposal 4 {9 Z8 ^5 D0 _9 y; K(ECP) 0 `( e n3 o/ d C9 k6 _" _2 F/ I6 PA proposal to the responsible authority recommending that a change to an# E8 J9 E9 ? h0 P8 | original item of equipment be considered, and the design or engineering change / c+ R2 j& V4 ]) k) Ebe incorporated into the article to modify, add to, delete, or supersede original 7 O) M( B+ f _; y3 Rparts.$ e2 r6 ?# g8 `) L$ q5 c Engineering/ m7 F) @! f* o9 r Development - r0 h/ v1 u& Y2 B* P1 F; r: d2 I7 XA funding category including those development programs being engineered for/ ]& f( `1 ^! }# m5 ` service use but which have not yet been approved for procurement or operation. 1 _- y# v/ o5 I* C: W/ X/ WMoney under budget activity 6.4. 0 a1 D" o! J: _Engineering " [5 A# L3 t7 \1 [# q* H* `! kDevelopment 7 C* R- V" c' r% OModel & g& i. ?2 L) b9 `) aEnhanced Target X ]" Z: ~+ Z% w2 V Delivery System $ T8 i( f1 q/ m6 r. Y# |' W(ETDS)! q) Q2 ?7 p# g4 Q An advanced prototype used during the Engineering and Manufacturing: F2 G8 ~. S6 x- C9 E Development phase (EMD) to resolve design deficiencies, demonstrate maturing " Y+ h$ L4 s: ^0 E. h" j1 c, Bperformance, and develop proposed production specifications and drawings. 0 _* E1 {7 t% bTarget delivery system being developed for future GMD testing that will ; {$ |9 `7 A& ]" o* q# J Jcomplement existing systems, provide flexible, modular configurations, and will4 g+ L: Y! L) f& x' @$ a! u/ w be launchable from land, air, or sea modes7 Z* M, D% ]1 U. D( {/ G! F: ] ENNK Endoatmospheric Non-Nuclear Kill.5 | K6 p$ w- h& R8 N6 _ ENSCD Enemy Situation and Correlation Division (JFACC term).: B8 K t! d4 ~" I# @3 [$ c Environmental% l3 m( E; O% }% E. L7 I# @ Assessment (EA) 1 b5 r# u5 P( H& LA concise public document whose primary purpose is to provide sufficient + } y0 R- E b: @3 {analysis of environmental effects of an action to determine whether to prepare% | A' ~" c& j3 P6 c. i an environmental impact statement or a finding of no significant impact.) y& d6 e5 \7 B Environmental$ s+ d" K# @9 B$ T Impact Statement 4 @; ~9 W/ E1 T! ?5 I9 N(EIS) - J0 O M1 J% H; HA detailed written statement analyzing the environmental effects of a major ! G. q" b1 z! i# }Federal action. 6 }, H& k; `6 k7 }' ^; H8 E1 ]Environmental * q+ p+ L/ @; |Security - C9 `' v3 [4 {4 P) wA specialized form of physical security that prevents technical penetration, e.g., # I% ]# i3 ?/ k6 a' Cpenetration by waves of electron beams. : Y- i% l: N. @: C9 ^Environments The media, conditions, and/or physical objects in which a BMD asset is immersed u0 I G z1 ]# K T or surrounded. For BMD systems and elements, the comprehensive0 T2 n3 [4 X3 ?. q8 D) i& { environments definition consists of natural, hostile, induced, and storage, ) p+ P" N6 a+ t& [ \5 a' Q4 etransportation and handling categories. ) X* u. w+ L2 WEO (1) Electro-Optical. 1 R6 t4 @1 @" I: d/ Y6 q$ ~/ Y(2) Engagement Operations. 5 ~+ c" E% U4 l+ l0 l(3) End Office.( T6 j5 H: z Y1 ~( V% X4 E (4) Eyes Only.3 [/ ^6 @9 ^' ^0 P, `2 B! i EOA Early Operational Assessment.8 R1 N; D! c$ h/ } [ EOB (1) Enemy Order of Battle. ) R. `4 f* W: B0 B$ V9 i/ a(2) Electronic Order of Battle.1 `8 I9 _* `# q( s; V9 D EOC (1) See Element Operations Center. . W$ R# X _# E$ c* t+ x(2) Emergency Operations Center; C! l. ~& P( J) h) W MDA GLOSSARY, VER. 4.0 E0 t2 \, j4 s3 ^$ i# Q6 q 96 * W; t, v& z- C. E) _1 bEOCM Electro-Optic Countermeasure. 5 f5 e& }" X1 _% |$ FEOCT Element Operations Center Test Bed. * X1 J" p g, t7 @8 _% E% X: TEOD Explosive Ordnance Detail 8 F" y6 A5 q0 M" d! m- D$ Q9 pEO/IR See Electro-Optics Infrared. 0 o; c% b& t. A1 S2 {EOM End of Message.) P) Q2 I# V/ I+ A7 o. j EOP Executive Office of the President v; |; a2 u: F EORSAT ELINT Ocean Reconnaissance Satellite (US). 9 D! \/ e6 h' i5 x. m% S9 ZEOS Earth Orbiting System (NASA term).% Q3 O. q1 g6 p EOSH Environmental Operational Safety and Health.' o- w$ F4 h. F" }" A; [ EP (1) Engagement Planning. (2) Evaluation Plan# }3 ~7 k2 F. `# N EP Cycle Engagement Planner Cycle (NMD BMC2 term).. |* j8 N" ]( e$ F EPA Environmental Protection Agency./ _/ o" \# E _+ a EPD Engineering Product and Development3 K2 B. \5 [4 _6 {5 Q, k Ephemeris/ ) Q# \9 b0 F- h: h) D- ^Ephemerides2 v8 s; n2 W5 w9 n U) q6 U' N (1) A table showing the positions of an object in space at regular intervals of ( m1 K" H$ f6 l/ W. R% ]- V! | Ktime. 1 D, J' @& q+ D(2) A publication giving the computed places of the celestial bodies for each 8 u% T" r' s5 {1 Mday of the year or for other regular intervals. * r. I) e- @, B( @EPITS Essential Program Information Technology and Systems.+ F1 Z& A& D; t! r! _" Q0 R EPL Emitter Parameter Listing (USN term). ) c6 t, ^5 \. b5 NEPLRS Enhanced Position Locator Reporting System.9 V Q& _8 t( U: e0 S EPO (1) OBSOLETE - ERINT Project Office (US Army term). (2) Element Program 7 j; q9 F% \' Y& `. QOffice.3 s6 f& h: d! B V8 [7 M EPP Electric Power Plant (PATRIOT).2 x! w8 Q5 u8 T. q) m1 o' Y EPROM Electrically Programmable Read-Only Memory.9 u4 Y# \& z; Z EQEC EurQuantum Electronics Conference (See CLEO). ) ^6 V5 ?) u8 v6 ~Equipment ) E: S# c5 j, u7 m% m7 t. {% uOperationally 7 }) W/ a0 W8 C2 ]' g* X2 t; BReady 9 F X9 H! e& ~, v$ Y# v# V) zThe status of an item of equipment in the possession of an operating unit that" }$ Z" E' k1 Z* A. P' ]5 [: R indicates it is capable of fulfilling its intended mission and in a system+ n. k: P3 H4 D configuration that offers a high assurance of an effective, reliable, and safe2 L4 q$ u7 q7 X0 [ performance. 8 Z' R$ s6 Q& `5 I, E' w: eER (1) Enhanced Radiation (“neutron bomb”). (2) Extended Range.4 V0 n- r7 ]1 `' d C ERA Explosive Reactive Armor1 m1 j8 q4 _+ ? n9 `8 w ERADCOM OBSOLETE. Army Electronics Research and Development Command. (Now) M2 [& V% j0 r/ x7 t6 l Laboratory Command (LABCOM), Adelphi, MD.)+ N I5 w- a2 X$ w MDA GLOSSARY, VER. 4.0 E0 S+ ?5 q* K* u' d) e 97 + o5 V' S5 R! {+ n, sERCS Emergency Rocket Communications System (US).3 m% e8 Q! t$ d- w4 m+ r# x ERD Element Requirements Document. . c- F, u5 @7 E" aERG Executive Review Group. ( j& s) T F0 n/ u) Q& X/ G$ tERINT OBSOLETE. Extended Range Interceptor. Now referred to as PAC-3.) |% s. G7 P- C5 X( _& w* F ERIS OBSOLETE. Exoatmospheric Reentry Vehicle Interceptor Subsystem. 0 ?; k% @: e+ z Z(Predecessor to Ground-Based Interceptor (GBI).)/ h/ q: z" F9 ~6 ` ERIS(F) OBSOLETE. ERIS Farm./ { p" q! Z1 \9 X- ?# F ERP Emitted Radiative Power.6 A/ |. P" T5 H4 `% D8 O2 H6 z ERR (1) Element Requirements Review. (2) Engineering Release Record. ( d- h3 u0 v: Y& L5 e. gERS (1) Early Release of Submunitions. (2) Emergency Response System./ ?% q" K* _" h; Z, s. ?, j2 w4 z ESA Electronically Scanned Array. 3 C9 V% `( H. B) y1 h8 b2 {( GESAD Electronic Safe and Arm Device. ! m% Q" r4 ^$ s9 r8 C: G% p2 LESAR Extended Subsequent Application Review. * u) \1 W% e0 I7 w3 ?ESC Electronic System Center (AFMC), Hanscom AFB, MA.+ ~& V* K7 J0 |9 L# E; z q% z ESCN Existing Systems and Center Notebook. & \: R3 f5 I: u7 I& e) sESD OBSOLETE. Electronic Systems Division. (Now Electronic Systems Center, & w3 }: L% h7 T; Z |( |" b3 YHanscom AFB, MA.) 5 K1 P ]$ G/ [! GESH Environmental, Safety and Health ) g( t0 d1 _6 O& A# R3 rESI External Systems Integration. 2 w4 f* a2 W; H: e3 r; {ESI ICD External Systems Integration Interface Control Document. 3 S, W4 g: v0 V3 XESM (1) Electronic Warfare Support Measures. (2) Electronic Support Measures. 6 d" l! U- J. E$ KESMC Eastern Space and Missile Center, Patrick AFB, FL. 1 @( N! Y& {3 dESNet Energy Sciences Network.) e9 V- ?" Q X7 w) T& A ESPRIT European Strategic Program of Research in Information Technology. 8 Q) L4 y+ ^4 R" q- {. ]9 I5 UESQD Explosive Safety Quantity Distance. * C: C, k( T6 y7 x" dESSM Evolved (Enhanced) Sea Sparrow Missile.% l( Z1 c1 ^$ A* Y ET&C Extended Tracking and Control. 3 k* M: j. a; z0 D6 CETA Estimated Time of Arrival. + y; }$ ?; n8 W) _( bETC (1) Electro-Thermal Chemical. (2) Estimated Time-to-Completion. V8 P$ r$ v! r2 t# V- }0 B1 v ETD (1) Estimated Time of Departure. (2) Electronic Transfer Device.8 U9 \5 @; c' y( l l/ n9 @6 n MDA GLOSSARY, VER. 4.0 E $ s5 Y) S9 v4 u$ x+ y98! _1 w- m( ~. p W0 ]# e& X* p ETERTS End-to-End Real Time Simulator. 0 ?8 `: Q' e/ x e' rETESD End-to-End Sensor Demonstration.$ v U5 _9 z% B i6 K ETI Estimated Time of Intercept. # }& w1 {: I8 QETIC Estimated Time for Completion.2 Y2 g l& P& ^' w p' I, l ETM Engineering Test Model 2 a! w9 f4 w5 L& f% e% h' mETR (1) Extended Test Range (Pacific Test Bed) (2) See Eastern Test Range. (3) : z& q2 o4 z @; s2 s% z7 S; oEnvironmental Test Round. (4) Estimated Time to Repair. ' F4 C p6 h) ^ETS (1) Experimental Test System. (2) Experimental Test Site.; X+ j9 W; M. E* N# i EU European Union [formerly European Community (ECI)]7 |7 F( R4 ~7 F) ]# t2 G4 h( | r EUCOM European Command. See USEUCOM.0 S' t4 N* i. A! b- W* a. v EURATOM European Atomic Energy Agency. ; O, e; z' q3 Y9 M, h; hEUREKA European Research and Coordinating Agency.5 ~, o' s9 m. q5 \& G0 E7 _ EUT Early User Test. 9 B: X( K8 m2 L. `EV Experimental Version1 t1 s3 V; V% A. n2 N" z7 v EVA Extravehicular Activity. % k8 n; u X* H; p+ u' C, z5 M9 NEvasive MRV A reentry vehicle, which maneuvers for the purpose of evading defensive/ x" n# d; l% |8 ` weapons. & m1 t, t+ K. S! D5 m6 wEvent Based h# [4 ?& A* C/ f1 ]( o6 l7 bContracting4 [7 a5 f, R! y: P0 }0 J Support “event driven acquisition strategy” by linking specific contractual events 8 c* `+ a9 U8 Z- Vto the “exit criteria” for the acquisition phase, or to intermediate development + Y$ F3 `( g5 O Y/ jevents established for the acquisition strategy. # n' E# `+ W# u+ q2 z7 vEvent Driven5 B8 V& |! J/ j* l# @+ e! M Acquisition+ B1 u, K* a" T2 R# Z. F Strategy : ~+ a& R* n* m; [& M3 NAn acquisition strategy that links program decisions to demonstrated5 E# ?- ^/ j' E8 p) y$ s5 Z4 E accomplishments in development, testing, and production.3 Z* v `0 A1 G$ L$ R' h, B Event Validation A sensor element internal process that results in a determination by the operator% A1 X) s8 }1 W0 K0 g5 C that the sensor is healthy and the event reported is real.

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发表于 2008-12-25 20:06:02 |只看该作者
Event1 e. h. Z7 K. A: G. K Verification }3 @* _) l5 P, E6 fThe process by which it is decided, from SDS external data, that the event 4 r1 n3 l7 I7 P! ^( o+ R2 greported is real. - h% r/ \/ ]& EMDA GLOSSARY, VER. 4.0 E/ f! O. h1 B. P7 j0 y1 ]; L8 ~2 J 99 3 p7 t" S- M0 M) p& t3 A9 X' \Evolutionary: ^% u& S/ }4 e Acquisition4 T$ S# v2 @( x/ E (1) An approach in which a core capability is fielded, and the system design has: [* c, V C' r/ h2 E/ u) x$ B a modular structure and provisions for future upgrades and changes as }( f& [8 Q+ t requirements are refined. An evolutionary acquisition strategy is well suited to% n* }5 w9 O4 C) C high technology and software intensive programs where requirements beyond a 1 u0 c0 c3 u$ R5 `5 s! d, v1 F- Jcore capability can be generally, but not specifically, be defined.+ m7 N8 u4 Y* T2 b# b) _ (2) An acquisition strategy that defines, develops, produces or acquires, and $ O" W' J( S% B" {! O. L8 \fields an initial hardware or software increment (or block) of operational capability. 1 W) C$ Q* z% s. VIt is based on technologies demonstrated in relevant environments, time-phased( f0 r/ ~/ ~. W$ I requirements, and demonstrated manufacturing or software deployment" C& `7 b5 x# g$ ~: B) X capabilities. These capabilities can be provided in a shorter period of time, % C6 c! U+ f9 q; j) z! J4 r0 b& b! yfollowed by subsequent increments of capability over time that accommodate 9 \+ A+ M$ @7 L* h) a0 [improved technology and allowing for full and adaptable systems over time. Each3 K: L1 |9 v! a7 X, j increment will meet a militarily useful capability specified by the user (i.e., at least / j6 Q* }% P9 Jthe thresholds set by the user for that increment); however, the first increment, P+ A5 S' C5 X1 V5 z$ m4 ] may represent only 60% to 80% of the desired final capability. (MDA Lexicon) + q) E% E, I6 {9 ~Evolutionary 0 V- S; J) O9 f6 Q+ ^) W- pRequirements / E6 Q8 N# |- z/ t6 z! j- x/ O" ZDefinition % e3 J" J* j1 f/ X& }# HMission needs are first expressed in broad operational capability terms, and then- _6 _6 k; B5 a( ^ a5 a progressively evolved to system specific performance requirements. ' V4 X+ R* R3 _: r+ J. {EVPA Experimental Version Performance Assessment.7 {0 W3 M& H3 t& E: w, t EVPA/TEVS Experimental Version Performance Assessment Test Environment System.6 D3 u9 U! U9 @9 j0 [1 x7 z* b EVS Enhanced Verdin System./ I3 y6 L, Y* V3 P EW (1) Electronic Warfare. (2) Early Warning.- q& t3 c5 `1 e. V EW/AA Early Warning and Attack Assessment.+ {; c- }! S. t6 \/ T2 ` EWCC Expanded Weapons Control Computer (PATRIOT).) x- a: c( N7 O7 | EWDA Energy and Water Development Appropriations (US). ' O- A2 j) r; l$ J* _; iEWG Event Working Group. ; f) Q7 Y8 s5 ^3 n7 s# r. p5 nEWN Early Warning Net." Y* N7 s; N5 V! J8 n% A6 c EWO Electronic Warfare Officer.: n7 t2 E2 r# w& q0 `2 Z EWPE Electronic Warfare Pre-Processing Element. / l- ]7 W, b8 k: A/ K$ D# I/ YEWR Early Warning Radar. ( @4 T. K5 p- i2 i/ F/ \EWS Early Warning System. # S# {6 `! M! }6 b, T3 AEXCEDE Electron Accelerator Experiment.6 |6 }( X0 l6 w Excimer A contraction for “excited dimer”; a type of lasant. A dimer is a molecule& U; f2 G7 ?- ]* r2 i consisting of two atoms. Some dimers (e.g., xenon chloride and krypton fluoride) ]) b7 q5 V, j7 s, eare molecules, which cannot exist under ordinary conditions of approximate + {6 x6 t# m+ J) m0 l5 Dthermal equilibrium but must be created in an “excited” (e.g., energized) condition4 \7 F/ R1 P2 @4 b/ } by special “pumping” processes in a laser. ?7 G0 U* s( vExcimer Laser / }0 a. A% c$ j% @5 m- X' s(EXL) W* B6 D: z6 h0 VA laser in which emission is stimulated when a gas is shocked with electrical 5 l8 X2 ]: Q8 w1 E( p$ lenergy and the excited medium emits light when returning to a ground state.( \' X& ^- q; p/ f* f3 o MDA GLOSSARY, VER. 4.0 E 8 ~3 o. s" B; T3 j100 : _' m5 e, f8 G3 y3 P% s! QEXCOM Executive Committee. X' m# g$ B6 b x2 [! R/ y Executable2 \! y+ r' ?+ g* a Program* B2 e: T3 g s4 Z& o' W/ o R A program is executable if the PM has adequate near-term approved funding.6 I0 u+ u1 w, L- q- [; P/ _; y Executing Agent The individual within the executing element assigned responsibility for managing " A: t$ q) M' s7 c# lMDA funded programs.; J6 G( y/ r4 M0 Q Executing 7 @' C3 L6 K, O. PElements: E) d$ L8 \9 u$ `4 ^: V Agencies or organizations (DoD or non-DoD) that are managing BMD-related ) e5 Q6 N7 Z- h1 [2 e8 vprograms. ) v4 F2 ?7 Y2 Y+ DExecuting % P. R& S0 o& s- T1 |2 tResponsibility# G- f( t9 q# D j Program Manager responsibility. 9 X8 x) s4 J) B* u* `, e% `Exercise A military maneuver or simulated wartime operation involving planning, K& G2 E- J( G1 m" fpreparation, and execution. It is carried out for the purpose of training and " N" L* N% C! r H8 Q0 a/ Pevaluation. It may be a combined, joint, or single-Service exercise, depending" R4 Q/ M. S* j$ I0 R( u* T ?' l2 J& P on participating organizations. See also Command Post Exercise.) A7 L- U9 C" |# b Exit Criteria Program specific accomplishments that must be satisfactorily demonstrated 0 _) }1 b7 c# cbefore an effort or program can progress further in the current acquisition phase 7 k8 {* N1 f( q$ K; Uor transition to the next acquisition phase. Exit criteria may include such factors! q. g$ H! {9 i6 o8 \& {" ` as critical test issues, the attainment of projected growth curves and baseline! L9 y6 r6 B# y& J parameters, and the results of risk reduction efforts deemed critical to the % g/ u/ {4 \1 Y- V# q% z2 T3 Cdecision to proceed further. Exit criteria supplement minimum required+ _$ W* @( q2 I! F$ x accomplishments and are specific to each acquisition phase. : P% y& d! `6 U( O l$ DEXL Excimer Laser. : k: w/ g. H- d( u, m! \/ x& cExoatmospheric Outside the Earth’s atmosphere; generally considered to be altitudes above 100 , T# p5 B$ P+ fkm. 0 x) v0 X- s+ L1 MExoatmospheric % Q+ K- E6 z9 @+ Y9 m8 w! yReentry Vehicle $ D! j+ d" ]: H* ?Interceptor 8 ?3 H8 [6 n2 W7 X7 h! ySubsystem 9 _# W/ e5 {' B# y! l, y! F(ERIS)! q/ Q( X9 u( q6 ? OBSOLETE. Interceptor designed to provide functional test validation of GBI.* t; E2 Q& B# u% z) ^2 N5 N" m" A Exoatmospheric * v! r7 H/ H4 `- uTest Bed (XTB) ; m2 d5 Q. ~. ^$ a( B2 Y; S/ NFlight qualified and range integrated vehicle to support other programs such as & ?- B2 C o8 ^( C: d) E* rGBI-X.( b1 x: A* J" Y/ D1 I! F) W. g5 o Exo Decoy A decoy that matches RV signature exoatmospherically. Exo decoys can use0 D$ z7 \7 c1 ^2 | radar and/or optical means to deceive sensors. - g( V$ ]/ K; P$ BExpert Systems Software programs, which use artificial intelligence techniques to capture and & C1 T/ }6 \' Y5 d, c5 s! Oapply the non-algorithmic knowledge and procedures of human experts.( r4 [9 ^( b& ?! ]9 C Expired 5 _! D/ K3 j# A3 \Appropriation 6 G+ M6 D( f: v, N! ^) {6 v0 ?An appropriation that is no longer available for new obligation but is still available # A+ V; R) G3 s- l8 Tfor disbursement to liquidate existing obligations. Under current legislation no0 m( |8 H( v3 [4 i0 {/ e/ _ disbursement may be recorded or paid after a five-year expiration period. , R! \. S4 j' T6 U- \. G0 _) oMaintains all original accounting identity, e.g. FY, appropriation, PE, etc.! U) ]9 L: q3 h EXPLAN Exercise Plan.7 Y" {3 O! `; W& j8 N Explicit * h# ?4 e1 O, wCoordination) S. @) W- m5 q( y( z# W) }' H A battle management technique which communicates results, decisions or . \' C! ~7 w$ Q4 ~command from one battle manager to another, usually from a higher command 3 D5 j4 H D2 N& y r& ]! Hto a lower command. + ^8 S+ J9 ?7 u( B6 E; Z4 C7 uMDA GLOSSARY, VER. 4.0 E , c8 @- r; y. i6 u101 # z6 z: L4 ^) ~: n) WExtended+ K& \8 o7 u: j* B# K. S* I2 b: h Planning Annex Y& T. @4 y, p4 u A document providing program guidance for an additional 10 years beyond the * M" D+ S% U* ~$ W$ w" K0 `POM.) G' d: E. G/ i3 z+ S MDA GLOSSARY, VER. 4.0 F5 z# v! s" U/ N) h3 C 1039 A4 n. q5 m( a F (1) Fluoride. (2) Fahrenheit. 5 G5 d* D* e: N- y; p1 GF/O (1) Fiber Optic. (2) Follow-On. 2 y- {/ I1 f' U \& m5 \- kFA (1) Field Artillery. (2) Feasibility Assessment. ; o/ E! G2 V: ]4 y4 lFA/RD Functional Analysis/Requirements Definition. 2 _8 v. ?7 o, p* j5 l5 XFAA Federal Aviation Administration. * G, G7 ?: @: D k: b9 D% DFAAD Forward Area Air Defense (US Army)./ L. ?2 W4 N9 @ FAAD C2I Forward Area Air Defense Command, Control and Intelligence. ) `+ ^+ r- S. p5 \. F) z ]FAADS Forward Area Air Defense System (JCS term).- p' q/ ^, S1 Q- n8 u" L8 C! K$ J FAAWC Fleet/Force Anti-Air Warfare Commander.9 D0 T" ]( A/ @# J/ A0 _ FAB Fly Along Probe. , Y6 ^# @ q/ O! C1 iFac Facility (MILCON term). 7 t* _& {- V3 m, Z/ }9 g6 EFACP Forward Area Control Post (JFACC term). C+ G$ V. \- _% \+ U FACSPMF Federal Agency Computer Security Program Manager’s Forum. # y1 C2 p* \1 ~& EFAD (1) Force Activity Designator. (2) Feasible Test Date., q' F! c7 ] A+ K4 z$ _ FADEC Full-Authority Electronic Controls.$ P8 f0 g% B$ @5 p5 Z FAFB Falcon AFB, CO.4 G4 v0 g# \& a2 S/ S+ O FAFBR Falcon AFB Regulation8 h& p8 w( q1 t% ^ Fairing Structure to protect the payload during ascent phase.; h! f7 |$ W* [% @2 r' u. |: e* a FAIT Fabrication Assembly, Inspection/Integration, and Test.0 {1 C' W& K* Z. i, J FALCON Fission-Activated Light Concept. ; u1 `$ R" `* E. F1 C# oFAM Functional Area Management.6 z; j* O* }- ~ FAMIS Financial Accounting Management Information System. * u' p1 r% p5 |' Y! q& Z9 KFAMP Facilities Acquisition Management Plan.* B& O9 C, P& v" L; F FAMSIM Family of Simulations (USA term).* K0 n1 E' E; j FAR See Federal Acquisition Regulation. 2 D: f- t! t1 I0 U0 Q4 G" p3 @Far Field The region far from an antenna compared to the dimensions of the antenna and 7 {4 {) S& J! \( Kthe wavelength of the radiation.; L, r5 _, O4 e3 }- c# h FAS (1) Fly Away Sensor (TCMP). - @0 p7 M7 z8 H2 B3 ^(2) Federation of American Scientists./ g* m, R# G7 }+ W FAST Facility Allocation Study Team./ e5 ` T9 p9 A9 s MDA GLOSSARY, VER. 4.0 F) m i9 \$ X/ M6 w- @2 c+ u f; M1 k G 104 ) _. T. Z. Q* OFast-Burn " C/ B# P5 M7 D3 ~( ^) }Booster (FBB)/ l5 L3 Z/ \0 B3 i) y( b A ballistic missile that burns out much more quickly than current versions, F0 t( d+ H" o/ n S8 ypossibly before exiting the atmosphere entirely. Such rapid burnout complicates 8 h6 C8 F6 A/ k) E$ m2 ta boost-phase defense., e4 ]* _9 \0 ^% D: [ q4 j FAT (1) First Article Testing. (2) Factory Acceptance Test. - Z, M- l0 d+ u2 r8 X* qFault Tolerance The ability of a processor to maintain mission effectiveness after some$ Z3 j6 ]6 D% W* A& W subsystems failed.; |. t. D. z; \: O/ {" \2 e- W) n# W, \ Fax Facsimile. S8 G) A+ \5 V4 A- S# IFBB Fast-Burn Booster.; w4 v0 x6 V. U! w! r' h# q# x FBIS Foreign Broadcast Information Service (US). ; H/ c- _$ B, u: ~FBM Fleet Ballistic Missile. . Z" m; J2 |: c8 P' X3 ], f2 @FBMS Fleet Ballistic Missile System (USN term). , R1 ? a3 V2 z8 A n1 L! sFBP Forward Based Probe.8 @( m1 h! H+ c4 M @* a FBR Forward-Based Radar (US Army term).$ L2 S" M2 x1 T) G FBS Forward-Based System.# z/ F$ j; n/ r6 d9 ? FBXR Forward-Based X-band Radar.; m8 h( v$ x i FC (1) Fire Control [of weapons]. + p! d, A" N; s: V/ w1 z3 w(2) Fund Code.6 I4 b+ Q/ |+ A- b+ D2 K" x. H* k8 `/ W FCA Functional Configuration Audit. 3 [# |$ v* {6 P# h# v; g' GFCC Federal Communications Commission.4 z/ V L6 g- \3 Y; H9 r0 g FCCM Facilities Capital Cost of Money.( }# {, f; L- q6 _5 C FCN Fully Connected Network. ) Y5 {; L/ \* r7 N5 t6 R* ?: ?* V: nFCO Field Change Order. S3 O3 L& K9 A# l W- p1 hFCRC OBSOLETE. Federal Contract Research Center. @5 P7 c$ o) w& L6 }, N! {6 T FCS Fire Control Section.

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FCT Foreign comparative testing.; D8 |9 K1 ~+ u2 y/ s- s; W/ w! N% f- U FD First Deployment.- Y2 A5 G! a, J; m' q FDA Food and Drug Administration. % i/ t6 {0 X& R3 I4 ^8 J, T. _3 h* k" vFDC Fire [of weapons] Direction Center. ( q1 n5 _3 Z" d* f- U( ^9 zFDG Foreign Disclosure Guide.7 k" @4 L& p5 S FDM Function Description Manual. / C$ ~: n# \4 n7 x. yFDO Fee Determining Official. " P* U/ e$ \$ J7 s4 fMDA GLOSSARY, VER. 4.0 F # z1 o4 U. @) x$ H) h4 ]5 k) |105 6 H8 E, N4 [+ E" J# O0 o/ f; fFDP Flight Demonstration Program. 8 P3 O7 P1 ^; V: QFDR Final/Formal Design Review.: q7 c3 ?5 j$ p# d; H# u* r FDRU Final Design Review Update (MDA PAC term).! s" k, `: p! z2 D# g6 X FDS (1) Flight Demonstration System. (2) Fault Detection System. 7 Y. u5 `' E8 N7 nFDSV Flight Demonstration Space Vehicle.# I3 Z' B/ V9 f8 {8 D FDT&E See Force Development Test and Experimentation (US Army).& q$ \1 S- r' w" \5 N FDX Full Duplex (Telecomm/Computer term).: T7 j2 M' {% c% M3 g/ {$ H FEA Functional Economic Analysis. / v( B% E- \# Y% X# O; m0 xFeasibility Study A study of the applicability or desirability of any management or procedural, I3 d7 {/ E( J! g( F5 O- l system from the standpoint of advantages versus disadvantages in any given ' _' H7 R# h- N7 Ccase. # q" G$ i7 P7 E+ ?" j, M" QFEBA Forward Edge of the Battle Area. - j+ b4 O: Q, zFECA Front-End Cost Analysis8 o- r( D2 U7 e1 w1 P' k. h FED Federal.- {/ r E: R4 s1 A1 G FEDAC Federal Computer Acquisition Center. - a9 H: u- a* J' K/ K( XFederal " d8 Y' r# T( pAcquisition2 G" K) n. O4 }$ X" E$ c Regulation, Y( l: s9 u/ m9 [/ p The primary regulation for use by federal executive agencies for acquisition of# g/ i3 X5 Q' Z/ o c! n supplies and services with appropriated funds. It directs the defense program; D) p1 y! Z# _9 T7 r9 m$ l manager in many ways, including contract award procedures, acquisition+ I$ R% s' S9 Q- m7 H, y planning, warranties, and establishing guidelines for competition. The Military % j+ s5 o8 F/ @$ ]5 U8 D) CDepartments and DoD issue supplements to the FAR. The DoD supplement is9 Y! J% C0 ?# l: F ` called DFARS (Defense FAR Supplement).5 }+ |4 y0 _: O1 D) y) o0 g FEDSIM Federal System Integration and Management. 0 @+ I$ K! [9 H1 z: v- }7 w3 EFEL Free Electron Laser.( B3 V |% }; Z' X, i& J. n/ X FEMA Federal Emergency Management Agency. 6 d% D l5 |, a; p, n% R4 bFenced Funding An identified aggregation of resources reviewed, approved, and managed as a 7 m+ q3 j/ R: k4 t2 _1 z8 udistinct entity. The proposed program must be implemented within specified9 c3 l' p$ s' @ resources. Examples of fences areas are: Intelligence and Security, Support to& y# j) R* @# I( {( q3 ~ s Other Nations.$ l/ z, {+ S& _7 d+ w: C( y# w FER Financial Execution Review. ( z* W) q+ Z) n0 M uFES Facility Engineering Surveillance Plan. . ? ~" @8 R" l- |FET Field Effect Transistor. ' y7 t8 F _. d' ]" F5 Q2 l5 DFEU Flight Evaluation Unit.6 D% T) e' R0 p4 ^$ V FEWS Follow-on Early Warning System. & e: l; p3 [( |( M8 j: I0 ?% PFF Fire Finder Radar (US Army.# K) c. D% g0 x! B. N# m MDA GLOSSARY, VER. 4.0 F& y; b( l2 N' m. U: Z1 }6 }$ Q 1060 R! w5 ]& ?. U( @& D0 ~ FFBD Functional Flow Block Diagram. . c* W# w% [+ F6 |2 RFFCD Full, Final and Complete Disclosure (Treaty negotiation term).$ n5 E& O, F3 |. y0 X! m2 ^5 @ FFD Fraction Failure Detected.9 m2 I2 V4 S/ ^) u' Q7 O8 H/ ~ FFH Fast Frequency Hopping. / o" m4 ~2 F r; [FFP Firm Fixed Price.& v6 m( E: o# _. y FFRDC Federally Funded Research and Development Center. " q) f4 N& g1 Q& |4 m9 \9 ]FGC Functional Group Code (Navy ILS term). 4 B& F/ Y# e- w3 e+ R! [FGEP Fixed Ground Entry Point.) E. p K: U2 b% }2 o8 \. P FH Flight Hours.! e, Z4 q: r' K, K" C( M/ c* A FI Fault Isolation.5 d, o- F% y7 n$ y# w FI&A Fault Isolation and Analysis. 8 b1 F3 Q) D2 O5 R/ P, i7 h: a8 aFIDO Fighter Duty Officer (JFACC term). ) U- h3 ^8 U* V( @& \0 ^Field of View* K% t1 B0 t. T }/ @( h (FOV) 7 n$ R+ k, y2 U& N% G& ?' uThe angular measure of the volume of space within which the system can 1 u1 w. D$ G$ E9 drespond to the presence of a target.& R& L" ]+ v% h O2 b Fighting Mirror ! }1 E; {- u5 p/ {& F7 c+ e8 [! i( {(FMIR)/ s" ~7 l- P8 f2 a Part of the GBL System. The low orbit mirror, which receives laser energy and 3 S C% d2 p1 o* u* `reflects it to the target. 1 _, Z& Q' }5 B$ `0 a& W3 AFigure of Merit2 M! B b; G0 b* M! ?( m$ J! Z% M7 C (FOM). J$ l! V( J7 Q1 D5 W/ t The numerical value assigned to a measure of effectiveness, parameters, or; j+ _& d4 p5 N6 h( [+ ^ other figure, as a result of an analysis, synthesis, or estimating technique. : e7 t( T2 g( m1 L+ r. O0 d1 w) Z6 pFIP Federal Information Processing.# {9 q& @# T% o H: Z8 @ FIPS Federal Information Processing Standard. 1 z. ~9 s) _. R, E6 g, PFire Control The control of all operations in connection with the application of fire on a target. 7 d2 i7 J1 e, C& X/ m" L& sFire Control% p- `2 z+ `4 |: y' G/ r* w System / l$ N$ G" @) S" N: V. T! i1 m3 GA group of interrelated fire control equipment and/or instruments designed for8 X) X7 A/ G# \9 y% ^ use with a weapon or group of weapons.+ W8 ]$ W1 k) n' n Fire Support( w; l' I+ `5 C& a- R$ |; |( E Coordinating2 J H* J+ [7 v, u Measure4 ~' o: Y0 ?' ~ A measure employed by land or amphibious commanders to facilitate the rapid+ D6 t! T c& E8 x3 o% |: R4 e engagement of targets and simultaneously safeguard friendly forces.8 k3 Q- @9 J7 y4 Z9 }$ r Fire Support $ e9 q0 T0 s! bCoordinating Line1 {# H4 N# Y" [, F9 ?# i' V (FSCL)7 f7 h1 B V6 |9 b- V/ m, \4 D+ w A line established by the appropriate ground commander to ensure the& ^$ o) s' Z! x/ l% \( T7 V coordination of fire not under the commander’s control but may affect current& v2 |" ~/ x- ^5 Y) l6 U tactical operations. The fire support coordination line is used to coordinate fires * P+ A1 D Q" q+ R# G! fof air, ground, or sea weapons systems using any type of ammunition against6 t$ Y5 }" i M# G" T: E8 C surface targets. The fire support coordination line should follow well-defined% t" ^" }, a& _! |- G terrain features. The establishment of the FSCL must be coordinated with the 8 n; {: v( A7 C1 c5 Xappropriate tactical air commander and other supporting elements of the FSCL( r O2 i T4 K8 P# |, [4 f. m without prior coordination with the ground force commander provided the attack3 ?4 ~! ]1 R f will not product adverse effects on or to the rear of the line. Attacks against; ]% i) h" H! \4 V3 ? surface targets behind this line must be coordinated with the appropriate ground % s1 }8 b! }$ O7 C1 `, kforce commander. ) \" r; d* s5 |# x$ _MDA GLOSSARY, VER. 4.0 F * z0 I1 q& h7 u$ ?107. S$ ^, @3 g" ~. x Firing Doctrine The ratio and manner of assigning numbers of interceptors against given3 C3 O" i& D' @ attackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are U( K" s' Y% Z8 n0 k examples of different firing doctrine. The priority of targets being defended and# W% u7 k. q5 B, {& Y the number of interceptors available relative to the number of attackers drive! z$ O2 j$ r- [3 g0 z/ O% x doctrine. 9 \, e0 d D. X) {9 b) y. U& _Firing Rate The number of missiles fired per site per minute.3 k* Z, `5 F" ?. ^; O; m FIRMR Federal Information Resources Management Regulation. & ~6 q; F- S5 v0 BFIRST Forum of Incident Response and Security Teams. # y( J3 p+ k. ^0 C' \5 Y4 vFirst Article First article includes pre-production models, initial production samples, test $ O; o, ^1 K/ `. ~, W( y! Xsamples, first lots, pilot models, and pilot lots. Approval involves testing and " U, P- @% V' S8 d" e& j. K0 J# f* Oevaluating the first article for conformance with specified contract requirements & @$ C6 ~0 w6 O8 W/ P+ O9 _before or in the initial stage of production under a contract.2 z% z2 a: y* R T/ b8 g First Strike The first offensive action of a war (generally associated with nuclear operations). 6 X5 Y; k# v" s9 B) EFirst Unit' |! Q. J# C0 Z* s* Y3 I1 A" A Equipped Date& o6 W9 |" `9 }! i) \/ f The scheduled date an end item and its support elements are issued to the * c/ l" w4 q, e' Zinitial operational capability unit and training in the new equipment training plan5 B0 c$ l/ C8 h# h has been accomplished.2 m$ G: t7 b P7 r9 c FIS Facility Installation Standard.4 p" `4 k) Y6 i& M/ S Fiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which : w5 P2 R, U7 ]/ n; Z+ hprovides the fiscal constraints that must be observed by the DoD Components in9 M) Q. R1 v7 b9 _ the formulation of force structures and the FYDP, and by the OSD in reviewing) h( e5 J/ q" c; O! M proposed programs. 3 v9 w7 |$ W* GFISSP Federal Information System Support Program. % A5 v+ U, a. D- E/ f% VFIWC Fleet Information Warfare Center (USN term). 0 c$ ]. H# h) {+ \6 j/ d9 oFIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern: a5 c# Q& S, u* M5 Z2 T Extension).& m3 a- l9 b' A3 j( Z4 O Fixed Costs Costs that do not vary with the volume of business, such as property taxes, 1 C- p- D- x* h; Winsurance, depreciation, security, and minimum water and utility fees. & p: r9 `! p6 s' W9 A. E; wFixed Ground! k; `) X6 e# W2 a Entry Point% f5 P& f/ t; k" g( b1 F (FGEP) ( K/ S. |3 ?; l) h, J0 IThe subset of GEPs, which are not transportable. GEPs provide the 7 l2 q0 A: c" t' j% S, T4 i9 S5 Tcommunications interfaces between the SDS space orbital/sub-orbital elements6 z& t& Z; P9 U and the C2E. ; d% Z7 x& ]' y. s, G e! p, fFixed Ground/ [+ Q: v" }6 y Station) d0 K. N" @! A4 p& q( Z7 d8 F All hardware, software, and facilities located at a fixed ground site necessary to2 T; J4 R' q1 ^) L# |, a( m+ L receive, process, support, and analyze mission status and data, and disseminate0 G, ^9 q4 Q+ J7 q operational messages. / z6 |$ d; F, j( X0 h/ }FLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor: R: g) H! q. m$ u9 k4 [! `; h program to Extended Range Interceptor (ERINT).) * _% I) c% C: t9 }FLC Federal Laboratory Consortium. 7 q( K( p) `7 y- I# BMDA GLOSSARY, VER. 4.0 F8 R0 R0 ^% A9 t' q$ L, s 1086 z @ d0 b' a& H& Q: }! ~ Fleet Satellite( D: p! H2 P# I ]( e Communications# F' v$ p. O. V" S System # |: [1 Q: r- q(FLTSATCOM) 3 Y8 P' |& E8 D$ N: }$ HOperating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost # b% e% H7 b; ~; r; Kterminals with simple antennas for use on highly mobile platforms. It has a 5 C, u+ E3 P2 i' Jrelatively small capacity because of its much lower operating frequency. It' d: N9 {7 s7 D. H provides a satellite communication system for high-priority communication * r, Z' F* b, d' p5 o" urequirements for the Navy and Air Force that encompasses almost the entire2 S' G! @9 ~# @5 | z, ^ world. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF- W8 f9 k+ r* p and SHF bands. The Navy has exclusive use of 10 channels for communication / V: q; H) `+ r7 Q$ rwith its land, sea, and air forces. The Air Force uses 12 others as part of its ' H I4 s6 I/ pAFSATCOM system for command and control of nuclear capable forces. The ; V6 g/ U# p: w# k# A# Rsystem has one 500 KHz channel allotted to the national command authorities.. F4 U, D* i) B B# n8 k Flexible% n! E. ?; L/ j* @% N+ W& k Response! l) ~; H1 q: c0 b, I/ ^1 \. q The capability of military forces for effective reaction to any enemy threat or& c6 b; e. p8 y. v! h8 g7 p attack with actions appropriate and adaptable to the circumstances existing., a$ z2 s$ Q! P8 f# K( { @* ?2 } FLHER Funds and Labor Hours Expenditure Report. ! J8 \3 e. H. b5 KFlight4 U8 M9 T' R+ p9 S5 B" f' M Demonstration ! o. V1 O, L. u% ASystem (FDS) & `: E$ x6 P& g5 n- \- t7 sPart of the SBIRS Low Program Definition and Risk Reduction (PDRR) program+ q" Y/ |7 b/ U9 g5 F, J phase. The FDS will consist of two satellites and a ground system being built by' r7 U' S0 l1 s TRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test, W: O3 }1 L* j: T program to demonstrate operations and performance of a SBIRS Low concept, 3 {7 o) D# X/ p# E$ W9 M2 ucollect target and phenomenology data to support the objective system design,# l0 M$ ?* x, L1 j/ ?9 M2 f and validate cost estimating models. # y+ {! e8 o9 QFlight Path The line connecting the successive positions occupied, or to be occupied, by an 6 j. E9 |* Z! |2 |7 h& Gaircraft, missile, or space vehicle as it moves through air or space. (It is more7 I c# J6 G& z3 q& N9 P commonly referred to as trajectory for space vehicles, especially ICBMs.) _) @& O) [& J Flight Readiness, b6 W4 O4 i/ G4 Z# ^4 g Firing8 r7 T/ R' q0 K2 G4 Y! l+ j A missile system test of short duration conducted with the propulsion system6 X Z6 [$ Y ?# _5 f: R) x operating while the missile is secured to the launcher. Such a test is performed7 ~+ @, ~4 g% D. @7 t to determine the readiness of the missile system and launch facilities prior to : |# o/ R- w, w; D) y' F+ G0 Oflight test.4 w7 G. c) f# G7 N) m3 h9 C Flight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching. ' ~- g5 K5 _. mFlight tests are planned to achieve specific test objectives and gain operational . M) } J$ t* P" Z* i3 y0 A3 |information.6 f- i" D; s, C0 j# y Flight Test- }: w7 I0 J# `; |* p6 H3 I Vehicle (FTV)' H9 | v8 g2 U# _$ f! G Prototype of airborne or spaceborne hardware used to validate a technology6 O- t& K+ X* M2 \8 } concept.

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FLIR Forward Looking Infrared Radar. ( C1 K' X9 a. \8 |& v4 i. {- L) yFLOT Forward Line of Own Troops. 2 }8 S P! m' B& _* dFLT Flight.; F3 S7 s) C) T4 [( p FLTSATCOM Fleet Satellite Communications System.( p* K" g. ^% h+ y. c, J; l! x Fluence (or* ?2 f/ p/ G; g* j9 z/ P Integrated Flux), Z2 d$ c5 _+ ^8 [" T' n7 }; t The product (or integral) of particle (neutron or photon) flux and time, expressed & X0 N9 T: n# o* Qin units of particles per square centimeter. The absorbed dose of radiation (in5 Z& {: l/ }! v5 A5 \ rads) is related to the fluence. (It should be specified whether this is incident or 0 x! z- {0 u' mabsorbed fluence).) E x) e$ ?3 y" M6 Q7 @3 Q MDA GLOSSARY, VER. 4.0 F . Y6 h7 U; k# Z' o( K/ H109( w& E( P$ J+ p7 ~9 U Flyaway Cost The total cost related to the production of a usable end item of military hardware. ^2 |# j* c( L# [7 |! G Flyaway cost includes the cost of procuring the basic unit (airframe, hull, chassis,# G `7 n) k3 A% _" L etc.), a percentage of basic unit cost for changes allowance, propulsion # s/ v: H8 B7 h" L# M5 t+ ?6 T) requipment, electronics, armament, and other installed government-furnished- X. v& T) L: J! } equipment, and nonrecurring production costs. Flyaway cost equates to2 ] f- k8 d) A h Rollaway and Sailaway cost.% R/ t7 e; n% s FM (1) Flare Multiunit. + C# d3 @3 d- Y! t) t8 J T(2) Frequency Modulation.# w4 w) i' w9 G+ x5 v (3) Functional Manger. ! @1 H2 l2 M7 F# @(4) Force Module(s). + y$ A% A) p7 ]6 t) a(5) Field Manual.6 `/ t7 `! f( V$ a" k& L! H* T) @ FMA Foreign Military Acquisition. * M2 S6 s* j& A6 z4 ]FMB Financial Management Board." a: W2 U n) S9 o0 x3 P FMC Flexible Manufacturing Cell. : z6 R% ?3 f+ T( _# P9 C3 d. O3 NFMEA Failure Modes Effects Analysis (ILS term).7 }8 e) L" ]8 y, m5 c8 W& m3 M FMECA Failure Modes Effects and Criticality Analysis (ILS term).! ?+ R1 q" a! y) j9 ]( v FMIR Fighting Mirror. 2 R$ N+ O) g% s: ?. X# g* ~FMP Foreign Materiel Program.$ P9 V7 O' v/ U: L9 c2 I FMS (1) Flight Mission Simulator (PATRIOT), Huntsville AL. + F. A; j3 l- ]4 G! @) N, l9 k) c- i(2) Foreign Military Sales. 1 B- L# D7 F; m- CFMTV Family of Medium Tactical Vehicles (USA term). + Q7 |7 w& `! RFNC Federal Network Council ( z9 K3 ~; v( b0 R% _FO Force Operations (PATRIOT). 6 ~) l7 k, q5 ^8 C5 G5 A$ Q: ?9 PFO Link Fiber Optic Link. 9 [- s: q( V$ x2 FFOA Future Offensive Aircraft (UK RAF term). 0 q2 R) D* g: j4 |3 n) h1 w" m. hFOB Forward Operations Base.1 k, G3 v3 h4 ]) c. M FOBS Fractional-Orbital Bombardment System./ {+ _+ F& H( k7 L5 X! a& k* g$ n FOC Full Operational Capability. 6 H' r7 h" m4 OFocal Plane The plane, perpendicular to the optical axis of the lens, in which images of points$ t5 ~. i, F$ D& N in the object field of the lens are focused.* Q4 s' I/ p8 H6 N5 M. d! O Focal Plane % Q0 t% u5 ~) K, ~+ M1 g0 D9 AArray (FPA) , T* Q! t, O$ c. a, p7 x. b3 BAn FPA is a matrix of photon sensitive detectors which, when combined with low * i& l+ g9 E9 F: gnoise preamplifiers, provides image data for the signal frequencies of interest. , i7 ^1 m# N4 r3 y5 y8 V' o) x9 YFOFA Follow-On Force Attack. 4 J: o4 ^; D! l/ u' R( j4 Q5 Z& C3 fFOG Fiber-Optic Gyroscope. L7 j! Z. Y1 j* C& O; e2 i FOIA Freedom of Information Act (US). _" X9 j! D+ ]; b: sMDA GLOSSARY, VER. 4.0 F : ^/ m( K( P$ Q3 h% O110 / ~3 \) Y! q* D+ E9 nFOL Forward Operating Location. % i, N) m% ` |8 Y& O* iFOLAN Fiber Optic Local Area Network. , X& d& z5 A2 pFolded Optics Any optical system containing reflecting components for the purpose of reducing0 m- J( s) c5 V; p1 t the physical length of the system or for the purpose of changing the path of the " p" ]: U) X! o. uoptical axis. * ^9 H, L! Y1 ]/ bFollow-On& D# `) F; p8 t9 a0 c: ` Operational Test : |! _, m9 i# Z/ H9 f7 _and Evaluation # q+ S9 i' `% e' G(FOT&E)& V4 U9 O( J7 w# H" i That test and evaluation that is necessary during and after the production period : W7 I/ j2 ~* f D7 `$ \to refine the estimates made during operational test and evaluation, to evaluate ~6 A4 [3 {! K0 V4 d changes, and to reevaluate the system to ensure that it continues to meet# g4 R: O: c8 M3 W; R" a' O4 M2 i1 m operational needs and retains its effectiveness in a new environment or against7 W( E' K& |* o& l* ` a new threat. 9 ^) G; B, I1 N. fFOM Figure of Merit. ' L0 d/ ^* ~7 mFON Fiber Optic Network. ; b/ b+ s* J, ~7 V6 I0 j z0 \9 KFootprint (1) An estimated area of possible reentry or the solid angle of a detector or6 t6 I$ u, A; _ linear area of a detector at a certain location. ; Z0 @4 B' m$ g; o t: E, p' v(2) Geographic area in which a focused satellite downlink can be received. 3 b% ]0 h% G9 J6 K* ~2 lFOR Field of Regard.6 _2 g* @' o3 i$ X+ L Force Closure The point in time when a supported commander determines that sufficient9 C" ^& b- @2 E0 h' o1 V6 j8 }$ ? personnel and equipment are in the assigned area of operations to carry out 8 B. |, w5 _- Q1 m7 X/ w3 X4 lassigned tasks. * z8 S, k9 m( `Force Development Test and # W1 H ~0 f' q* NExperimentation 3 p+ {( \/ P# G/ wTests employing representative users to examine definition of materiel3 }# y# j+ i& {" s requirements or support/assess development of doctrine, training, organization,$ l+ s8 `, K" x M6 ` and logistics for system acquisition. (U.S. Army). - E4 G. X0 ?4 tForce Direction The operational management of the forces.* k+ I" @( j' d" l1 |) P Force Integration* ?8 {$ h& _& f0 i Staff Officer0 l' p1 Y! ?; T f( p; u Army individual assigned to ODCSOPS to serve as HQDA user representative for / q; Q+ k& ~+ `3 p7 La specific system. Provides continuous coordination necessary for integration of ) L: X/ M+ j3 x" R) M9 Za new system into the Army force structure.$ Z. ]. m- n# U f/ e7 Y1 @/ l Force 0 W% m' r1 f& Z" P" q% c1 K) N4 x0 DManagement 5 a# ^( _/ u; T2 HThe assessment of the effectiveness of the defense forces throughout an * h; w3 n# ^3 l* O: n( ]5 wengagement and adjustment of tactics and the system configuration as ' D/ r) C3 \5 w/ G6 s- Mnecessary to effectively allocate resources to satisfy mission objectives./ P+ G3 i: U0 w6 w6 Q( j Force Reliability The percentage of the missile force that will successfully detonate within 3.5 / g" W9 |5 X0 B9 c4 x* H! VCEPs of the target.* V7 A' [" p/ k& L" y( a1 \3 d FORDTIS Foreign Disclosure Technical Information System.1 f Q; z5 v c Foreign9 j; E6 D$ k! \* _; K Government # n8 M) g7 r% v6 h3 RInformation ! ]: S% X5 ]) [0 DInformation that is (1) provided to the United States by a foreign government or( ^# ?8 S! o. m- z governments, an internal organization of governments, or any element thereof 1 H1 R6 Z! T. P" Swith the expectation, expressed or implied, that the information, the source of $ |' b- S: W: p$ k1 e1 N6 Vthe information, or both, are to be held in confidence; (2) produced by the United 4 J# P! ^1 Q1 [) c9 Y/ s& LStates pursuant to or as a result of a joint arrangement with a foreign/ Z( w. N. B1 K# N government or governments or international organization of governments K2 v1 M; P5 ^3 t2 U8 rrequiring that the information, the arrangement, or both, are to be held in & S' C# Y% o, L, V+ i" _8 X" \$ Y3 {confidence. K8 a) ^0 V" E% X* Y. L- hMDA GLOSSARY, VER. 4.0 F, x: r: f" H/ e) G9 U% \$ @+ P7 A 1115 x0 @; Z" }% Y* T0 L2 A Foreign Military 1 F3 v, r q1 q7 C7 P* T# F' lSales (FMS) % o; G( A* B- \7 T; w' LThat portion of U.S. security assistance authorized by the Foreign Assistance Act0 |% }5 m# }7 V% ^1 w& t of 1961, as amended, and the Arms Export Control Act, as amended. The - S3 h" M0 Q; q( Orecipient provides reimbursement for defense articles and services transferred 3 I3 d* j+ ~ z( x% ^; o! e" e* Ufrom the U.S. Includes case sales from stocks (inventories, services, training) by ! d1 ^4 d8 R6 Q* f/ Othe DoD defense services.4 M. t3 [+ y" \8 i" Z" B Foreign Security+ B' f: W# d! \0 D0 S Policy Model 6 o9 {$ X! `8 c2 D- Q% IA mathematically precise statement of a security policy. To be adequately - d- S6 f: N% [8 yprecise, such a model must represent the initial state of a system, the way in" T+ c1 Y [7 K) T3 }8 ]: N which the system progresses from one state to another, and a definition of a& r' u K7 u. [) J0 U8 P0 A “secure” state of the system. 6 t" A% k; x6 o4 [8 O: CForm, Fit, and& N9 Z2 w- F% [- G Function Data* Z4 x6 |! e+ @ D; {! U1 ^ Technical data pertaining to items, components or processes for the purpose of 1 j, w% [& N- B# Gidentifying source, size, configuration, mating and attachment characteristics,; \2 ? @: C# }$ q8 S7 \( j% u& ]- c functional characteristics and performance requirements. : C3 A* g" V0 O9 a, iFormal* a8 I: o& B/ n2 h8 W Qualification7 x- H& l& d- A) Y% \) B+ B, K Review ! H/ R+ |3 w4 Y+ nA systems level configuration audit conducted after system testing is completed ) }- G8 E0 j/ b2 \6 o* V( l2 J# F* Eto ensure that performance requirements have been met.1 @- M. P+ E5 S' C Formerly 4 \# Q3 `' M/ R; X, iRestricted Data " g# @$ g% P7 m3 g8 DInformation removed from the RESTRICTED DATA category upon joint % g4 ~- ` \6 M. wdetermination by DoE (or antecedent agencies) and DoD that such information # [& Z% N4 O$ ~$ vrelates primarily to the military utilization of atomic weapons and that such8 B6 c1 W) t+ W t: v) R% j+ s information can be adequately safeguarded as classified defense information.6 O) n' ]& G# m9 E( {/ ~. M FORSCOM U.S. Army Forces Command, Ft. McPherson, GA.# s. D, _( F% T/ u6 O FORTRAN Formula Translation Language.

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发表于 2008-12-25 20:06:48 |只看该作者
Forward Edge of9 g" }( L" o1 R% }2 N; T the Battle Area 2 H( p- Y3 }. |3 p# b(FEBA)* _+ T0 v( ?4 q p) X% o The foremost limits of a series of areas in which ground combat units are; t2 L2 E8 O9 A deployed, excluding the areas in which the covering or screening forces are : ^. ]4 y% A9 B2 c' z& `1 x% V) Noperating, designated to coordinate fire support, the positioning of forces, or the ! Q: \$ ^' h, ^! d: a4 Mmaneuver of units. 5 v- G3 r8 ]: z) v2 ]1 W7 g( QForward Funding Carry-over of RDT&E funding into second year of appropriations availability. ! ]. ^0 M+ {! a$ ^4 Q& u; HRequires permission from high authority.- y" l* D! i3 w d$ W* U FOS Family of Systems (TMD).: }! _: i4 r( v# j FOSS Fiber-Optic Sensor System. " v, ^& x+ A4 [7 e3 f1 RFOT Follow-On Technologies. 6 |; T; w* P0 k) i" iFOT&E Follow-On Test & Evaluation.# l: M7 z }% m! {- E& ]* `$ s6 M FOTC Force Over-the-horizon Track Coordinator (USN term). : j% f6 v0 @* S V( K! PFOUO For Official Use Only.; f# J1 L+ f: K9 N Fourth & @2 v( i& w# J) W9 V: ~' |& o8 SGeneration5 p3 _8 F- K2 G% J& y% | _' F Language - ?2 k, N/ v# X/ b( s, WA programming environment that produces both screen and report utilities for . w& A% p" V1 M6 ~$ _4 }use by lower-level programming environments. y' a& y# M5 n$ t$ VFOV Field of View. 4 L N. t" E5 B- Y1 JFOV Radar [Full] Field of View Radar i' S! ?( E+ Q; c3 U# [FP Focal Plane.: o) k6 n2 \7 v" e- Y* g MDA GLOSSARY, VER. 4.0 F. n8 v/ d) V# c1 Z& E7 {* q% \ 112 + H2 ]/ z/ G! o. q1 j' rFPA Focal Plane Array. 2 l& F2 J: z3 {9 n* y, t( cFPC Facilities Protection Committee.+ P7 T# M2 g0 f) w FPI Fixed Price Incentive. 2 e! ?5 e% d& ?) a9 `FPS Fixed Radar.) G3 P/ E& d) }+ ~1 ] FPTOC Force Projection Tactical Operations Center (USA term). * q0 U6 |+ D2 p" a1 D- l# [FQR Formal Qualification Review.: Y5 c7 e) Y/ y FQT Formal Qualification Testing.# `2 o! ^3 E+ ?0 C' Q FR (1) Federal Register. (2) France.! s/ C9 `6 h" g2 v2 M" |# E FRACAS Forward Reaction Altitude Control System. 8 k3 l& D- A4 A( SFRACS Forward Reaction Altitude Control System. ' }8 K- u+ T2 [% C8 E% ]/ wFragmentation/ P1 v+ n E' @1 S Warhead6 r0 ?6 z1 v+ r5 k8 a% t3 ~0 ?! C A warhead, which releases small solid objects to damage or destroy its targets.) W8 ]/ O3 i) M0 ~2 A& [ FRAS Free Rocket Anti-Submarine. ' J" Q0 n- O. \FRC Fire Control Radar ) p$ D& Y& u9 ^* d: DFRD Facilities Requirements Document.$ M1 z, J8 }. @ L7 y; ]9 H Free Electron, r# k; W3 V) O0 T7 @3 G6 {& N& A2 X Laser (FEL)8 d# z0 J" i7 ~/ s V A type of laser, which generates radiation by the interaction of an electron beam ~) H' X4 M- E$ C$ ] with a static magnetic or electric field. Loosely speaking, free-electron laser - q- K% f$ W4 E4 gtechnology resembles and evolved from that used by particle accelerators (“atom / e1 A$ @0 |+ }smashers”). Lasers, which are not free electron lasers, are bound electron 0 R7 O8 a$ z" R; b4 Zlasers. ) O8 _7 z, \' Q' H& {$ BFree Rocket A rocket not subject to guidance or control in flight. - K x8 y; G8 F: o; R8 PFrequency3 ^, j2 A. ]8 Z: Z Management: x* k' r7 v8 {+ T/ m3 |2 c$ F The act of allocating frequencies, or bandwidths to a telecommunications N9 X5 J4 @$ m! S5 o' Z3 x5 [system, necessary to minimize the potential interference between 1 ?; A' o2 D3 T! w" `transmitting/receiving devices. Governing agencies and international agreement ) r$ K- z" W( M8 p1 t6 S# ccontrols authorized use of a particular frequency, frequencies, or bands. . q+ ~5 l5 ]8 N4 F5 f# n5 L6 e+ eFRG Federal Republic of Germany.) v! Y k, R- K" y6 I# c% D FRN Force Requirement Number.4 ^/ L+ }1 t' r4 `/ z* E) \( M1 y FROD Functionally Related Observable Differences.: U; V7 d) s+ {3 @ FROG Free Rocket Over Ground. / b$ t* }- |' QFRN Force Requirement Number.8 t6 N1 Y0 |# C: C9 @, }- a% m FRP Full-Rate Production. / ?5 f# K+ [ b" H3 V9 QFRS Federal Reserve System.8 R D+ ~% A4 L; x, i FS&E Facility Siting and Environment (MILCON term).4 v2 X& E+ t1 |, i/ f9 r MDA GLOSSARY, VER. 4.0 F4 x- @& U; @4 c* Q 113 ' { N+ g! `/ a/ G: AFS3 Future Strategic Strategy Study. 6 F% H) e: r, i( q, W& y6 y& Z1 Y% DFSAF Future Surface-to-Air [Missile] Family.) o* ^& s8 y1 N3 w9 e. P* a FSC (1) Fire Solution Computer. (2) Fire Support Coordination.' I) [9 z& w+ \+ l5 a FSCATT Fire Support CATT [for Weapons] (US Army term).0 w' V: f( Y0 c) K7 W FSCL Fire Support Coordination Line. : P& P& s/ o# N+ a. V) PFSD OBSOLETE. Full Scale Development Phase. See EMD.+ I2 k# _3 x4 C0 x2 d8 { FSE Fire Support Element.+ G9 u. H8 [7 E FSM Firmware Support Manual. $ ~ _- h: g0 o" y4 pFSP Facility Security Plan.: e5 I& b% k: C, U. X* k FSS Fixed Satellite Service. ; y. m6 ^; N, {, k A( F) t! @FSST Forward Space Support in-Theater. & L0 ?' V; t8 |$ X. Z3 ZFST Flight System Testbed. : F9 N7 k3 G" b! I& EFSU Former Soviet Union.( D4 o; T4 u: o$ W+ H7 E+ e FSU Republics Former Soviet Union Republics. d& P% e& V& l- S, eFT Flight Test., T4 o& f( K; l* Q3 |. f Ft Foot. f& A" E2 [ Q% j FTC Federal Trade Commission. ' m6 }4 y/ O6 b# y3 IFTD OBSOLETE. Foreign Technology Division (USAF), Wright-Patterson AFB, OH. 3 j% r# \3 x9 x* Y& \See NAIC. , \% S T: U1 k% U* p2 U/ x) F% UFTI Fixed Target Indicator ; V6 T7 }% e* E& a! \7 q& AFTLS Formal Top-Level Specification. ' a! S' c; o* }FTP File Transfer Protocol (ADP/Internet term). 2 X$ l: ~: n/ [9 mFTR Flight Test Round.; P1 Q6 q+ i _9 Q FTS (1) Flight Test Summary (2) Federal Telephone Service % u( Q$ h4 K2 sFTS 2000 Federal Telecommunications System 2000.& D% A" x2 r ^! a! ~! O( L FTV (1) Functional Technology Validation. (2) Flight Test Vehicle. & Y0 |. k" A) C7 t/ J5 u$ U* _4 kFTX Field Training Exercise. - m' n' G4 }7 ?! DFU Fire Unit (PATRIOT). ' D0 \1 A1 J2 s$ }3 E- s# I$ dFUE First Unit Equipped.% G5 `7 B' B3 }4 A6 o' l- B& Q MDA GLOSSARY, VER. 4.0 F& O" W% o% d" e; r 114 . A8 p+ S8 V% | Q9 p5 @7 m, LFull Mission + f+ @' Z( {/ jCapable' L$ D& d9 R1 q& k- H% h Material condition of an aircraft or training device indicting that it can perform all ; z) ~) L( [2 N% jof its missions. Also called FMC. `0 G$ Z) j1 f3 O. [( y% eFull Operational$ G6 U' L9 N- H/ A) d7 V Capability (FOC) ' M; w0 c* B( b+ u: k9 gThe full attainment of the capability to employ effectively a weapon, item of ) v9 d5 i% C4 I9 H& M" B$ k8 wequipment, or system of approved specific characteristics, which is manned and. Z# r' D3 u! p% x! x+ C" t operated by a trained, equipped, and supported military unit or force. % o4 V& ]/ n3 ~* |Full Rate + b& @+ V$ X. ?1 p, n) H0 qProduction9 M3 i* g/ ]% k0 K7 C# ? Production of economic quantities following stabilization of the system design 7 g& K& a- w3 l) U' o4 sand prove-out of the production process.% n- f+ k! M( x2 |* | Fully Configured% g) O6 T q1 i; n8 r End Item9 R5 i1 o. V7 w. G+ m f3 p The final combination of end products, component parts, and/or materials, which $ e+ J8 a& j$ W. lis fully ready for its intended operational use. Normally all production units are+ m" p5 q, N" y fully configured. Research and development units may be considered fully # }0 M; v3 H( W+ f6 ?" S3 |: ^configured if they are or are planned to become operationally equivalent to the. R3 T( L( M8 B# i! r) B: w) `. m production units.

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发表于 2008-12-25 20:07:01 |只看该作者
Fully Connected / \% I g( T/ c$ s+ O6 E+ RNetwork (FCN) 0 l0 b5 A3 U5 Q0 x( l& Z( E* O7 ~ AA network in which each node is directly connected with every other node.. t9 ^$ p0 y4 a+ E Functional 7 V" _2 [! \( z) y) E* n; `' O( \Analysis ) W+ ?! w9 k2 {, E2 q3 k/ FAn approach to the solution of a problem, in which the problem is broken down! m# ?; g! x+ F2 ^ x into its component function, such as intelligence, firepower, or mobility. Each . E3 L1 R: X, {% H/ T8 j& e# T1 Y+ orelevant function is then further analyzed and broken down into smaller/ s) F5 O, {7 Q: J functional components until a level of molecularity suitable for solution of the$ V: \6 n: X2 {3 J problem is attained.) _% c2 r; l8 I" n Functional5 U+ t2 ^9 v* q: S# e6 x' M Baseline & M9 ]! N9 i& a& s$ u5 q6 v# L5 ~(1) Established after the system requirements analysis/design activity has: {) l: V1 T4 D4 r1 Q completed the definition of the system functions and associated data,! e$ Z' J; `# L" s' D6 Q+ L% b, T: ] interface characteristics, functional characteristics for key configuration; Y0 ]9 @; r: c3 J7 R items, and tests required to demonstrate achievement of each specified 1 C$ Q h6 L: A* m( U+ a) rcharacteristic. This Government normally controls the baseline. # x& D: N$ |& [; `9 i s# q: V; C5 r(2) In configuration management, the initial approved technical 3 ~) i; K2 ^) P8 @documentation for a configuration item." j7 _- N- r* L0 z: E (3) Documentation describing a system’s functional characteristics and the4 i/ X+ [3 G( D, U verification required to demonstrate the achievement of requirements.4 c: i3 v+ U( @* a9 [1 R5 N Functional 8 p8 }& ?/ W3 q/ V, E. o) [1 b( c, _Configuration 3 p2 S1 t8 [4 r. ~! d- AAudit (FCA)2 N$ s6 s" n, ]. l! J& ?( h# m The formal examination of functional characteristics test data for configuration; z3 [) Z% G6 z D' Q: O+ V: f( L item, prior to acceptance, to verify that the item has achieved the performance . F+ e( a& a5 _6 [: x; C) Xspecified in its functional or allocated configuration identification. 4 D5 f" T0 C7 d% SFunctional0 w8 _7 H+ \0 d Economic 7 l+ T1 ]# J; ?" s2 T0 w6 c& |! WAnalysis (FEA): m, R9 B+ l; t" c2 f5 y* | A structured proposal that serves as the principal part of a decision package for& ^+ a& E* x; b0 ]# |2 C/ A enterprise leadership. It includes an analysis of functional process needs or, m' O. G0 g2 I4 j$ ^ problems; proposed solutions, assumptions, and constraints; alternatives; lifecycle costs; benefits and/or cost analysis; and investment risk analysis. It is ( V: ?: E# x/ rconsistent with, and amplifies, existing DoD economic analysis policy in DoD) G2 B$ w* b! K* u8 R Instruction 7041.3. 6 N0 I0 l( a l% vFunctional Kill The destruction of a target by disabling vital components in a way not ; v6 v' x3 |" v/ I# L6 O. S' iimmediately detectable, but which nevertheless prevents the target from ) l3 W4 _1 |3 X5 ofunctioning properly. An example is the destruction of electronics in a guidance. i: q! h" e0 p) A/ W0 I# s system by a neutral particle beam. Also referred to as “soft kill.” 9 e$ q( X6 o9 h: r5 d: q+ C1 l bFunctional- r* ]1 M: I7 `( S: l Support 6 q+ Z: |, d3 v7 sSystematized methodologies and procedures, or a common set of standards,, [6 U! R% q. Y4 q+ } applied to materiel acquisition programs. " }; o+ n* ~$ s! U4 n$ wFunctional( h) E: S; a2 p, B. G1 z8 I. @ Technology $ n) t' I0 d/ X4 h# N; @Validation (FTV)/ n& y1 k1 Z* o Program with the intent of proving or disproving a technology is useful for a given " i1 f! c: H6 L, `application. 0 s) f9 a3 N7 L( x+ W( GMDA GLOSSARY, VER. 4.0 F 4 s: U: y* v+ F! C! r0 w) E1 ~115 + Y k* W% b, \* C" dFunctional 4 M- I, d5 M% X5 f( o" n: N+ cTesting : s" P, p! C: c( w9 L) [The portion of testing in which the advertised features of a system are tested for + \. H% e* s6 F1 s9 f! zcorrect operation. , S, N$ e; i0 _$ Z. q0 o" yFunding Profile Program funding, usually displayed in columnar spreadsheet format by years,2 u& G6 o/ [8 Z! r7 B starting with previous year through current year and out-years. 8 q8 I% V( G5 J, W3 V; MFuture Years& [3 [. ~; {# }+ [8 X Defense Program + G N8 N0 u' A' e [! [) o(FYDP) 6 m3 g4 v% [! O1 O* bThe official DoD document that summarizes forces and resources associated with% C; _) c% t7 d# K8 a, H/ ^ programs approved by the Secretary of Defense. Its three parts are the) X# ^( P8 r+ H, N- @$ b) \ organizations affected, appropriations accounts and the 11 major force programs, Y% m9 J1 T# B" V, p6 U. R7 r (strategic forces, airlift, R&D, etc.). Under the biennial PPBS cycle, the FYDP is 6 ]) `) g0 |3 l @7 uupdated in even years in April (POM); October (budget); and then in January" L! R" q$ ^+ T6 X! Z (President’s budget) of odd years. The primary data element in the FYDP is the; F2 k% f& L: k5 ?4 v0 N- j7 | Program Element (P.E.). Formerly known as the Five Years Defense Program. 8 x* x! ~6 r6 k1 ]& mFWCA Fixed Wing Combat Aircraft. ! K. Z- N! h# F2 s- s6 R2 SFwd Forward.) f9 h1 u2 |: U. n3 w, Y2 p FXBR Forward-based X-Band Radar. : L& D n8 x2 rFY Fiscal Year. 2 V ^9 [ b! R& y# k0 f1 }3 Y6 s% sFYDP Future Years Defense Program. 7 G: d& E, Q, s! r" T% [MDA GLOSSARY, VER. 4.0 G5 l! G" H4 P( U8 f 116 % m% B( c& w4 q# ]" X, [" FG Giga (one thousand million). 4 ^, ^' L9 y. ^ ]# Lg Gram. # u# z( T: ^3 _' n9 ^ OG&A General and Administrative costs.) {* v0 i/ T5 F: q! y, j G&C Guidance and Control." }% X( z$ t* m G&O Goals and Objectives. / r0 I4 M$ c( l' z0 D) s# W& WG/A Ground-to-Air ) d3 R- V% X2 ?8 h! a, q* h: ~G/G Ground-to-Ground.& N# G% B6 F% m6 M# i0 A GaAs Gallium Arsenide. % D( }& W' b1 U) H+ qGalosh The Soviet Anti-Ballistic Missile system built to defend Moscow from missile $ x) W) I. L k! f6 K# pattack." q6 }1 X! n# q Gamma-Ray Electromagnetic radiation resulting from nuclear transitions. Although incorrect,& Q$ U; f4 I# g7 { high-energy radiation, particularly “bremsstrahlung,” is sometimes referred to as9 L& G+ K$ U9 e gamma radiation.- N1 f' t0 {2 C% y; t; o G Gamma-Ray 9 d0 m/ Z }) i ?Laser - B; |$ }2 A' Z# D& CA laser which generates a beam of gamma rays; also called a “graser.” A2 c3 i4 r5 r; k' j2 [5 _) S gamma-ray laser, if developed, would be a type of x-ray laser; although it would/ O* H) ]9 c" C: a employ nuclear reactions, it need not (but might) employ nuclear fission or fusion+ k- ~( q8 N. r c# q; h" A reactions or explosions.- H) ~" @! ?5 l) H& _ GAMS GPS (Global Positioning System)-Aided Munitions. : v" z7 ~2 m3 q4 ^+ e' c0 KGaNMPA Gallium Nitride Microwave Power Amplifiers. (A demonstration program to develop3 K5 v5 x" T) k: O5 b2 l) I GaN based transistors and integrated circuits for power amplifiers in systems \- |# n$ H0 ?4 N+ e such as Ground Based Radar. Goal is to reduce total weight and size by a) F' `: i3 {- c factor of 10).) i K+ J& k6 b& j/ F GAO General Accounting Office., b+ K1 b% _% v( ~. O; y GARDIAN General Area Defense Integrated Anti-missile Laser System. 9 ]8 X0 P4 X1 S1 i! FGAT Government Acceptance Testing. 7 W; S4 S: b* U0 hGAT CALL Guidance, Apportionment, and Targeting Call (JFACC term).5 t" y- a( e* I3 z" d* x0 [2 e3 z. ] GATE Graphic Analysis Tool Environment./ L# w f6 x6 R K) q9 j; ~# v Gateway An element that contained a node on the SDS backbone network as well as on' t6 a6 a- J5 R9 {5 R/ R some other network(s) and would have performed protocol and format 0 w! C$ z$ h& @3 G) _% v+ O/ Zconversions necessary to accept messages from one network and retransmit# F1 t) w3 c( _; q- t* h them on the other.( P: H9 @# e* N2 G' |+ X' y GATS GPS (Global Positioning System)-Aided Targeting System.* W* O& v5 A& V1 O& e, R GB (1) Ground-Based. (2) Gigabyte.# C+ z% |) |5 u1 F& b GBD Global Burst Detector./ v' @; M4 F I: \ GBDL Ground-Based Data Link.( N4 \0 I* u; H0 l' B9 o1 ^ MDA GLOSSARY, VER. 4.0 G 0 {, N; G8 _, U% }& @117 0 s5 `! y. g) x3 E6 G( D3 tGBEV Ground Based Experimental Version. ! H, Y4 d5 P9 h1 T8 }GBFEL Ground-Based Free Electron Laser. " l7 d' x) R/ D. ~* iGBHE Ground-Based Hypervelocity Gun Experiment. 9 N2 r Q- f. E/ @$ b! N9 c, iGBHRG Ground-Based Hypervelocity Rail Gun.8 ^! ?, m* h, Y4 B GBI OBSOLETE. See Ground-Based Interceptor.1 j- ?) I, c, b! l& O9 Q4 A GBI-P Ground-Based Interceptor – Prototype./ Z8 u& L1 H, d8 }3 a& z GBI-X Ground-Based Interceptor Experiment.1 z$ G6 _# q+ g- I: r- q GBKV Ground-Based Kinetic Kill Vehicle.' y/ O3 e: Q* k+ h GBL Ground-Based Laser.+ j, D: C: M" I3 {% S; y# k GBLD Ground-Based Launcher Demonstration.1 F, X- m3 l7 Z! L GBLRS Ground-Based Laser Repeater Station.. @% R) A8 V; O6 d, L+ `4 v GBM Global Battle Managers.! b E8 b7 D- { GBMD Global Ballistic Missile Defense. 9 n; q. J K7 k7 z7 G5 {% QGBMI Ground-Based Midcourse Interceptor. 0 x' H/ f, ~7 a9 y( tGBOS Ground-Based Optical System.# Z1 Z L2 m4 ^& z: r* \ GBPST Ground-Based Passive Signal Tracking. : g! L" V9 ~2 r+ u( E, CGBR See Ground-Based Radar./ E) ?7 e# w: c8 M* t, O0 |# Y$ ? GBR-M Ground-Based Radar-Midcourse. $ X$ z a. p1 `' f2 pGBR-O Ground-Based Radar-Objective. / w7 m5 O* s6 c% x5 k" g% j6 M) \& d0 sGBR-P Ground-Based Radar-Prototype.+ z3 k9 W3 `* D% |0 [7 D- v GBRT Ground-Based Radar Terminal. % {% t% g% n$ q0 u6 n( {1 C- X& \GBR-X The experimental version of the GBR.. V: a5 S4 c( }5 K, } GBRF Ground-Based Radio Frequency.

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发表于 2008-12-25 20:07:14 |只看该作者
GBRI Ground-Based Rocket Interceptor.6 y6 D8 r1 f3 z, ?8 r, C+ H GBRT Ground-Based Radar Terminal.. D$ I3 E% ?* k; C6 ^$ ] GBS Ground-Based Sensor. & S7 |9 I* S& |# E6 f6 M, \GCA (1) Guidance, Control, and Avionics. (2) Guidance, Control, and Airframe./ |, p2 N7 J. c GCC Ground Component Commander (JFACC term). 3 o, M( K% E5 j" d) _5 IGCCS Global Command and Control System. . I2 I" g. P7 p( c+ DMDA GLOSSARY, VER. 4.0 G 4 i! t1 \+ E* l+ }118; O, d$ X4 o: [' Y6 \9 L GCI Ground Control Intercept.2 Z N! g& B8 X1 d& B GCN Ground Communications Network. 8 o% X/ e$ V- @5 yGCS Ground Control Station.1 u) ?5 n' E: x/ G GD General Dynamics. 9 E' }. L3 P; m4 E KGDL Gas Dynamic Laser. % ^$ j+ e' i0 g& pGEDI Ground-Based Electromagnetically-Launched Defensive Impactors. 2 Z1 H; M. g1 kGEM Guidance Enhancement Missile (PATRIOT).8 C7 c2 J+ o) t4 j General Manager1 B2 d7 n6 F" d d$ X6 [2 _ Program % _! I l. o+ R9 Z, Q6 B. {Management * ]. m3 X: d( t \( H8 B! t' F- UDirective (GPMD) : b) ?% {3 b) @1 ^4 U& cOBSOLETE. The primary document used by the GM to direct the Service BMD5 @2 w" y/ g, q Q7 M3 Y' M N PEO on the specific actions necessary to fulfill BMD program requirements. + p& x6 V) t9 Z! Z, Y* I4 jGeneral( J) x6 c+ S4 m1 ~4 q8 [ O Specifications 0 d" P3 U- ^$ I( ~- |, e p6 \5 nA general specification covers requirements common to two or more types,% b" Q% c6 ?! S$ ?' g classes, grades, or styles of products, services or materials; this avoids the ' C0 D- T o" s$ Q1 Z/ Crepetition of common requirements in detail specifications. It also permits+ Z" u0 ~1 M# k4 G$ B) Z+ F- @ changes to common requirements to be readily affected. General specifications " j$ F9 l& m, u$ nmay also be used to cover common requirements for weapons systems and % V% j. w# N$ E3 P, i0 v. ^+ X6 Jsubsystems.+ D+ k1 b, t5 q/ u w% l9 m Generic Rest of2 q% p; w. w7 X4 _ World Target0 H. S+ Z1 k6 v/ N, x (GROW)4 h9 O6 F( g5 t Strategic target being developed for GMD program.& M1 q5 i- a' }) W1 `: l GEO Geo-synchronous Earth Orbit. # c7 G+ T- U# l0 s$ Y2 G' LGEODSS Ground-based Electro-Optical Deep Space Surveillance System.% o: K: ^$ _$ b Geo-stationary" ]* K- @0 c. p0 H8 [7 K# q. ` Orbit (GSO) 3 x7 s7 @/ @8 |+ [8 rAn orbit 35,784 km above the equator. A satellite placed in such an orbit % } \0 H5 B7 ]. q$ Orevolves around the earth once per day, maintaining the same position relative/ F* f! \/ G* o0 B1 J+ ~4 \* L to the surface of the earth. It appears to be stationary, and is useful as a 2 E9 F5 ] R" _# [communications relay or as a surveillance post.1 b, S' _- i3 e9 s5 k/ m GEP OBSOLETE. Ground Entry Point. IFICS.5 }" P, o# x y; `" \# @' A3 |' u GES Ground Engineering System. ! v% V' [! l+ A. eGFE Government Furnished Equipment. See Government Furnished Property. . a1 y: _8 s5 a4 Q; c( PGFI Government Furnished Information." \" G4 |/ Z9 n( s& t. Y GFM Government Furnished Material. 6 z+ S9 O1 e. ]! C9 q% s' v4 E( l4 IGFM/P Government Furnished Material and Property. See Government Furnished $ i: b" ?! h! W7 kProperty. 7 ]* @: k0 j4 M- H+ jGFP Government Furnished Property.& K' V {3 W+ R GFS Government Furnished Software. See Government Furnished Property. ; E& n7 R: I) bMDA GLOSSARY, VER. 4.0 G3 A$ j7 u/ B) h! p) s2 t 119 ) q) g' _' e7 X( s; FGhosting This condition occurs when two or more targets reside close to the same plane1 S* Q+ p: R8 V5 z& b4 F also containing two sensors viewing the targets so they are within experimental: E4 X' L9 v% o3 G9 ?5 n5 A* j determination of having the same hinge angle F. Thus, ghosting depends on + o( ~) G0 [2 k8 C& yLOS error and positions.2 t. |- `) y0 c! R* B! \" p5 E GHz Giga Hertz (1 x 10(9) Hz). + h$ B; a* a8 V, T0 zGIDEP Government/Industry Data Exchange Program. . G' X' i' k! E/ F. k- S% c1 zGIF Generic Interface. 2 Y0 Y: @5 F8 n, g0 g' Y5 pGII Global Information Infrastructure.3 D( F2 @$ Q: D: I+ v GIP Ground Impact Point. 0 R R+ S6 v; r( s; ]GIS Geographic Information System. $ R7 @6 ?7 q7 [3 j, R* a' S* OGITIS Government Integrated Technical Information System.$ @0 y9 G/ t' O6 [; |/ A GLCM Ground-Launched Cruise Missile.2 H" B! A7 I& J+ g* p% I P GLP Ground Launched Probe. See Brilliant Eyes Probe.* x2 X1 M# m4 o: G. `" b: c+ d Global& k4 g" O ^4 V1 _2 X6 w" a Environment 5 z1 Z9 N4 s" t* e* E1 CThe ISTC Global Environment is responsible for the creation, propagation, and & P8 D5 A6 f& d. h- [+ Smaintenance of test scenario common knowledge, how subsets of this ! W9 Q4 C8 u/ A0 G& [information will be determined, and how common knowledge will be disseminated " z8 q1 {4 ]( l8 Hto the various element representations (nodes). The Global Environment; w1 X8 o5 u2 V# |% z3 z performs functions which are common to the scenario such as timing, health, 4 L- p4 ~& M, G$ r1 Dstatus, state vectors of objects, and effects models. 0 p$ A1 p' |( T# SGlobal2 i; \' z- x9 V) b0 E- H Positioning$ `7 ^+ ]3 w8 k System (GPS)& q7 ?8 Q. v6 }- v3 G M The NAVSTAR Global Positioning System is a space-based radio navigation * B) O( @7 C5 y- l; E0 B. \network providing precise positioning and navigation needs of all the military $ A' p9 ~% N( Z# nservices. In the fully operational configuration, there will be 18 satellites in six- i$ a* D: [' B( \1 F orbital planes with an orbit period of 12 hours at 10,900 nautical miles altitude." v4 V8 L3 j; [1 P1 y Each satellite transmits three L-band, pseudo-random noise-coded signals, one * y( ~& o- p" K1 K2 n% u6 G; B" X L2 DS-band, and one ultra high frequency for spacecraft-to-spacecraft data relay. + j6 b! f g# `$ Y1 B7 t/ L! Y, [! J" AGlobal Protection6 O' F6 y t5 \ Against Limited : v' [7 C. S" f3 g. L0 aStrikes (GPALS) # F5 O6 U, R% k7 sOBSOLETE. GPALS was an architecture denoting an anti-missile system8 d; S1 Z' U/ [4 P+ | designed to provide protection against limited ballistic missile strikes, be they$ S+ |) O3 ^: N5 K, M3 H4 v deliberate, accidental or unauthorized—whatever their source. GPALS was 3 ~' m% Q9 C. m; x3 Z+ H/ t& Kcomposed of three interrelated segments: (1) theater ballistic missile defenses, 1 G* Y% P( L9 band associated space-based sensors, to protect U.S. forces deployed abroad,+ R" J: r/ s* [ and our friends and allies; (2) ground-based defenses, with space sensors, to ( y! a& }2 Q' K6 S! X2 M$ z0 N9 x( hprotect the entire United States against long-range ballistic missiles; and (3) , ?9 {3 b) J9 |# {/ einterceptors based in space – Brilliant Pebbles – capable of providing ; F+ h' y) u9 Q. N8 Zcontinuous, global coverage by intercepting enemy ballistic missiles with ranges 4 G3 H; u# n P' T3 pgreater than several hundred miles. * u7 `7 s" s% z$ S4 [& pGlobal Protection0 }, [- p8 b& | Against Limited# V7 a" Q5 i" {5 L' y- z Strikes (GPALS)1 s2 p( O2 m0 q- V* r8 W3 Y Program% M! V! E$ a( X5 ?) a OBSOLETE. The GPALS Program consisted of six Major Defense Acquisition 1 i- G8 @* e( v& ]1 Z0 TPrograms: GPALS System/BMC 3 " C" K4 H* D/ l. [, National Missile Defense (NMD), Global Missile( V# s! I1 k" n1 s* |* Z. d. k ` Defense (GMD), Upper Tier Theater Missile Defense (UTTMD), Corps SAM, and G% I+ n; E/ {: mPATRIOT. Army PEO GPALS was re-designated PEO Missile Defenses in 1992.) n+ m- k* b' A1 E& ~ GLOBIXS Global Information Exchange System. % D: {# W; K _6 z2 H- Y4 ZGLONASS Global Navigational Satellite System. / k( C- V7 ^; N$ s7 d9 FMDA GLOSSARY, VER. 4.0 G & ?/ G# K$ A% u) i, I4 O V) P120' ?% t# `: z* L" M- v GLOW Gross Lift-Off Weight.. K' `4 ~' m7 w( z1 h GLP Ground Launched Probe. See Brilliant Eyes Probe. 9 E w& U8 K: ]! l x" M8 p9 B& LGLS Ground-Launched Sensor. ! C0 j) L- F& Y2 z3 [. d9 xGM (1) Guided missile. (2) General Manager., d! V" X# `; ]) N% b GMACC Ground Mobile Alternate Command Center. T+ G& b* }1 B& `( w) }GMAOC Ground Mobile Alternate Operations Center. 3 W/ f* s* U% Y0 U* s( z4 F4 ZGMCC Ground Mobile Command Center.. R, r; g( O' s- @& t0 _ b GMCP Ground Mobile Command Post.% ~! U; _+ x4 Z& [ GMD (1) Ground-based Midcourse Defense (formally National Missile Defense) (2). U# J2 u( ]$ d) U9 t R/ H Global Missile Defense (OBSOLETE).. D- _, T) R5 y) T3 L9 C GMT Greenwich Mean Time. 8 e4 S r3 d; ZGMTT&C Ground Mobile Tracking, Telemetry, and Control.4 h4 s6 j( p* |& o8 G GN&C Guidance, Navigation, and Control. 9 |* E7 Y' h, o3 i- ]GNC&P Guidance, Navigation, Control and Propulsion.. a, H c7 }6 _% ? GND Ground. 1 Y) f3 O0 Q1 M; e% [GOCO Government Owned, Contractor Operated." ?, V% G" j8 x" o6 ?$ a GOES Geo-stationary Operational Environmental Satellite.4 e# f+ s% Z8 y6 k* k+ x' I7 z GOI Government of Israel. ; x5 I8 h1 R! O" oGOJ Government of Japan.

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GOSG General Officer Steering Group. 0 F3 s3 [" @) ~; u. K( u8 jGOSIP Government Open Systems Interconnect Profile (CALS term). ' W' k6 C# n& ?* dGOSP Government Open System Protocol (CALS term).5 P' h" n# q1 {+ }) Y2 Q8 `: ]: l GOTS Government Off-the-Shelf.7 w, @9 U1 `, c9 p# Z( N. a Gov’t Government. + R @: {, v* l! \/ B+ A) dGovernment' l0 u: T7 f& j5 x Furnished, ^& z6 e& V1 i: k6 g8 Y Property 8 u3 ?# ?5 M; r: I% j5 j9 PProperty in the possession of, or directly acquired by, the Government and # D& I0 |- ^. g6 p2 B0 Z- q2 usubsequently made available to the contractor. (See FAR 45.101.) + p0 H8 G" O# ?. Y, `Government : M) P' Z; _& |+ |5 F( h+ ^Verification2 h1 g: W4 |7 f& r1 P7 Y Management 9 Q: H/ e! q4 ~- r* Q* G6 Y5 wPlan (GVMP) 5 }/ b0 x& V# j& oA management document that provides the overall framework for BMDS% H& W6 W8 \! T0 r verification. It includes processes for implementation, organizational6 a9 v3 U# _& a relationships, and stakeholder responsibilities. It covers the full scope of BMDS 2 I7 G2 ^1 t- D9 B3 vverification and identifies how all BMDS verification activities will come together to# q) e2 X: [4 i- B% N confirm BMDS capability. 0 Z. q7 U, R" r$ [$ X0 D' j2 k+ nMDA GLOSSARY, VER. 4.0 G4 {" B! U: Z" O+ y 121" F) q: {7 v, e" q7 _( h GP Group.& n! n* U& i* t7 O; I" T2 l+ p GPALS Global Protection Against Limited Strikes. . l7 ^$ C; m% t; rGPC Global Protection Center. 8 J) Q3 T+ G/ D- L; QGPMD General Manager Program Management Directive. ; d0 S2 h4 k3 L! l; \+ Q: X, \GPO Government Printing Office (US).$ l4 u2 h7 C+ M8 r( u# q" c GPP General Purpose Processor. l+ E9 T; t# }. i% g6 A GPS (1) Global Positioning System. (2), Global Protection System.$ Y+ b2 R. f( o GPSIU GPS Interface Unit. 0 Z0 @. x5 H' j, gGPU Guidance Processor Unit (US Army term).5 \! l+ n* A4 i1 s5 c Graceful ! ~4 K1 \0 h eDegradation; o6 L+ i! d0 a: x8 O: m) V A condition in which a system continues to operate, providing service in a1 R8 T$ O0 _: H1 a# E. D degraded mode rather than failing completely or catastrophically.4 v" C" B0 D9 n: U7 C: y GRASER Gamma-Ray Amplification by Stimulated Emission of Radiation. (See Gamma- T2 X0 b- P. b! T Ray Laser.)$ K* u! ^. [7 e GRC General Research Corporation. . c: u2 { r2 Q& L& K! k- `Green Code Interface Software.& ^3 R5 D6 ?* P6 |7 K Ground-Based 6 |2 i% b' f; I2 B tDefense, D H& ?+ ]% }( e# { The ground-based sensor and weapon systems of BMD.* v3 W1 R5 _9 D Ground-Based 3 f3 a. n, r3 j% b) mInterceptor (GBI) # ]4 x2 y6 g7 @7 m W% S* B X+ L8 MA kinetic energy exoatmospheric interceptor with long flyout range to provide,; j$ j) m4 x* \. P6 ^8 n, q where possible, a multiple engagement capability for defense of the U.S. with a : l( B" k$ l% S& V V) w5 Frelatively small number of missile launch locations. It is designed to engage 2 L- m" }$ z: upost-boost vehicles and/or RVs in the midcourse phase of flight. 7 g9 E2 f. ~1 N/ r9 Q: B! d(USSPACECOM) (Successor to Exoatmospheric Reentry Vehicle Interceptor / b9 P) {$ `, N: [% P- @Subsystem (ERIS).) See EKV.* q* W; M" l/ H- h9 }6 x: s1 M Ground-Based 5 k" T2 k6 Z6 q" n) B0 EInterceptor) o% y+ V9 P/ K% x, G( n0 A1 { Experiment6 E( F$ y/ Z; P* W Y0 D- n (GBI-X) ! n6 m3 a5 Z) W9 @Designed to infuse advanced technology and promote competitive environment6 b# R" W5 i( c" O( _% @; [. y for GBI. % t( X1 V Q" P( x2 ~2 }: AGround-Based # k9 v9 l' f, I. h% a: n. G7 X, O. V( @Radar (GBR) % A' s! }9 h% O% F# [. v/ \! H: rA task-able, modular, multi-function, phased-array radar that provides4 G; P0 v: X! [' h! T$ d surveillance, tracking and engagement planning data in post-boost, midcourse, " ?2 [, n' P: @8 E; uand terminal flight phases within its capabilities. It also provides target 2 c u3 h9 N; b0 W: {discrimination, in-flight target updates (IFTUs), and target object maps (TOMs) to % x9 {5 ]; S" B$ M; J! k! J( }3 H, q/ Minterceptor vehicles. See THAAD. (USSPACECOM) 5 M( l1 M$ L* O' Q! a% j. FGround-Based/ Z' d9 m* j, v2 z Radar Terminal+ C6 S* n" h j* ?) c4 V& z (GBRT)1 F. {' D( g2 F/ @* Q: e The sensor for the NMD system. An X-band, ground-based, phased array radar 6 K% o- o( U; L! l5 Ccapable of detecting, tracking, and providing discrimination information to a 0 M+ f9 O. i7 p k8 o3 Qground-based interceptor. \3 J) G/ g) a n2 M' ?" w6 KGround-based F2 q2 _% _- w, ] [Surveillance and 0 G; R& y1 [: ]Tracking System" l8 I* r2 u1 S6 K5 r (GSTS)9 r( x* y% H" _/ B* d; C A fast-response rocket-launched sensor, which can support the SDS midcourse 8 [# `0 ^6 ~) z8 z9 z; t k9 Ksensor suite by employing multiple Long Wavelength Infrared (LWIR) wavebands: X1 h; o7 [: B/ o: g. [4 l and a visible waveband sensor to provide tracking and discrimination of , E0 o ~" X5 @/ I W6 g7 ppotentially lethal targets.2 c/ C* z) ^: W3 M( d0 f9 W& { MDA GLOSSARY, VER. 4.0 G $ L% B# v; b. t122' l/ { F8 K; I7 w Ground Entry4 P+ B( J7 @2 d+ D) `9 `! a3 _ Point (GEP) - A" B" x) \# d |/ _OBSOLETE. GEPs provide the communications interfaces between the SDS $ o& Z& C5 \4 A* t& k" }space orbital/sub-orbital elements and the C2 E. See IFICS. " v( f0 w5 g& o* G; [8 D7 b& ^Ground Mobile; V) U8 x) p- k L Regional' _5 C/ n. l0 n* c5 q5 o Operations ! g4 _) m6 c ~% r' v4 J; UCenter ) M4 Y5 @8 o, k% F5 {) D0 H(GMROC)6 e3 o9 R8 b( q$ H+ n* { Transportable ground segment of the Regional Operations Center. % b! Y, l. }' S1 Y5 n8 V' H8 bGround Zero The point on the surface of the earth at, or vertically below or above, the center3 S: `' ^# k) [) y Y of a planned or actual nuclear detonation. 6 w9 ^6 w6 }, K$ W% q% Q2 |GS Garrison Support (US Army term). G) Z R3 c) j/ b$ P, dGSA General Services Administration (US). H4 O. i6 Y! {) V$ z' v1 ^GSDC Ground Station Demonstration Lab. ; c5 }! [ Y& S& L/ V: iGSE (1) Ground Support Equipment. (2) Government Support Equipment. 1 ^6 b6 |- k& O1 @7 ^; IGSFC Goddard Space Flight Center, Greenbelt, MD.* ~) k5 F8 A6 g, ]" Q1 U GSII Government Services Information Infrastructure." n+ x( d% b, Y GSM Ground Station Module. 9 X. s) n6 T- P; p% ]GSO Geo-stationary Orbit. 5 Y! |3 @) ?5 I. J3 zGSR Ground Station Radar.& K5 U& J: S4 e" `# s* i GSTS OBSOLETE. A fast-response, rocket-launched, Long Wavelength Infrared 5 @9 a6 v$ `: `9 H3 I4 C(LWIR) and visible waveband sensor, which would have enhanced the : Y2 d: }5 m2 I: Jinformation available from the SDS’ midcourse sensor suite by providing tracking ' {. V8 k6 D- ~+ |and discrimination data on potentially lethal targets. + H7 a) O! [" N$ A ZGSTS (F) GSTS Farm. 5 b' r; H# z' v ~% W# U' {$ vGTA Ground Test Accelerator.) S5 T/ ^ T4 u* w5 \ GTACS Ground Theater Air Control System. 1 v, x4 E5 y) z3 ?GTE GTE Corporation. 4 T& ?5 z' K1 N* [4 AGTF Guided Test Flights. 6 ?8 n5 t3 ?# Y8 y: l* r1 N$ RGTM Global Track Manager. 2 G8 S3 }' R5 r7 gGTN General Technical Note. ! P0 V4 E0 Q) jGTR Gulf Test Range, Eglin AFB, FL. % i) X+ x X' C: iGTSF Guidance Test and Simulation Facility (PATRIOT), Huntsville, AL. 7 M& a" r6 K5 u: u+ {* eGTV Guided Test Vehicle.4 X( D/ L1 J) @( S1 G GUI Graphic User Interface. # K5 L) \1 V: V# C6 w& bMDA GLOSSARY, VER. 4.0 G + S0 p* [$ h- o) u6 S123' Y) f7 D4 _6 u' Z& _9 b; T4 P Guidance (1) Direction, altitude control, and navigation (where appropriate) of sensors ( d+ a4 R# C" ?+ k( Vor interceptor vehicles. 1 p* f8 V( F/ `. c) P( N(2) The entire process by which target intelligence information received by a * R+ X/ l. @+ pguided missile is used to effect proper flight control to cause timely " B, K9 d i9 b8 adirection changes for effective target interception. " I) C2 }9 Z) p$ x" |9 R4 Y; Y. d: I# vGuidance $ H6 ?7 G, T1 hEnhanced+ K% L# |3 u8 u5 t Missile (GEM) , u. ]% E# q" u" c5 S1 [A companion program to PATRIOT PAC-2, which includes enhancements to the) w1 n# K' H F% x radar to increase intercept range and performance.) @1 C! f4 K* j ? Guidance * l1 i8 e t xSystem (Missile)8 A- j, d! i) [4 i5 ?. N' ^3 Y; t A system, which evaluates flight information, correlates it with target data, , r5 t; A5 J# Zdetermines the desired flight path of the missile, and communicates the" x2 U! e% U; a/ ]! g8 B) G necessary commands to the missile flight control system. n: G8 O {; J8 d: A0 rGuided Missile An unmanned vehicle moving above the surface of the earth, whose trajectory or 4 }1 ?4 m: Q, _' }& k; gflight path is capable of being altered by an external or internal mechanism. 2 h3 V4 i8 r! O, N# EGVSC Generic VHSIC (Very High Speed Integrated Circuit) Spaceborne Computer.7 J/ Q+ ]( J# K/ Z4 \ GWAPS Gulf War Air Power Survey, 1994 [a DoD-sponsored survey]. A+ N& ]* l1 W3 V0 U _Gwd Giga watt-days." S; Z# X! Q8 `( ? GWEN Ground Wave Emergency Network. 6 l& B" a; R- L e# x$ a. UGZ Ground Zero. % E/ m& U8 ~: O% k' M' cMDA GLOSSARY, VER. 4.0 H% i) ?4 d/ V W2 {; [; q 1240 J; k7 i6 @' _. V% I H Hour. " Y7 _7 n4 r# g, }3 [5 c0 vH&S Health and Status. 6 O2 _( J+ R4 f. _H/W Hardware. c- ^9 F5 o0 m2 \3 y& GHA Higher Authority.* }5 ?) U& h4 @& u3 g$ J HABE High Altitude Balloon Experiment. ) x8 L6 c% {+ _" H3 X1 \3 J& cHAC House Appropriations Committee (US).: b1 p6 H4 {& w, r' W! G HADS High Altitude Defense System.3 {( Z" \6 T% W, D9 Z3 J+ t HALE High Altitude Long-Endurance.. b$ }6 P' q/ s! \ HALE UAV High Altitude Long Endurance Unmanned Aerial Vehicle.8 K6 Q$ G* a6 f/ K Half-Value " s) D9 F5 L A# ^! O& N- e- YThickness (HVT)2 [' J9 f( ~" M2 b+ p0 ^ The thickness of a given material, which will absorb half the gamma radiation+ M4 }; V/ r( x5 W incident upon it. This thickness is inversely proportional to its density and also : I* ~7 D5 o f8 Odepends on the energy of the gamma rays. ) f4 C, O+ R7 a. q8 @HALO II High Altitude Observatory II6 C4 l- c" t9 u: g1 I HAMS Hardness Assurance, Maintenance and Surveillance. a5 W/ g/ a6 R- k6 D, g- C* wHandoff This occurs when information on positions, velocities and tracks are given by one/ J( ]1 d5 }# K) k0 } sensor or system to another and the first sensor or system continues to track the e9 D e7 E4 @' h) t8 F) G objects. 3 C5 F% r+ F/ ^/ s* `Handover This occurs when information is passed on to another sensor or system in which$ ]* \- \+ ]% W. ] the first does not continue to track.* J+ F" g- {) `/ N `1 U HAOI High Altitude Optical Imaging.

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HAOIS High Altitude Optical Imaging System. % m1 d1 }+ G0 m7 }2 x- Q" @HAP High Altitude Probe.* I4 d. v4 t5 y6 t. L, P Hard Kill (HK) Destruction of a target in such a way as to produce unambiguous visible 9 M8 |: i- u; Y4 {* Kevidence of its neutralization. . h- O' I p+ `7 {8 {4 g, vHardening Design and manufacturing process and other measures, which may be employed / p, Y, l: y, U; J3 {to render military assets less vulnerable.. ]8 i8 N% m! n+ r! Q HARDMAN Hardware/Military Manpower Integration (Navy ILS term). 9 p, H& V% T* W& n- d7 G8 _( i SHardness A property of a target; measured by the power needed per unit area to destroy j; l0 D( o0 f the target. A hard target is more difficult to kill than a soft target.( A+ P7 T* J' R! K# l2 A& P: Y Hardware-in-the- % o6 h2 `9 @% s4 c7 GLoop (HWIL) - z: [. c/ w& p* oTests in which BM/C3 computer and communication test systems will be in0 R7 ?; |; T/ E. v- E communication with some of the hardware test facilities developed for other BMD0 ]% [; X& X! Q- A5 s technology programs. 5 c% S1 _5 }6 A) O5 yHardware" x6 s) y* V: s4 B1 _! c Security% u- C9 G& T+ R3 t S1 ~ Computer equipment features or devices used in an ADP system to preclude ! W% z# v4 H3 m2 {unauthorized access to data or system resources." J( ?% {1 f& m! H. r HARM High Speed Anti-Radiation Missile.& f5 j4 C7 p/ E- ~1 a MDA GLOSSARY, VER. 4.0 H3 g7 m- e: c6 i9 W1 i1 |5 u: w6 c 125 % ]( t& r' O4 u1 nHASC House Armed Services Committee (US). ! K% H2 e Z+ s9 g, @8 h8 f, D/ RHASP Hardened Ada Signal Processor. : s3 s0 ^' j; y1 u# dHATELM High-speed Anti-TEL Missile. : x# S6 O9 e/ ?3 u: AHATMD High-Altitude Theater Missile Defense. (U.S. Army)8 ^2 r) D" f& E7 i. Z3 c* u4 e HAVE STARE Name assigned a proven sensor capability.: _0 ]2 A+ o! K- n+ f HAWK Homing All-the-Way Killer.4 o0 d1 A. n+ ^. @ HBCU/MI Historically Black Colleges and Universities/Minority Institutions. ( U$ g1 m+ H! ]HBHO Hard-body Hand-over [algorithms]. ( J3 f- L- ] b6 oHCO High Consequence Option (Safety Engineering term). ( L: D. ^" b( q- T% zHCT Mercury Cadmium Telluride. - x, R y6 P+ E/ v5 k$ u4 XHDA Hybrid Detector Assembly.- j$ f9 {* @" K5 Z( { n9 e# ` HDBK Handbook. 6 j$ E3 M/ E: P6 a3 QHDR High Data Rate. * H; I. }! i/ n! H3 D0 UHDX Half Duplex (TelComm/Computer term).3 k p6 i2 h, r: A3 d6 _7 Q3 Q4 F8 @ HE (1) High Explosive. (2) High Energy. ; r0 s6 R i, j$ w2 QHealth and Status* G7 D" {$ B1 w- ^" G4 d (H&S) 9 x, V6 r5 b$ [% q$ QHealth and Status pertains to a unit’s ability to assess the conditions of its6 A* {3 E" g3 h1 D. A" s subsystem functions. The term H&S is used for units in remote locations, such( k4 @# s: Q6 R. E0 o as satellites, where ground controls must interface with BITE to determine8 g& O u# w4 H7 M, X& n operational status of the satellite and its equipment. . q$ R+ Q! L6 j y) ^Heavy Replicas1 K% q2 t! B1 V" ^* w (HREPS)% h0 S- f6 Q$ ~1 J; B, { Decoys, which by virtue of shape, size, and mass, closely approximate an RV’s - H& T5 a* R: F& ksignature. HREPS have significant off- load penalty. 5 s' m6 X! x- oHEDI OBSOLETE. See High Endoatmospheric Defense Interceptor. ) C, K4 V9 S, R* _+ ~4 R: Q& ]HEDR High Endoatmospheric Defense Radar.. ]/ ]! w* T) k( g; s HEDS High Endoatmospheric Defense System. $ Y6 C# K4 e: X/ y2 ^: |! ZHEI High Endoatmospheric Interceptor. , V5 R; t/ b O# f4 `5 nHEL High Energy Laser./ L: Z9 Z' V' b1 f( _+ K HELKS High Energy Laser Kill System.& _$ Q0 B' q9 o* W/ X: A. p HELLO High Energy Laser Light Opportunity. 7 _7 a/ q1 H, e" F/ LHELSTF High Energy Laser Systems Test Facility. , ^' d3 ^3 k! ZHELWS High Energy Laser Weapon System. 6 O5 C0 f- i" ?' m& ?4 R/ T- ]HEMP High Altitude Electromagnetic Pulse.7 w" u$ W# q* P# K. S; G MDA GLOSSARY, VER. 4.0 H 9 X1 l) w9 q2 o+ D h9 E126 ' I- S" D9 P( aHEMTT Heavy Expanded Mobility Tactical Truck (US Army prime mover).% ^6 G$ ]! p0 \( |* z8 Z; d! j Hen House Soviet area defense radar used as a component of the Moscow ABM system$ N- K/ V, w) A/ \9 o/ k2 E5 Y3 }& Z that provides VHF coverage of space to monitor orbiting satellites and early # u* l9 y' K7 j' Kwarning of ICBMs launched from the U.S.# q! Q% r- Y3 k( t HEO See High Earth Orbit. - X- Z5 h# v9 l0 u6 ^HERA (1) An improved surrogate TBM test target. ' O3 U/ W5 x, x1 L5 w: |* c(2) Two-stage, ground launched solid propellant theater target vehicle. (MDA H- f& Y* x: S7 CLexicon) 5 ?! Q5 Y- l* U; h* [, B LHERO Hazards of Electromagnetic Radiation to Ordnance (SM-2 Bk IVA).$ j: V; a0 ~: h HESP High Efficiency Solar Panel. e, d. p; c2 }# z0 M# r5 m5 `8 j HEU Highly Enriched Uranium. $ W% o& {% [( |1 |; YHF (1) High Frequency. (2) Hydrogen fluoride.. `8 H _. B2 Z# p8 d8 ^6 v2 x7 \ HF/DF (1) High Frequency/Direction Finding.1 M5 @+ f, } }3 R m9 M& ~ (2) Hydrogen Fluoride/Deuterium Fluoride. (Chemicals used in IR chemical i" W$ {" j: F( u% m* P, Flasers). * B9 s5 ~/ d1 y) YHFCNR High Frequency Combat Net Radio. + |& `/ K0 B8 Q7 A WHFE Human Factors Engineering. 6 B# t1 Q+ ]4 JHgCdTe Mercury Cadmium Telluride.4 j( ^1 ?1 `3 s HHB Headquarters and Headquarters Battery. 8 K P1 T5 J7 V5 aHIBEX High-Acceleration Boost Experiment. ! l: m3 n4 p! m$ M4 P# bHIBREL High Brightness Relay.* d' Z% ~/ }5 S5 {" t HIC Human-in-Control.$ \: W7 e3 }/ R5 C6 R# x HICOM High Command (Navy term). / J" y: G9 j2 GHICTB Human-in-Control Test Bed. 2 o6 \% t3 E2 S1 ~8 i) v5 eHIDACZ High Density Aerospace Control Zone.0 L3 a8 X8 F( m/ ^" N# s HIDAR High Data Rate. ) _# m8 w6 z. H+ s( t! V: oHigh Earth Orbit / u* @% T9 l+ m# d(HEO)8 N! i3 k; L& H6 Q: _ An orbit about the earth at an altitude greater than 3,000 nautical miles (about 5 U2 I# R0 [4 _5 s" V5,600 kilometers). + F& Y+ B: l/ ~4 h- `& rHigh ( x3 G; b3 V8 b8 mEndoatmosphere / @% Y5 t" ?9 K2 f% dThat portion of the earth’s atmosphere, generally above 40 km altitude.7 ]6 y. m- h( j- b& Y; k/ ?# W High 5 j# a0 o3 X- EEndoatmospheric2 W$ V0 L- A; ?7 Y5 V- z# l Defense 8 g0 P+ C0 @; Z. j0 s/ j8 n; MInterceptor (HEDI) ' ~( T5 D8 e& c0 ^3 V pOBSOLETE. Interceptor concept designed to engage RVs within the (upper or7 ], C6 T+ Q" W: R2 t3 X- M1 j high endo) atmosphere. (Predecessor to Endo-Exoatmospheric Interceptor0 M" @- [5 T- o* d (E2I).) 0 a) x! M: D* ]+ F) u6 NMDA GLOSSARY, VER. 4.0 H 5 J1 h1 r, F5 k5 O* T127, Q2 I/ }. f! r High Density8 J& I) d; t3 A N# s Aerospace 9 B- p8 W' o$ z9 I0 s9 @: H) jControl Zone $ |" r8 e" L1 s7 E. [, D0 C(HIDACZ) ) G R$ P4 @/ B; T% {1 dAirspace designated in an airspace control plan or airspace control order, in 9 ]' c6 d3 B, S- e0 d. g( Fwhich there is a concentrated employment of various weapons and users. A 8 W; ~. u+ X* {HIDACZ has defined dimensions, that usually coincide with geographical + ^# \( a& R; @8 e3 D/ Y1 yfeatures or navigational aides. Access to a HIDACZ is normally controlled by the& r0 d0 d- k! J# d( w$ V0 y maneuver commander. The maneuver commander can also direct a more7 v L6 V, L# K% ~ restrictive weapons status within the HIDACZ.$ t( q& P6 ^ A' ^ Higher Authority 5 x; ?$ r5 O u6 j9 |7 _! UInterface & J% {1 b8 u, q" IPolicy, strategy, doctrine, readiness conditions, and rules of engagement from: J3 B& c& Z' { higher authorities for use by the defense system in conducting system+ x+ j; n0 T( C8 J operations including specific orders specifying actions such as testing, defense ( l- \ J3 J8 u3 L& o; tenabling, pre-delegation of authority, etc. Also the reporting of situation- _( r; m5 b# w2 V' l- H; j assessment and system readiness to higher authority. w, |4 }( O5 G8 W I7 u/ V High Order 0 U3 ~9 ~. d% z& u/ _- R9 wLanguage (HOL) & D/ Z3 L- P$ A3 e4 ?. E9 B& z2 uA programming language that requires little knowledge of the computer on which , U7 x, Y% N; v; \: ra program will run, can be translated into several different machine languages,+ T% t9 _2 X. c1 |) m+ z2 J allows symbolic naming of operations and addresses, provides features2 ~3 T8 |6 A+ H- e. U; l. V designed to facilitate expression of data structures and program logic, and 9 {& ^2 a+ a* _" S, [) z2 {usually results in several machine instructions for each program statement. 0 W& q7 i! t. y' d! xHIL Human In-the-Loop.( b- V* s8 D& V; O1 g HIMAD High to Medium Altitude Air Defense. ) F/ d8 _: Z9 SHIMEZ High Altitude Missile Engagement Zone.! G$ m9 u0 g2 o HIP Hot Isostatic Processing.8 e; \/ F4 H Z N HIRAM High Resolution Infrared Auroral Measurements.9 M+ _$ j4 B, D+ P+ `' y HISEM High Speed Environmental Multi-burst Model.7 ]3 F9 b/ w5 H0 x HIT (1) Heterojuncture Internal Photomissive. (2) Homing Interceptor Technology. 5 X2 z5 I9 Y; N* t, c/ g4 EHK Hard Kill.4 g. z, X5 w0 Y# d, g HKV Hit to Kill Vehicle. - ^2 M1 ]; f- M: r. g) Q$ qHLD Hardware Description Language. / ?7 R8 ]3 ]7 N& gHLLV Heavy Lift Launch Vehicle. ( [5 `1 ~1 @1 b. N4 a1 q: XHMC&M Hazardous Material Control and Management. 9 o! _; B O' gHMI Human Machine Interface.( I1 q% R9 w* f2 E8 s2 g& B5 } HMMWV High Mobility Mutli-purpose Whealed Vehicle (USA term) (pronounced Hum Vee). * G) ]& w, n4 E* J8 I9 M" }* vHMPC Hazardous Maintenance Procedure Code. & U$ _) Y- Z! j8 @; R$ D5 |1 yHMSC Hughes Missile System Corporation. 0 k% `. |# U" W% D9 J/ gHOB Height of Burst. 8 `# e5 ^( B! s! @7 d6 KHOE OBSOLETE. Homing Overlay Experiment. (Predecessor program to 9 S& d+ ]6 |) F: Y5 \7 xExoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS).)" G: r$ J) l) j% o6 ^# } HOL High Order Language. : k( X' U& u8 J3 X) o. |$ D" iMDA GLOSSARY, VER. 4.0 H) x3 E# T; ~ j1 V 128 # g" o5 ~; ~+ T+ oHoming All-the- ) d. D, S% o6 p* z' N4 rWay Killer2 o. N/ T- l( t8 k7 k (HAWK)5 S, j$ s2 r) d9 s (1) Upgrades to the HAWK interceptor and radar system to provide the * Y( z; `) g2 Q: ~1 ~Marine Corps with a mobile point theater ballistic missile defense% i e* a5 V& O( [: b0 p) M capability. % t. Y4 _6 t) k. ]) l/ ~) M% v(2) A mobile air defense artillery, surface-to-air missile system that provides, X0 g0 M8 W1 j! p6 x non-nuclear, low to medium altitude air defense coverage for ground - Y7 Y2 T# E+ M& fforces. Designated as MIM-23.: P" Z8 A" g+ i! k3 t9 r Homing Device A device, mounted on a missile, to aid its guidance to a target. The homing ; A& P2 U1 b# K3 |device uses sensors to detect the position of, or to help predict the future! }0 u/ j# g% Z5 T* D6 s5 n position of a target, and then directs the missile to intercept it. The homing/ z1 E3 x, s5 p1 O* p device usually provides frequent target position updates during the flight of the# o$ d) K6 \9 k/ Z9 V" w missile. % y+ J" K/ D9 C% u2 e1 ~Homing/ {$ X: }- H2 o# }% |1 F Guidance3 e4 D+ a; B& m9 |3 i5 I A system by which a missile steers itself towards a target by means of a selfcontained mechanism which is activated by some distinguishing characteristics of + o2 ~7 E7 I D( m& A1 p+ Wthe target, such as an infrared signature.6 _/ V3 n, z9 A" I HOMS Homing Overlay Mission Simulation.( y4 T3 b/ Y, w# c& _8 k* q3 C1 F! | HOST Hardened Optical Sensor Testbed. % ?6 s. @' t8 ?" B: v% h; YHost Installation A designated DoD facility that provides non peculiar SDS support of SDS3 v; c* e2 x2 D. B7 U elements. $ E; F' B* h7 X- N" b. wHostile( D' M* E; W4 l: b Environment8 M7 q) L% x1 Y, k; a Those environments that result from a BMD system engagement of an enemy% a) g) \; h5 a2 T1 I% M threat or collateral conditions resulting from deliberate hostilities. Hostile* G0 S, N, T# k- @: p; C; ^ environment categories currently applicable to National Missile Defense are# b9 q) ?5 S( r4 q- t8 F Nuclear, Battle Debris, and Electronic Warfare. " A, M/ O% x' u- e8 e. pHostile Track The classification assigned to a track that, based upon established criteria, is) h6 P$ |: |4 S& s" M determined to be an enemy threat.* X% q8 S- o3 l: j8 c; `( k4 s- ~ Host Interface The interface between a communications processor and a host computer. / s. ^/ n4 O9 t1 Z1 c7 U! T& OHost Nation & k0 C2 Z$ {1 S/ V W. @+ G6 rSupport% w! U( _: Q( d9 Q Civil and/or military assistance rendered by a nation to foreign forces within its 4 ^7 W+ e) t; V+ i9 ] ]' Z$ E5 Fterritory during peacetime, crisis or emergencies, or war based on agreements3 I8 i, C5 R% Z M8 k4 p concluded between nations.2 y$ o2 y! t/ A/ Y+ U$ `% B: w! ?0 O hp Horsepower.- ~1 t' {# L2 I+ H( x! x* A- N HPA High Power Amplifier. - y/ B6 G. l/ M2 T+ e& GHPC High Performance Computing. & P. `0 [+ [; x fHPCC High Performance Computing and Communications. % m6 ] d3 ]6 c1 X# N! ]( @6 r" CHPG Homopolar Generator.' j6 a" g& }4 w) x/ T HPI High Power Illuminator (Hawk).5 r4 v; w7 D/ n" [* r$ f+ J3 a HPIR High Power Illuminator Radar.+ G# [5 m+ v( k8 V! k: V/ E" _ HPL High Power Laser.: v# p; d5 X9 c0 m. @% p' ^4 A. k HPM High Power Microwave.6 f, v5 A* S% e, w0 e S" T HQ Headquarters. 0 E$ X1 Z7 {; z4 Q/ O! m N2 p: e, iMDA GLOSSARY, VER. 4.0 H , A) z: q+ {% ?2 j129! n) E- s: D0 S6 a HQMC Headquarters, Marine Corps.$ i* A% \7 n; C! f HRDS High Resolution Display System.; F+ {, H9 d7 s9 B; Z HREPS Heavy Replicas. B% V1 U$ {' ~& ]4 d2 e HRR High Range Resolution.- X; \5 l3 p* U# f; \9 {4 [ HRSA HICTB Requirements, Support and Analysis. ) N1 u5 _8 N. G$ s ^$ r; u1 ]HSDB High Speed Data Bus (TelComm/Computer term).2 _- z# g& y0 Z5 F HSFB High Speed Fleet Broadcast (Navy term). ) |$ P" L7 R0 s$ S, E( ^" ?2 S% BHSI Human Systems Integration.5 A5 J5 n% K& R7 d1 k' ~- l) U7 Q: g HSV Huntsville, Alabama. , Y: r/ W1 M4 UHTICIA High Technology Crime Investigation Association. `7 u- P- ?- N/ C2 c+ w* }HTI Horizontal Technology Initiative.1 w* @& l2 D' v6 u HTK Hit-to-Kill. ! v; m6 p$ Z1 n4 RHTMIAC High Temperature Materials Information Analysis Center. 0 n1 O6 V( U. _7 M0 I6 D2 ~. I' YHTML Hypertext Markup Language. : g3 h6 k% Q, A! C+ u( u8 ]7 GHTPB Hydroxy-Terminated Poly Butadiene. - \ j# w: \$ T& tHTS (1) High Temperature Super-conducting. (2) Hawaii Tracking Station.5 s+ M, V; k1 {; {, V7 b HTSA Host Tenant Support Agreement./ W2 a8 c/ \5 f' y: l b/ V% w HTSS Hardened- sub-miniature Telemetry and Sensor System. 5 J5 C- k$ r' E; D% O4 RHTTP Hypertext Transfer Protocol. ) w* J- X+ T0 B* v+ b3 ^, wHUD Heads Up Display.- Y- {. Q# H- u Human Factors A body of scientific facts about human characteristics. The term covers all 8 B" l6 Q) M" wbiomedical and psychosocial considerations; it includes, but is not limited to, ) j' P+ U9 |( y3 Fprinciples and applications in the areas of human engineering, personnel ( I8 t4 X+ ?8 H/ {5 r% |( Rselection, training, life support, job performance aids, and human performance y+ q8 p5 s) O' t! R# x1 t" fevaluation. 0 z! B# t/ |8 v6 O" lHuman Factors0 D, A/ ~8 i* G2 v Engineering6 |7 b7 o; }, t# b q5 P# Y The design of man-made devices, systems, and environments to enhance their3 Q& i5 {4 O& D+ ^6 b' R use by people. Also called human engineering, human factors, and ergonomics.

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