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Rank: 9Rank: 9Rank: 9

41#
发表于 2008-12-25 20:05:33 |只看该作者
ELPRS Enhanced Position Location Reporting System. 6 l+ ]4 `/ d1 j6 k" ^/ ZELS Earth Limb Sensor. * u m3 h" @! e/ C8 p. x: BELSEC Electronics Security. 9 N, C: {7 p. A5 |1 X3 X6 YELSI Enhanced Longwave Spectrometer Imager. 7 Q! }! a, W* d6 |ELV Expendable Launch Vehicle.4 H! D& R+ `: J+ r" v' l" L Emanations0 u$ x& t: r2 b% S+ y$ R Security9 m. W7 t" I# I n2 ?) k (EMSEC)* f% K& O: \( Y The protection that results from all measures designed to deny unauthorized 3 W+ L: \2 j: X1 Apersons information of value that might be derived from intercept and analysis of* j- G; ^4 B7 C) y+ U; T/ d compromising emanations. 7 g7 V3 p+ H" u5 {5 rEMC (1) Electromagnetic Compatibility. (2) Early Midcourse.2 O6 w( s7 g% A8 m& s: s EMCON Emission Control 1 g8 N0 N. A, [/ [1 F2 r4 lEMD Engineering and Manufacturing Development (previously referred to as FSD).3 o2 K$ q+ K4 ~! v Q$ x EMDCT Expanded Memory DCT.' D; H; B* \0 Y- B! r% x2 B1 k EME Electromagnetic Environment.4 O, _; f: u& Y4 i0 u6 j MDA GLOSSARY, VER. 4.0 E a! |7 G! ]$ j: ^. s, G93, N- w: e3 k% t; S2 l% R/ o2 |: ~ Emergency 8 N1 K0 a3 ` K. U( W- N# x7 yCapability, l/ o; b5 v+ s s: H+ c: s (replaces 8 p2 }) O0 W' r; B3 d( Z9 R4 iContingency+ Y7 ~. F) g* Y/ j' a Capability)7 b6 f. K* }3 e* O, ` BMDS elements or components that are still in development or testing that1 s1 c7 n! |! G8 B2 x. k0 B( ? provide limited ballistic missile defense capabilities. MDA, working with the, f0 ^3 s, O7 x: Y Services, will develop plans, which cover the potential use of prototypes and test , b) M6 G4 f% ^3 h2 E% Eassets for contingency deployment should the SECDEF determine that an4 s3 U I8 l4 C7 E4 a emerging BMD threat requires emergency fielding of a BMDS capability. ) M6 i9 \5 ?$ l! V+ g" e% sEMF Electromagnetic Field. ' V/ B6 g$ `& T5 A/ f% _EMG Electromagnetic Gun.- k$ L* U. ~( S" v7 @ EMI Electromagnetic Interference. 1 N8 G# a. b$ r1 u! REMIP See Exoatmospheric Midcourse Interceptor Program.1 S. ]7 [ R6 J x8 C' f1 \" Y Emission Control) ]+ z+ x5 o2 d( }2 M* M( Q (EMCON) 2 Z7 {" V! G& j* rThe selective and controlled use of electromagnetic, acoustic, or other emitters! u6 h4 i! y* f& @ to optimize command and control capabilities while minimizing: a) detection by ; A5 @7 K* w- K0 Oenemy sensors, and b) mutual interference among friendly systems. EMCON 8 S1 w) @, y9 T% G: A6 F1 W: Lcan also be involved in military deception plans. Also called EMCON.8 y9 Y+ z) w Q9 I( A" n- t EML Electromagnetic Launcher. A device used to launch hypervelocity particles. % M4 ^; h& E2 w3 [ l" tEMP Electromagnetic Pulse.+ N& i! z# Z3 D! L EMPSKD Employment Scheduling (USN term). , v$ Q1 \# m' S' e+ BEMR Electromagnetic Radiation. 0 H% q: h& X6 KEMRLD Excimer Moderate Power Raman-Shifted Laser Device. 4 J, C7 q# Z* x n) p( z: ZEMSEC Emanations Security. # o/ q: `/ n' {$ r$ J4 v( p% S( \% dEMSP Enhanced Modular Signal Processor.7 N! G* X- L, ` EMT Engineering Management Team.* I: v0 d+ M& E0 N: q& R1 q4 L8 ] EMV Electromagnetic Vulnerability.) q e. r; ]# P5 ^ k ENA Engineering: Architecture and Analysis.; W& W9 C5 J+ J4 n" u$ @' T ENCATT Engineer CATT (US Army term). L# j6 j. z: ~0 @3 Z Enclave Isolated resource – an SDS asset that has lost connectivity with other SDS3 }9 k: ~) k. O assets with which it normally has connectivity, but is still capable of coordinating0 k" M8 a8 r3 U% p with SDS assets to conduct ballistic missile defense. Various combinations of 0 {* g' d8 r+ }3 n: ?. [' t3 pconnectivity losses are possible; for example, (1) an operations center has lost. X- q7 V3 O. S) j, w% S2 D/ ~% m connectivity with Higher Authority, yet can still provide sufficient C2 and can still. M/ `& D/ s, U' n, Z connect with sufficient weapons and sensors to conduct an engagement and (2)+ W! ?- @" d! u. w* d an operations center has loss of connectivity with another operations center with . S v! y+ w9 o8 m% e, Fwhich it normally shares data, but can still conduct an engagement.9 w+ l. E$ k$ t" j: Z- K! f Endgame FOV The field of view of the interceptor’s sensor during its final maneuvers after target % O' \& Z5 w! O1 O0 @* V/ sacquisition to intercept the target. May be less than the acquisition FOV. + b/ G/ `8 P: xEnd Item The final production product when assembled, or completed, and ready for 9 {8 n9 @) {; L* h/ H1 Qissue/deployment. $ F2 ]! ?6 Y; O/ T% ~, {5 WMDA GLOSSARY, VER. 4.0 E; z0 A6 _7 n5 J0 H) g 94; w$ a* g6 O/ F+ S! y5 z r Endoatmospheric Within the earth’s atmosphere; generally considered to be altitudes below 100 ( r: ?; e7 v' _- |8 Rkm. An endoatmospheric interceptor reaches its target within the atmosphere. % U# g5 w) {7 W& iEndo- 4 w' N7 q- G9 A! h$ xExoatmospheric 6 Q8 ~+ }$ _3 h, M: j. r* EInterceptor (E2 I)" C ]: m/ G+ _) B! T7 U. @ A ground-based interceptor capable of engaging RVs either endoatmospheric or4 i% E" e5 f/ [- l$ s exoatmospheric. (Successor to High Endoatmospheric Defense Interceptor 9 H& Z; L C% v" e' N(HEDI).) ; ^; _9 K$ A3 p# FENDOSIM Endoatmospheric Simulation.6 c9 A" h4 J+ t3 X% g Endurance The time an aircraft can continue flying, or a ground vehicle or ship can continue % s' w" T( j" P/ R+ G% eoperating, under specified conditions, e.g. without refueling.9 c* I/ ?* N8 v1 V6 ^ ENG Engineering.& I% m! @: `5 K0 q0 ~& j( p: ~( ^ ENGAG’T Engagement.6 e5 s5 p' H' a; ` Engage (1) In air defense, a fire control order used to direct or authorize units and/or: b4 _& T3 O- n0 }/ n weapon systems to fire on a designated target.6 v: z# h6 o5 ^8 f- Z2 ~. B# u3 s2 w (2) In air intercept, a code meaning, “Attack designated contact.” 0 m' n( |8 a, C2 Y6 f H& {Engagement (1) A period of hostilities beginning when the first ballistic missile target& [4 { L4 F# b$ Y7 N; ? undergoes fire from the first defensive weapon. & \. F5 V- S d( a, h; r: m0 r(2) A period beginning whenever any hostile object is identified (designated) ( A" Q, }! X; Z8 ras hostile and ending after the last hostile object has been attacked. " T, C. ~$ j$ l(3) In air defense, an attack with guns or air-to-air missiles by an interceptor * `1 t* k( N/ U, @% e6 ?. P/ zaircraft, or the launch of an air defense missile by air defense artillery and , ~) ~( b7 \' hthe missile’s subsequent travel to intercept.$ t( k0 [7 }2 l9 S8 t Engagement 6 q: e9 v8 j- Z- w$ d7 ZAuthorization 7 k) `/ \0 b6 I. Z! m0 XThe authorization given to USSPACECOM to use weapon and sensor systems 0 ]# R6 j2 L5 j& {4 Runder previously coordinated and authorized rules, procedures, and conditions. , x# h7 @) x7 `) R5 b' A( EEngagement; {: h3 v% y/ P; b6 L& H, I Control ; O9 Y. k8 p; e! ?( [: ](1) That set of coordination, assessment, decision, and direction functions5 b# H9 V4 G5 `7 n& p8 h; `8 r( j$ ] normally implemented automatically to execute the selected battle plan, b5 V2 R6 I2 q: a$ ^- k$ Ymilitary strategy and tactics within partitioned battle spaces (i.e., a1 f/ s( c0 j# S" W# } spatial/functional subdivision of battle management). Includes the # S0 q3 e1 W/ q$ G( P4 A( C9 Qdetermination of: what specific objects to intercept in order to implement q2 A8 H; q" A3 k- Nthe selected military strategy, and which specific interceptors to assign to 9 `9 c+ ?: L% \) x8 {each attacker to implement the selected tactics within the rules of Q+ W+ a7 n3 i2 q engagement. , a, G- C* P) m7 R, K3 t(2) In air defense, that degree of control exercised over the operational 8 t" `# J, A8 `$ \functions of an air defense unit that are related to detection,6 ?1 S7 y. ?* i0 y$ a7 a1 L 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
Engagement & b9 _1 I9 p4 t) G. O5 ]3 o/ M2 NPlanning 5 E! P2 O9 S4 M0 c+ l, L- l uA set of rules and parameters to be used in developing weapon-target9 o. i3 H' \2 o2 @$ b9 M1 l6 m( C assignments and for sensor resource management. (USSPACECOM)0 z7 N. K! R; r( x B$ e) k( W$ R Engagement ; r5 Z0 b3 B7 Z( mSurveillance. ?" Q" M$ n% d2 r# C The surveillance required to support RV negation in the midcourse tier. $ w6 d2 m% V" G! E9 r, MEngagement ! Q9 w$ K& K5 l$ z1 j1 d0 HTime * i3 O6 ]" N! g* u, { tThe time that a weapon takes while engaging a given target. This includes not0 m' D3 x3 R6 Q9 W! T0 }( \9 M9 y& E only firing at the target but all other necessary weapon functions involved that + V! Q0 {: j# E+ ^" Gare unique to that particular target.+ v8 ~# [3 k: K MDA GLOSSARY, VER. 4.0 E; |# ?) k2 e O0 F; B 952 E/ ]7 X/ i# ^9 x6 y Engineering and , s3 s; x& y. a9 q3 tManufacturing $ k4 @6 Y' ^. r4 qDevelopment3 i4 Z! p% F+ s6 l (EMD) 1 E5 Z8 G) y$ l9 TThe third phase in the acquisition process, following Milestone II. The system * m' H0 V2 [% g, j) [and its supporting items are fully developed, engineered, designed, fabricated,8 m& o4 T& ]# f+ e6 F1 O tested, and evaluated. The intended output is a pre-production system that 6 s6 P, O2 E. Y C( n' _& I1 Mclosely approximates the final product; the documentation necessary to enter the 0 G+ i# U( {* ~. d( l8 Tproduction phase, and the test results demonstrating that the production product 5 A8 Y, I! r* ^6 q. j" }will meet stated requirements. $ M1 I K) J) s+ g7 MEngineering- v& I2 l6 y; q9 r+ p+ l Change Proposal3 C: W& f$ t# I5 E2 ~& f (ECP)! b4 G- l: v3 g9 ~ A proposal to the responsible authority recommending that a change to an 6 q; w }1 O4 moriginal item of equipment be considered, and the design or engineering change 0 {1 I G# ]/ G; K) F, X0 ebe incorporated into the article to modify, add to, delete, or supersede original9 d& y/ L/ A( a6 e3 H& S8 r1 G parts. ! D: r* M! I$ n4 n5 x' l7 TEngineering; v' C% e; n8 ^! G Development 8 z3 C @8 ^$ M* g4 RA funding category including those development programs being engineered for $ y+ F( Y* o& i2 `5 q1 Nservice use but which have not yet been approved for procurement or operation. 3 }0 V8 \/ ~% G$ `% @Money under budget activity 6.4. + u/ K7 x$ z) c4 _1 m8 _1 LEngineering% F) j' X6 \" x1 e7 P2 }. e Development 1 D2 j! J$ x# g/ I9 e5 E$ k4 kModel1 u! t+ K! R, c) [ Enhanced Target* P8 P" {' I) N- d: {5 O Delivery System 7 N8 C- J, E. J. I# I+ S M0 R(ETDS) 9 G* p( x- v, m6 q% i8 zAn advanced prototype used during the Engineering and Manufacturing " }' }4 k: h* w; a6 E5 NDevelopment phase (EMD) to resolve design deficiencies, demonstrate maturing ( u+ t: j1 s- v* F8 l4 ^. ^ bperformance, and develop proposed production specifications and drawings./ _. [( d" B* L: I Target delivery system being developed for future GMD testing that will, O1 ^4 _$ T) `, ~7 I9 K9 ~ complement existing systems, provide flexible, modular configurations, and will 4 f7 n& R+ F( ] z6 b8 A1 r( d8 _be launchable from land, air, or sea modes d* ~8 w0 m0 u1 U ENNK Endoatmospheric Non-Nuclear Kill. 5 P2 U: i% E4 G; ?* j* r$ s7 NENSCD Enemy Situation and Correlation Division (JFACC term).& V7 u" A$ J% {: s$ y6 v* V Environmental ! P* w- Z2 f w0 g+ u; EAssessment (EA) * x% Y u4 j. |A concise public document whose primary purpose is to provide sufficient$ Z& f$ ?2 y: z9 Z2 A3 G' } analysis of environmental effects of an action to determine whether to prepare 2 M+ s4 S$ ?% N* Zan environmental impact statement or a finding of no significant impact.5 I6 z0 v4 q4 @% y/ ^ Environmental W m1 J" A. Y2 z# uImpact Statement 1 M0 X% w& L6 \' p+ V9 w- a8 e(EIS): P# ^! S$ o% j1 `; p A detailed written statement analyzing the environmental effects of a major1 p5 o1 q7 @' ]- w" p Federal action.; g4 e" o6 N$ {/ N Environmental( w+ _1 J$ L; l q2 q; b Security# n# {* b( f. R5 w0 @ A specialized form of physical security that prevents technical penetration, e.g., : d; B7 ]+ E# B' }$ `. G# Hpenetration by waves of electron beams.) ]( D8 l& R2 O Environments The media, conditions, and/or physical objects in which a BMD asset is immersed9 X. ?8 k2 t' F/ I z or surrounded. For BMD systems and elements, the comprehensive # w* C7 `1 {/ ~8 T* e: m2 Genvironments definition consists of natural, hostile, induced, and storage,3 c1 t# p6 d* o6 f# U7 i. o transportation and handling categories. 4 H* | f r X6 Q/ R- q K/ q9 TEO (1) Electro-Optical. 7 G) ~+ k+ L4 `6 R(2) Engagement Operations. ' q' H- S9 x7 N. c" l6 D(3) End Office. : g7 X t6 G% |3 d R" {3 l: W(4) Eyes Only.% H% v8 S# I' ?& t' D2 U; u; c. A EOA Early Operational Assessment. 6 m7 j' x3 F! sEOB (1) Enemy Order of Battle. 6 ~, C3 G( J" S1 Q(2) Electronic Order of Battle. X$ f) J5 n3 u- X/ uEOC (1) See Element Operations Center.; {3 f" _, Q2 t, X: c- y6 }8 Q! [ l (2) Emergency Operations Center$ }; Z$ u* g0 p# D# V6 n! ^ MDA GLOSSARY, VER. 4.0 E, g* A* l0 D8 i; @) { 96# N0 `/ f$ E( ]5 s( M& f% p EOCM Electro-Optic Countermeasure.2 ]3 k. O D! s( d4 _: |' l EOCT Element Operations Center Test Bed. ~/ g D }/ x+ m" b EOD Explosive Ordnance Detail# ~# ~5 W9 I% Y6 f% t6 o4 v EO/IR See Electro-Optics Infrared.* r6 Y0 U; A$ j2 u EOM End of Message. ' P" L% k i4 t/ ~$ q2 TEOP Executive Office of the President+ Y _8 x8 a" ?; H" N: f+ s5 S. t EORSAT ELINT Ocean Reconnaissance Satellite (US). & q* {* t0 l2 h! x: H' G, P: XEOS Earth Orbiting System (NASA term)./ y- O9 c! N% J4 T6 ? EOSH Environmental Operational Safety and Health. 1 B7 S! ~0 @2 Q* R b$ ~EP (1) Engagement Planning. (2) Evaluation Plan ! F7 @8 X- J) A5 H% h* t. CEP Cycle Engagement Planner Cycle (NMD BMC2 term). : }. c3 N Q) Y. S1 IEPA Environmental Protection Agency.7 I& x& \( o0 n( V) W& j/ N. e EPD Engineering Product and Development7 G- O2 K* W$ p% b) b% [: d Ephemeris/2 I7 t$ s, a/ D! L& x6 j Ephemerides - L \8 d' \9 k% k4 g2 g: H" \(1) A table showing the positions of an object in space at regular intervals of6 I( ]' B8 j. [) N8 T0 x% M time.2 B8 Y, x" T+ I* l- ^4 a (2) A publication giving the computed places of the celestial bodies for each0 y% s: T3 H- b day of the year or for other regular intervals.4 H9 D2 p$ n4 J/ w A' R2 L6 S/ p EPITS Essential Program Information Technology and Systems. 8 n1 T! ] w; |: F$ mEPL Emitter Parameter Listing (USN term). & L5 B% V/ j) c# v. [6 mEPLRS Enhanced Position Locator Reporting System. 5 \& z' y& @1 Y5 D( k: YEPO (1) OBSOLETE - ERINT Project Office (US Army term). (2) Element Program y- [" P3 H' YOffice.1 f, \ B( G6 k( f; M; W5 m! `+ P EPP Electric Power Plant (PATRIOT). / @) Y0 \- ?, R3 vEPROM Electrically Programmable Read-Only Memory.; o! E {2 c* r8 ]* H EQEC EurQuantum Electronics Conference (See CLEO). ; b: v4 ?& X6 y! _/ \) d2 N9 WEquipment5 D" [3 _) L" q/ Z$ u: l Operationally: L! H$ C; B( v& z Ready ( W& ^ B ^4 ^The status of an item of equipment in the possession of an operating unit that : r# _. C( f2 d( ?indicates it is capable of fulfilling its intended mission and in a system, c( ~1 e% ^/ w0 `: w: F configuration that offers a high assurance of an effective, reliable, and safe 5 T% U( v' a" j0 |performance.) a3 O' Y0 F: i5 ^7 m- n" q* H) W ER (1) Enhanced Radiation (“neutron bomb”). (2) Extended Range.4 G) p/ I/ }; ]& W9 ~, g' H ERA Explosive Reactive Armor8 w' m+ C& g) @8 Q% p* v, N( Y ERADCOM OBSOLETE. Army Electronics Research and Development Command. (Now* c9 A% K% ^) ^5 n Laboratory Command (LABCOM), Adelphi, MD.) & U( Q+ n8 \' g/ o7 S6 AMDA GLOSSARY, VER. 4.0 E % c( v* A7 [* H7 G97 9 }& A& Q" K/ l* FERCS Emergency Rocket Communications System (US). $ t) ?' s5 U0 }- ^+ gERD Element Requirements Document. _$ b j2 {: Z8 A( ]ERG Executive Review Group. + N% V) u0 s- i7 t, vERINT OBSOLETE. Extended Range Interceptor. Now referred to as PAC-3. " q- W% L3 W: kERIS OBSOLETE. Exoatmospheric Reentry Vehicle Interceptor Subsystem.4 T" x: j8 g6 u: K; ^9 ^ (Predecessor to Ground-Based Interceptor (GBI).)4 S' o7 D. v- B! X6 g ERIS(F) OBSOLETE. ERIS Farm. 8 b8 V A! A! U8 nERP Emitted Radiative Power. * G8 J! H1 |: r2 _$ V+ C) P1 `# [& C% eERR (1) Element Requirements Review. (2) Engineering Release Record. 7 y7 U9 F$ G6 Q) w+ T$ ]ERS (1) Early Release of Submunitions. (2) Emergency Response System.+ ~: B2 |* c6 K' @7 t9 z& l ESA Electronically Scanned Array. : B% k9 t' c: j" g8 O2 kESAD Electronic Safe and Arm Device. 5 q! t2 M1 m$ G; m, L/ j/ |ESAR Extended Subsequent Application Review. , g- T, y3 n" d6 ? d& I' [! t% ~1 uESC Electronic System Center (AFMC), Hanscom AFB, MA. B4 ^. M! r0 D" e ESCN Existing Systems and Center Notebook. 9 p. Q9 _1 J( ?% m4 AESD OBSOLETE. Electronic Systems Division. (Now Electronic Systems Center,' E) |4 b0 m5 | f, h1 A8 R Hanscom AFB, MA.) _: X7 l4 J/ F0 s+ Q ESH Environmental, Safety and Health : `, D. r( R, z# @# bESI External Systems Integration. G" ~$ ]$ N! bESI ICD External Systems Integration Interface Control Document. ) i7 o8 Q' k0 Y; Q$ EESM (1) Electronic Warfare Support Measures. (2) Electronic Support Measures.$ m, |8 c8 E2 M% x2 | ESMC Eastern Space and Missile Center, Patrick AFB, FL. # t9 I- t. S/ D% ?ESNet Energy Sciences Network. $ L: T4 [1 w2 m8 L7 Q. X+ C9 ZESPRIT European Strategic Program of Research in Information Technology.3 e, n! S1 F/ j ESQD Explosive Safety Quantity Distance.) S n4 q& v3 h v5 t5 I ESSM Evolved (Enhanced) Sea Sparrow Missile. 2 s3 ?$ e0 X& o2 d) ^3 s. VET&C Extended Tracking and Control.: g9 D' P1 b6 k" k( h ETA Estimated Time of Arrival.2 [5 y' K+ M. d! U" R ETC (1) Electro-Thermal Chemical. (2) Estimated Time-to-Completion. ; X+ O# C$ V* S0 PETD (1) Estimated Time of Departure. (2) Electronic Transfer Device.# Z9 f: Q6 Q- e, X) N MDA GLOSSARY, VER. 4.0 E 8 j, c" S5 y x% ]( ?. C7 T6 b98" o5 t& g7 R( F) G ETERTS End-to-End Real Time Simulator. . P& Q% l' w6 _( j bETESD End-to-End Sensor Demonstration. 1 D' V% Y4 D( [5 d* TETI Estimated Time of Intercept. 3 d, R E! F! ^. G7 C& b- S0 ?ETIC Estimated Time for Completion.5 Z& s' S9 W9 O5 M3 Q4 O7 U ~ ETM Engineering Test Model: L% j* m7 F; R( ` ETR (1) Extended Test Range (Pacific Test Bed) (2) See Eastern Test Range. (3)2 y% K, c$ Q: }6 k: h; c& @; o9 ] Environmental Test Round. (4) Estimated Time to Repair. 3 U) D2 L0 ~3 I/ S UETS (1) Experimental Test System. (2) Experimental Test Site. ; N" q H2 \) `5 N' g1 C# @EU European Union [formerly European Community (ECI)]1 A; i+ ]4 l% v EUCOM European Command. See USEUCOM.+ D8 L. c( H/ J) Y EURATOM European Atomic Energy Agency. $ }% k8 t8 Z$ G9 XEUREKA European Research and Coordinating Agency.; c2 [: \9 a3 a. z% a$ V F EUT Early User Test. , ^' T( @# d' R5 r. A& LEV Experimental Version ) R2 t. P7 F3 s0 IEVA Extravehicular Activity. , ~% x' b$ w4 s; HEvasive MRV A reentry vehicle, which maneuvers for the purpose of evading defensive 6 R1 [/ r" j3 |weapons. : m$ o; Y& M) @8 x: |Event Based; g8 R. c0 T# ?* [0 Z Contracting + `( m+ B6 ?4 \2 `8 [; ?Support “event driven acquisition strategy” by linking specific contractual events( w5 b4 D8 l) H to the “exit criteria” for the acquisition phase, or to intermediate development6 p3 r8 J# J( q/ g4 ]3 m events established for the acquisition strategy. 1 F/ g+ o8 r; y' n: hEvent Driven3 q) k- g" l$ v( W6 q0 O ` Acquisition 2 u6 Z- A5 O/ cStrategy- o& [+ o% e6 p% k An acquisition strategy that links program decisions to demonstrated- L; e1 j/ {9 W( d) X2 F; e accomplishments in development, testing, and production. 2 v! v2 J7 q8 t5 b' e, v, REvent Validation A sensor element internal process that results in a determination by the operator 4 Z8 y. v* u$ d/ \4 Zthat 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
Event) A1 w! g. ]& P7 R5 H& ~ Verification " v/ x# k3 s/ @* i8 \! f2 N: NThe process by which it is decided, from SDS external data, that the event 2 X' c" G8 W9 P, t2 U, O1 g+ _( Ereported is real.* L/ g% a$ Y6 [& p MDA GLOSSARY, VER. 4.0 E9 H0 l6 H9 D2 g/ B1 H* ? 99 3 O- S5 j% L y- V# KEvolutionary : h2 j3 K. l8 J+ n" _) xAcquisition' O3 P& `# T% u5 y (1) An approach in which a core capability is fielded, and the system design has 6 y( x$ R3 L2 u3 F& s0 t+ ya modular structure and provisions for future upgrades and changes as ! b' ^; n( W4 X' Grequirements are refined. An evolutionary acquisition strategy is well suited to. b8 m" \' h! F. Y, m. i- J7 e/ ` high technology and software intensive programs where requirements beyond a & E& T c {3 ^: D% e( mcore capability can be generally, but not specifically, be defined. " V: E& Q5 E9 }" }(2) An acquisition strategy that defines, develops, produces or acquires, and. E) D5 S+ g2 C K3 u' q fields an initial hardware or software increment (or block) of operational capability. 9 w; R( g. o0 DIt is based on technologies demonstrated in relevant environments, time-phased: s4 \! P% D4 R requirements, and demonstrated manufacturing or software deployment ' j* m* |7 e7 g4 K; m* Ycapabilities. These capabilities can be provided in a shorter period of time, 2 e# o9 m* `' Ufollowed by subsequent increments of capability over time that accommodate# F- }/ g$ I/ A0 x5 z7 c improved technology and allowing for full and adaptable systems over time. Each' c" }1 v4 H6 s8 o* q4 | n increment will meet a militarily useful capability specified by the user (i.e., at least - x( l% c4 e) Othe thresholds set by the user for that increment); however, the first increment0 Q; h/ N8 B7 H: ]6 j may represent only 60% to 80% of the desired final capability. (MDA Lexicon)8 x. A* k) h7 J* I+ t Evolutionary % r0 z* d% ?, V: ?/ K6 k2 ^Requirements : B- m- S5 I0 @( K5 DDefinition0 F$ m4 t/ \% c( u4 m0 t% w4 G Mission needs are first expressed in broad operational capability terms, and then " A e! w7 S: y0 Eprogressively evolved to system specific performance requirements.$ q8 {* W. n) f EVPA Experimental Version Performance Assessment.: _% [) z% s7 Y! C EVPA/TEVS Experimental Version Performance Assessment Test Environment System." K3 w. d$ d) k2 H' t EVS Enhanced Verdin System. + W/ N# F( b, ]- Y) i$ bEW (1) Electronic Warfare. (2) Early Warning. 3 }- g+ E' |3 h: Q( pEW/AA Early Warning and Attack Assessment. ; s. \! H! E; r1 g, c0 N# ^ K0 fEWCC Expanded Weapons Control Computer (PATRIOT). ) o5 ^9 ^5 |0 z$ Y, l- }% XEWDA Energy and Water Development Appropriations (US). : Z" Y# ?8 a% g8 [) p* x" F; {EWG Event Working Group. 3 [. F4 C, K! c# WEWN Early Warning Net. / m/ f7 B+ p- r& s: XEWO Electronic Warfare Officer.3 t* v9 w, b' N9 L9 }8 G7 N" m EWPE Electronic Warfare Pre-Processing Element.1 w3 b! q2 V2 W) A3 f1 V, M EWR Early Warning Radar.9 [, R+ o. {4 R( N7 N0 d7 w EWS Early Warning System. 6 ~. |$ f) n# {" q8 g4 ~EXCEDE Electron Accelerator Experiment. + d3 \* y' i/ }! YExcimer A contraction for “excited dimer”; a type of lasant. A dimer is a molecule + l+ i; t% r, f3 x0 |consisting of two atoms. Some dimers (e.g., xenon chloride and krypton fluoride) % n& S. G0 Q7 Eare molecules, which cannot exist under ordinary conditions of approximate3 @0 a* R8 X1 a( a; X3 a: i" z thermal equilibrium but must be created in an “excited” (e.g., energized) condition ! R- E4 m0 U& ^& Lby special “pumping” processes in a laser. 3 f2 l8 O; [/ y2 `& H aExcimer Laser) w; z: ?7 B: D, I7 z% c, w (EXL) 1 ^; X2 x1 W7 }5 |- SA laser in which emission is stimulated when a gas is shocked with electrical 2 Z% y1 i. c* |) @ V% oenergy and the excited medium emits light when returning to a ground state. " v I, G3 U6 v. @7 u$ {, [MDA GLOSSARY, VER. 4.0 E ( i9 ^: ~+ r6 S' x5 ` b& b100 % U0 u$ A, `" e2 F& y7 j e: qEXCOM Executive Committee.) m/ N2 `8 g8 o Executable 6 b: F; j. s- W* g/ H" t$ GProgram- {" L$ ^& b( g) e, v7 z A program is executable if the PM has adequate near-term approved funding. 3 W: d4 e' D0 x. w* U. T, E2 w5 `Executing Agent The individual within the executing element assigned responsibility for managing- L8 J* D- A: Q' p& ] MDA funded programs. X& p0 u) d# b) B: ^Executing H) ]4 {9 m+ m* y/ g; c Elements / B& B' t7 s9 V( _$ I9 l- d3 [' ^+ Z2 VAgencies or organizations (DoD or non-DoD) that are managing BMD-related 7 ?9 F1 p/ a/ oprograms. 6 o" N8 M; d: ?# M$ eExecuting& ^0 ^1 d+ W, s Responsibility4 P5 P1 \+ F$ D) s8 y' n5 H' C Program Manager responsibility.3 O- g( j4 q q% P Exercise A military maneuver or simulated wartime operation involving planning, + F1 e9 n) ^# y( {preparation, and execution. It is carried out for the purpose of training and ) p: \6 ?( U" `3 r8 z2 F+ Kevaluation. It may be a combined, joint, or single-Service exercise, depending 4 w# d- E# D3 J) ^ a/ Con participating organizations. See also Command Post Exercise.- [; F- ?* {. _6 x4 A5 h. V Exit Criteria Program specific accomplishments that must be satisfactorily demonstrated, T5 H6 Y8 N, O$ w+ }& o3 R8 n before an effort or program can progress further in the current acquisition phase B, a' R4 m0 d6 Y- X$ E or transition to the next acquisition phase. Exit criteria may include such factors1 j. u! h" Y& c) w7 [ as critical test issues, the attainment of projected growth curves and baseline ! u. G1 S, y# q- y. r& Fparameters, and the results of risk reduction efforts deemed critical to the, o' R" t6 @( n decision to proceed further. Exit criteria supplement minimum required ; c% h$ p; U/ z2 i0 \2 P* Uaccomplishments and are specific to each acquisition phase. 4 E* E* i v! X! [3 oEXL Excimer Laser. 0 _6 l# k5 c. \& L5 ?Exoatmospheric Outside the Earth’s atmosphere; generally considered to be altitudes above 1008 u8 y; s5 {! r w+ W Y/ ~6 e km.- `1 `! d' x4 N6 T, W Exoatmospheric4 c% ~& B4 C5 Q( r+ [/ q. ^ Reentry Vehicle2 V1 c/ w) Y/ x" U7 i Interceptor1 F% R0 l) ~9 ? Subsystem # z1 I- Q6 c$ S! p! @( m5 P(ERIS) " I" u- e4 U& g8 J( V3 U9 s/ g$ aOBSOLETE. Interceptor designed to provide functional test validation of GBI.$ Y( X" l8 h9 W7 q Exoatmospheric 5 f; R) Q* m+ o& t. e5 B6 KTest Bed (XTB)( \. d0 Z6 K5 B6 E* _( h- R! B% ~- G2 Q Flight qualified and range integrated vehicle to support other programs such as - h# x/ D( v6 l: @8 K8 W5 bGBI-X.; E6 B x% M. Y! w7 a9 ~6 H( e& `/ c Exo Decoy A decoy that matches RV signature exoatmospherically. Exo decoys can use- Z! H6 P5 j' e6 ~2 | radar and/or optical means to deceive sensors. D8 J! u( |" b9 @4 C. rExpert Systems Software programs, which use artificial intelligence techniques to capture and " ~) M. S/ H% f: bapply the non-algorithmic knowledge and procedures of human experts.1 X. N8 x' b" K2 p5 |; e- f Expired# m' q4 [! q3 ~9 Z. E Appropriation 7 G: Y* C: W: R0 j/ T" B! |# V5 S! YAn appropriation that is no longer available for new obligation but is still available9 W+ |$ D4 I. j# J% {) }* o2 ? for disbursement to liquidate existing obligations. Under current legislation no! C* D! i+ o/ T/ d. @3 O disbursement may be recorded or paid after a five-year expiration period., C8 H& ^" T' j7 ` Maintains all original accounting identity, e.g. FY, appropriation, PE, etc. : N! F# o* t8 ^2 X9 p% i. x( bEXPLAN Exercise Plan. 5 U4 Y) G2 J! R2 d7 y7 EExplicit9 r. R# B) b; M( ~/ B Coordination 5 G3 v6 R: g9 ^7 rA battle management technique which communicates results, decisions or6 A* N O. j( [2 Q* s command from one battle manager to another, usually from a higher command - @2 i; j$ f; U! r: C hto a lower command. * v& p" P/ A2 ZMDA GLOSSARY, VER. 4.0 E * c" A: @0 S6 v2 F+ t) x101 0 a; `( v0 S+ s( V* ~0 `: {9 ?/ HExtended+ h8 D. |. ?9 m3 d Planning Annex) ^- M" H; Y6 _9 Q; {, T% e A document providing program guidance for an additional 10 years beyond the 2 ?. k0 k w; f6 ~ W+ wPOM. + f. h o( Q: [2 IMDA GLOSSARY, VER. 4.0 F 6 \3 V$ o6 Q7 i" Y( P5 ~1 \) ?103 $ s6 j' Z B# Y# bF (1) Fluoride. (2) Fahrenheit.: i8 T7 d! @" d! _5 W& B. q C F/O (1) Fiber Optic. (2) Follow-On. # x+ K1 f3 E- c5 @4 dFA (1) Field Artillery. (2) Feasibility Assessment.& ]) d' X& y a. S! q" U& i! v FA/RD Functional Analysis/Requirements Definition.$ T! K* W; F( f. _6 C# Z# C FAA Federal Aviation Administration.- u. S, k# K4 ?- l FAAD Forward Area Air Defense (US Army). 6 }4 T5 k. l% CFAAD C2I Forward Area Air Defense Command, Control and Intelligence. # M: M$ u- e$ DFAADS Forward Area Air Defense System (JCS term). 1 D' \# W" D% D u& EFAAWC Fleet/Force Anti-Air Warfare Commander., [1 k/ e& ^/ k5 A! v) a FAB Fly Along Probe.7 {8 [$ W6 c7 |" |* d' ]: {8 Z Fac Facility (MILCON term). 9 C& x6 s+ A; ^' T1 dFACP Forward Area Control Post (JFACC term)., n8 v# O. s! n8 E( | FACSPMF Federal Agency Computer Security Program Manager’s Forum.% [! ]+ i5 s9 B% {( N0 P; r D' r4 w FAD (1) Force Activity Designator. (2) Feasible Test Date.% w; W- ]3 e& S FADEC Full-Authority Electronic Controls. " T$ W8 f$ L' E! T3 O- g! fFAFB Falcon AFB, CO.; E: I+ k" J5 S" u- U FAFBR Falcon AFB Regulation! f7 z" [8 A6 }6 h Fairing Structure to protect the payload during ascent phase.8 y. l S% R/ O% M FAIT Fabrication Assembly, Inspection/Integration, and Test.: G9 a; Z- Y$ i" w/ m* k FALCON Fission-Activated Light Concept.% f3 M. ?' O5 w/ o& x FAM Functional Area Management.2 M+ K' p2 a4 r) D$ ?7 } FAMIS Financial Accounting Management Information System. ! W2 g1 R7 s( u* r9 |$ H$ q) q) b) fFAMP Facilities Acquisition Management Plan. / s3 w* j- R9 b/ ~2 X2 L5 iFAMSIM Family of Simulations (USA term). $ e5 U" R v6 h! \+ DFAR See Federal Acquisition Regulation.3 i5 r* Q4 D6 X i* J- j Far Field The region far from an antenna compared to the dimensions of the antenna and6 T2 L; b, V/ V, M the wavelength of the radiation.# Z/ Y+ j7 v) n" ~! T4 g" y9 W FAS (1) Fly Away Sensor (TCMP).+ y5 j2 Z n2 T a2 X3 S" x y( } (2) Federation of American Scientists. + o0 z/ w$ C) z* K# A% ^FAST Facility Allocation Study Team.1 c& Q$ V: P# f: ?& g4 r. l, p MDA GLOSSARY, VER. 4.0 F& S0 z8 p& W9 K3 L4 w. v+ e, t 104 & e: J& `: i8 f; M" ^* vFast-Burn & B& f r; {' JBooster (FBB) + G1 b% c5 _8 a# n9 s. K9 dA ballistic missile that burns out much more quickly than current versions,5 x& |& X9 R0 ~8 b& O' _ possibly before exiting the atmosphere entirely. Such rapid burnout complicates) M, f. }- q1 L' J# i+ u6 W a boost-phase defense. % d% q2 J+ [) Y8 HFAT (1) First Article Testing. (2) Factory Acceptance Test. 9 e$ |- I; t3 y* f) l! O7 f& g& ~Fault Tolerance The ability of a processor to maintain mission effectiveness after some6 u% C* ^2 k& r7 x4 {4 ]+ X# G subsystems failed. & T" D, ?. r$ t# O5 FFax Facsimile. " G6 g; X- l8 N2 ]3 r( xFBB Fast-Burn Booster.8 Y. i3 k" B1 y2 \ FBIS Foreign Broadcast Information Service (US).0 _! \. H% s+ N) C% r# J FBM Fleet Ballistic Missile.: e- _4 @6 @- o- s8 D; R FBMS Fleet Ballistic Missile System (USN term).) p$ D. q4 m/ D- i FBP Forward Based Probe./ w. B2 N7 n7 N# o7 [3 M FBR Forward-Based Radar (US Army term)." |1 S/ H+ z5 W' s: C FBS Forward-Based System. 5 l. b5 H c+ n% \FBXR Forward-Based X-band Radar. . y; B6 r) g' H& v9 E' I6 W( r5 gFC (1) Fire Control [of weapons].3 Z) R4 h7 X H (2) Fund Code.: N$ K- h' V0 L% ] FCA Functional Configuration Audit.. U5 a! U, k. a" X7 s) k FCC Federal Communications Commission. - c! `6 m; R8 _, C0 ?! q5 L' bFCCM Facilities Capital Cost of Money.6 ~( \' \4 i9 t% _# k2 m9 I* n FCN Fully Connected Network.2 G! P8 i) n6 h4 |. y/ P2 E: y/ } FCO Field Change Order. 1 H# O- A- P, fFCRC OBSOLETE. Federal Contract Research Center. + N6 F$ p8 \% m R8 N( XFCS Fire Control Section.

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FCT Foreign comparative testing. % E9 q. ?5 v% Z* d7 m' `, ?FD First Deployment.$ x) q1 l2 E% l6 L; q3 u# K8 z) W FDA Food and Drug Administration. ' ^2 N% T2 e# ~9 ]FDC Fire [of weapons] Direction Center.: e9 B1 p: n/ b5 F1 r$ Z# t FDG Foreign Disclosure Guide.) L( z! X A1 v r7 n FDM Function Description Manual.. v( o2 G6 g. a8 L( F FDO Fee Determining Official. ; J9 l; w6 N3 I3 hMDA GLOSSARY, VER. 4.0 F ( L$ j* ^# z4 \" P) t' Y105 . Z K3 f1 ^; p! Q$ ?6 WFDP Flight Demonstration Program.) R$ A9 X! N/ o& m* D' ^8 X/ Q* p, R FDR Final/Formal Design Review. 6 }: S M# E/ `FDRU Final Design Review Update (MDA PAC term).- F! e4 J3 c# d; R# Z: j: S6 Y- I2 d FDS (1) Flight Demonstration System. (2) Fault Detection System. 8 ~ y$ _2 D5 Y6 U, G1 T8 wFDSV Flight Demonstration Space Vehicle.; M6 [3 F/ ~( X4 e- G FDT&E See Force Development Test and Experimentation (US Army). " y' G; s% J- I5 b. RFDX Full Duplex (Telecomm/Computer term)., p# U' C# F2 f FEA Functional Economic Analysis.7 ~5 g( `3 D+ \8 _7 }. r Feasibility Study A study of the applicability or desirability of any management or procedural 6 Y! w- |, O$ |% Lsystem from the standpoint of advantages versus disadvantages in any given; f! ]+ V i* b9 H# H% Z case. 4 L' K) t% q! U- M9 ]) EFEBA Forward Edge of the Battle Area.2 z4 a; E. }' q; C& ^ FECA Front-End Cost Analysis % Q: c( Q" t3 ~) sFED Federal. 1 n/ q: Z( t3 \# kFEDAC Federal Computer Acquisition Center. # `- O& c* ]5 W2 j1 [- i, U' O/ AFederal 9 J5 u" b" T% UAcquisition / i) J4 d# w m* S( ], BRegulation6 H3 n: j2 N% s- C$ R The primary regulation for use by federal executive agencies for acquisition of ! C/ m: u, R, Zsupplies and services with appropriated funds. It directs the defense program ! U _" H; Z7 y+ t- nmanager in many ways, including contract award procedures, acquisition # u# P1 K @! y+ d$ S7 z% K; gplanning, warranties, and establishing guidelines for competition. The Military; N4 v" C$ h& d2 ]# u Departments and DoD issue supplements to the FAR. The DoD supplement is % i* x2 e" t# K! Y1 n4 X# D! S1 mcalled DFARS (Defense FAR Supplement).( Z3 G( F( V8 x) V) [ FEDSIM Federal System Integration and Management.: A; C1 w. ?, g9 G1 r FEL Free Electron Laser. ) b u5 X* {3 i, v- L/ y3 \. k( V% |FEMA Federal Emergency Management Agency." z+ Z5 p. l0 h. [. { Fenced Funding An identified aggregation of resources reviewed, approved, and managed as a8 j2 p" e, {8 m! O distinct entity. The proposed program must be implemented within specified 0 I3 Z- a9 @" }/ Z5 x& Qresources. Examples of fences areas are: Intelligence and Security, Support to / a/ T# `/ Z& q- | N' [Other Nations., |7 [# D' i- L; x% T0 C) h% p1 f FER Financial Execution Review. ( C/ g& _* c" D+ c8 R9 M2 cFES Facility Engineering Surveillance Plan.) E3 K% c- B1 b+ E1 K( g FET Field Effect Transistor. " Q, B- @! }6 f) q; u7 a* ?+ GFEU Flight Evaluation Unit. 2 I- \: E& X B: wFEWS Follow-on Early Warning System. ' ]4 Y" o; ?9 ~, {FF Fire Finder Radar (US Army. 4 q) J6 U V" r6 f( YMDA GLOSSARY, VER. 4.0 F ; e/ |8 Q& i6 ^+ y2 l. N, F106 A2 J+ E4 n0 q0 v: f6 A FFBD Functional Flow Block Diagram., J! v& v9 b- q/ Y, r2 r FFCD Full, Final and Complete Disclosure (Treaty negotiation term).) I) V( D' Y, u2 ~& \" ]- S FFD Fraction Failure Detected. : l Q6 F1 \: x" A6 R( m) uFFH Fast Frequency Hopping." T# k3 Q, {0 |. f v1 t9 q4 Q FFP Firm Fixed Price.8 M, Y/ G2 R8 d# G FFRDC Federally Funded Research and Development Center. 2 m, I4 ?1 y/ { i5 Q. jFGC Functional Group Code (Navy ILS term).1 L4 T4 H$ l$ {3 k FGEP Fixed Ground Entry Point. + r8 ^( a$ G) c+ h, k+ y5 ^4 h5 |FH Flight Hours.; m2 X! Q- C' ^6 [4 v FI Fault Isolation. 5 n5 r+ `" ]5 \FI&A Fault Isolation and Analysis.4 k6 Y3 l' k \" i3 k FIDO Fighter Duty Officer (JFACC term). " p, F3 B5 |/ m+ q% m$ B/ CField of View! C* m% `: @: x) O! q+ e (FOV)( r1 G# j J0 J+ z( z# e The angular measure of the volume of space within which the system can 9 z: s5 A7 i2 m( x" l1 i' Z. yrespond to the presence of a target.# y; J+ T/ Y! U' M Fighting Mirror' m# {) ]# a2 Q$ ^& L. r$ x (FMIR): t5 J' p$ S/ C- Y% \( K Part of the GBL System. The low orbit mirror, which receives laser energy and- `6 `+ y- v: M/ g3 P! b2 w reflects it to the target. 8 c% z0 t- J. W5 I( iFigure of Merit / @# v. P; ], ^ i, t(FOM) * t+ ]- }8 f0 Z- e8 \$ EThe numerical value assigned to a measure of effectiveness, parameters, or" R# d, Y9 n" f6 z5 ^5 Z3 V3 ^ other figure, as a result of an analysis, synthesis, or estimating technique. 3 `% @7 X" P+ c& B& x$ OFIP Federal Information Processing. & Q2 S8 r2 B/ Q. f; ^8 BFIPS Federal Information Processing Standard.: T* o$ T1 m6 U: [ Fire Control The control of all operations in connection with the application of fire on a target.& j3 l: C+ t& k4 I/ { Fire Control" N M y5 ]9 ^' _; s- p System 3 m% I# H' Q/ l" QA group of interrelated fire control equipment and/or instruments designed for% H) \# Q- Y M( ?; e- H use with a weapon or group of weapons. + e6 J# M6 v% G7 k8 c; Y. qFire Support % W# w: k5 ^, N! LCoordinating 9 Y% ^. I2 }' |- M9 QMeasure 9 j6 ~1 P- U& {& a$ h( XA measure employed by land or amphibious commanders to facilitate the rapid % j) H8 x" h* g* [4 ?' }6 Dengagement of targets and simultaneously safeguard friendly forces. 1 O- @ }3 I6 |5 Z4 Q: rFire Support 9 T. Z6 V1 K3 O; l$ nCoordinating Line) |, q% K Z4 F! y; V6 r (FSCL) 2 o- I/ _2 J, a4 ?1 SA line established by the appropriate ground commander to ensure the 5 |6 r& P- }! F7 a) z) q! k1 Jcoordination of fire not under the commander’s control but may affect current 3 w8 O8 R P! {) `- F. ytactical operations. The fire support coordination line is used to coordinate fires% }6 Z9 u x( n# B- v; z+ F6 F of air, ground, or sea weapons systems using any type of ammunition against g' K9 l" q! z# \9 K surface targets. The fire support coordination line should follow well-defined6 n' D2 \0 v4 S terrain features. The establishment of the FSCL must be coordinated with the / z2 S4 J2 e" a" |" i) r. d/ P. \9 ~. qappropriate tactical air commander and other supporting elements of the FSCL & X4 L. h% w: } K' S9 kwithout prior coordination with the ground force commander provided the attack) J/ F) k: u, U' x$ L will not product adverse effects on or to the rear of the line. Attacks against , Y, j- s4 l5 c8 \( z( I9 p+ ^surface targets behind this line must be coordinated with the appropriate ground ; x/ w) O+ Q# ^( R' Jforce commander. 9 N' Q+ H8 I- GMDA GLOSSARY, VER. 4.0 F! i) r4 f7 P. S. d# G$ @ 107& E* G9 w( O; Y8 O5 C G) m+ L0 G Firing Doctrine The ratio and manner of assigning numbers of interceptors against given- q4 r. v4 G" L" Z# P4 P& M3 } P attackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are( E5 K. Y# ]$ A4 r8 ]/ y# u examples of different firing doctrine. The priority of targets being defended and7 r4 i5 G/ f. P/ V- `% v m; v the number of interceptors available relative to the number of attackers drive + d; H: `4 L4 ?: V- t8 Ndoctrine.- w7 l7 X1 ?8 g5 ]4 G7 \ Firing Rate The number of missiles fired per site per minute.; K0 f: ]; z. ^8 C, x FIRMR Federal Information Resources Management Regulation. ' p$ `" X5 {' c& Z) W! ^, Q) VFIRST Forum of Incident Response and Security Teams.* |. A* P3 g" }9 f. { First Article First article includes pre-production models, initial production samples, test1 o R( J' ?( n2 y5 d samples, first lots, pilot models, and pilot lots. Approval involves testing and4 r# {( ~6 R" s! Q# S9 e evaluating the first article for conformance with specified contract requirements ( _# e5 ?0 t& F$ f7 e4 kbefore or in the initial stage of production under a contract. / b* i3 y U( x; L% j6 O* YFirst Strike The first offensive action of a war (generally associated with nuclear operations).9 @: A0 ^7 a2 t+ E/ j4 b* p First Unit 5 e, w- f7 n6 v( x+ J/ UEquipped Date' o: D% t( }9 ?# Y6 Q' {9 B The scheduled date an end item and its support elements are issued to the 5 c! a/ c1 b( q& R* Z' \3 H( |& x4 linitial operational capability unit and training in the new equipment training plan ) j. W8 m9 a% m! @2 O3 yhas been accomplished.* b# ^- A5 A$ h1 h9 E2 W FIS Facility Installation Standard.+ a$ y, U! e4 h Fiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which . m# \- A; o$ ~% l: I% E% Jprovides the fiscal constraints that must be observed by the DoD Components in# U! p; T+ m& @2 o9 E( F the formulation of force structures and the FYDP, and by the OSD in reviewing ; t' C. i9 ]9 U0 J8 A7 J2 Pproposed programs. 7 k Y7 B; ~1 d! u. y mFISSP Federal Information System Support Program.- K9 }% o* c6 t FIWC Fleet Information Warfare Center (USN term)." ]1 N$ m! e) ~5 e FIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern % a" q2 Q7 e. OExtension).% H6 ?3 v F# a7 `/ b% j' j6 { Fixed Costs Costs that do not vary with the volume of business, such as property taxes,8 K1 T' e$ G3 J( O5 i# Y5 y insurance, depreciation, security, and minimum water and utility fees.' y+ W! N2 D8 ]- H& j Fixed Ground 4 P% o2 g% B4 M8 |) w$ i; S2 Z' IEntry Point. v8 s0 |$ B1 m1 t) w. z5 A* E* N4 v (FGEP) : }' G5 B9 t5 c( O: G, b( a1 B8 SThe subset of GEPs, which are not transportable. GEPs provide the ( i6 R% c& [1 vcommunications interfaces between the SDS space orbital/sub-orbital elements! q1 R6 q0 @/ k/ k+ n+ C and the C2E.4 Q7 _, ~4 `( A6 F0 R; r Fixed Ground 0 A5 u3 k. \+ d: S9 f( h; eStation4 L3 ^/ _ m7 \" l4 L, d( y All hardware, software, and facilities located at a fixed ground site necessary to3 c- E, A; ?; N receive, process, support, and analyze mission status and data, and disseminate 9 l( ~& [8 n5 n8 M& b ^3 [operational messages.- x# w r0 S, O" f% }8 | FLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor, z: y0 {% T# B0 D program to Extended Range Interceptor (ERINT).) + P2 x- N# @* m: p# KFLC Federal Laboratory Consortium. . F3 U& f. O2 `& I8 iMDA GLOSSARY, VER. 4.0 F . \; s4 D) Z. |, [+ C108 ; j0 F4 z/ {$ F$ N( YFleet Satellite 6 \3 t) k7 s4 g2 Z O0 ICommunications9 Z( W q( _6 @, V9 J! w4 ]5 ^ System : \ F5 _' s6 E% p(FLTSATCOM) 4 o; \" p2 D+ O! d) F3 r; TOperating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost / |/ B% C, n9 c7 mterminals with simple antennas for use on highly mobile platforms. It has a ) o+ A: Y) U. _' ]relatively small capacity because of its much lower operating frequency. It $ a" b9 F$ n2 c! z8 b: }/ wprovides a satellite communication system for high-priority communication! S1 Y$ A7 _8 P+ M requirements for the Navy and Air Force that encompasses almost the entire 0 V3 O4 I' ~) F. l6 T% l/ z8 G' [world. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF 7 Z" X) V' O4 I& z! eand SHF bands. The Navy has exclusive use of 10 channels for communication + f& }/ x7 H A4 Q- o2 Swith its land, sea, and air forces. The Air Force uses 12 others as part of its ( D) Q) x8 q# h* v: H: IAFSATCOM system for command and control of nuclear capable forces. The) L- L& ^( ]1 ~6 y system has one 500 KHz channel allotted to the national command authorities.8 z: d& N ]( n W% _4 Y Flexible 5 H% S. }" }/ @3 h. YResponse* S( t0 `0 H1 T `( _ The capability of military forces for effective reaction to any enemy threat or 5 i6 b4 x. s. b& ^% Z% Z" @% U% hattack with actions appropriate and adaptable to the circumstances existing.% I9 d- l1 X: Q, V FLHER Funds and Labor Hours Expenditure Report.+ R: Q3 h2 a1 U- y Flight, e2 g* ^' x2 h8 P4 [" V$ \3 O Demonstration 2 g9 i/ s ]( N$ G7 TSystem (FDS) $ Y- e; t( l- r; K6 `0 b4 k( _Part of the SBIRS Low Program Definition and Risk Reduction (PDRR) program! s1 L5 e, z& H, x6 c, m phase. The FDS will consist of two satellites and a ground system being built by$ R8 D% Z+ C! T; k0 ~/ r3 _* S TRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test9 t- } R0 j8 M& @( F/ m8 W program to demonstrate operations and performance of a SBIRS Low concept,1 m( _# F+ \2 `! l7 R( U- a collect target and phenomenology data to support the objective system design,. q% L, A9 E6 K) y. b% e- q and validate cost estimating models.% X% `5 l) f! ? w Flight Path The line connecting the successive positions occupied, or to be occupied, by an5 m5 l y( k6 T aircraft, missile, or space vehicle as it moves through air or space. (It is more 1 u1 A/ s8 C/ b. |commonly referred to as trajectory for space vehicles, especially ICBMs.), ^, s; L" M) r G1 @4 d/ { Flight Readiness/ o7 s! |" s) f+ s. T8 t Firing / i& T3 E; G& \2 K/ N. `9 A) _, mA missile system test of short duration conducted with the propulsion system ; ~ J: I- v( N1 R3 e' ^operating while the missile is secured to the launcher. Such a test is performed5 V, @2 s9 [% I i6 j to determine the readiness of the missile system and launch facilities prior to s# D) N5 J# {* _ flight test. - \- }9 Y H9 s! P9 E6 `5 lFlight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching.3 I3 d7 f9 J$ |+ O0 t Flight tests are planned to achieve specific test objectives and gain operational3 G a0 c8 Y4 j' D! h8 F! @- D information. % u7 ~6 h( F x/ m/ _4 r+ xFlight Test) B A9 @. V- V; s Vehicle (FTV) $ ?& T$ h4 x$ q- N% \Prototype of airborne or spaceborne hardware used to validate a technology q+ K* A8 w' h* {+ oconcept.

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FLIR Forward Looking Infrared Radar. # {3 }* F4 t" Y5 _" HFLOT Forward Line of Own Troops. Z F3 \2 L8 l FLT Flight. 8 U. y1 v, N7 u+ n% i r1 P' ZFLTSATCOM Fleet Satellite Communications System.5 v Y0 \( v. I# Z* p Fluence (or , N7 J; i+ h+ X- b3 F$ {5 ]2 hIntegrated Flux) 9 ]' b E6 B1 N2 SThe product (or integral) of particle (neutron or photon) flux and time, expressed u, x0 ~; q T0 ^2 v5 T0 Kin units of particles per square centimeter. The absorbed dose of radiation (in L- w, @( {' Z8 ?6 ]rads) is related to the fluence. (It should be specified whether this is incident or 7 ~/ V1 M* m5 m, \' Dabsorbed fluence).8 s! V' A1 U8 V6 Z) O MDA GLOSSARY, VER. 4.0 F . O- m# O3 q& A# m0 q" r/ J: j1096 u9 R; n; B' }" B! E% g Flyaway Cost The total cost related to the production of a usable end item of military hardware.- C8 R3 f1 W* r- k% ? Flyaway cost includes the cost of procuring the basic unit (airframe, hull, chassis, 2 w9 R0 g$ P2 h7 y# o: p# A* x/ Fetc.), a percentage of basic unit cost for changes allowance, propulsion % o2 G/ A% y0 o2 w, }4 }4 R; lequipment, electronics, armament, and other installed government-furnished" l' h- O9 _; i E0 h: w! ?: M equipment, and nonrecurring production costs. Flyaway cost equates to6 S( ?8 e9 j7 B0 ^0 a Rollaway and Sailaway cost.5 Z7 d$ w& n* j# o) o FM (1) Flare Multiunit. ) o: H; A% D& W& T$ j. _(2) Frequency Modulation. % G& ]8 P' i- C( h. j7 e4 `(3) Functional Manger. & o0 f$ }$ h4 _' B(4) Force Module(s). $ |; O/ B3 P- T3 x0 a( i$ B3 g(5) Field Manual.; _1 e; }2 @3 n" K! q2 V" { FMA Foreign Military Acquisition./ n+ M: C/ P4 X FMB Financial Management Board. ( U( v. X/ K7 B! E# h$ N. @6 CFMC Flexible Manufacturing Cell./ x* m% l* `+ j4 O P FMEA Failure Modes Effects Analysis (ILS term).$ D7 |: G& u7 @, x1 M FMECA Failure Modes Effects and Criticality Analysis (ILS term). 2 C' a. k( J1 W4 L; d1 ?( ]FMIR Fighting Mirror. 7 K, C7 w) k, ~1 _, n9 SFMP Foreign Materiel Program. ; P" w6 ^( _, _! L, ZFMS (1) Flight Mission Simulator (PATRIOT), Huntsville AL. 7 R' E7 {& D3 q5 Z9 z(2) Foreign Military Sales.( y) I y/ N9 ~6 C( q) s FMTV Family of Medium Tactical Vehicles (USA term). ! a! s9 H! g7 _6 [6 G2 K) r% D* Z. sFNC Federal Network Council3 c( t2 I( c s- o% D FO Force Operations (PATRIOT).5 H% i1 d( }+ K z6 {/ ~ FO Link Fiber Optic Link.& H f3 Z2 k3 k- \5 K3 k2 _ FOA Future Offensive Aircraft (UK RAF term).0 [' l r8 f6 p6 ~ FOB Forward Operations Base.$ c. j6 \4 j( m5 P4 N% u FOBS Fractional-Orbital Bombardment System.8 L: y5 y2 D7 R9 @8 ~ FOC Full Operational Capability.3 n# h+ N# i. x* I' H Focal Plane The plane, perpendicular to the optical axis of the lens, in which images of points6 r: F# o& b7 Q7 L5 V in the object field of the lens are focused.* ~ ^( V5 v E9 q+ ?. l u Focal Plane - a7 ^7 Z# c g4 u: ?8 b" HArray (FPA) + \# Y6 F" Z1 c) WAn FPA is a matrix of photon sensitive detectors which, when combined with low# J; |& @' F+ {' `; T0 \ noise preamplifiers, provides image data for the signal frequencies of interest. . \# c/ t6 b4 Z! }7 t x1 sFOFA Follow-On Force Attack.: ~/ a" s& s' a+ l FOG Fiber-Optic Gyroscope. ' p5 {- z& `/ `+ kFOIA Freedom of Information Act (US).! _ q* P9 G1 U( H8 G MDA GLOSSARY, VER. 4.0 F4 O( U: J9 G/ W9 F7 k. X7 E 110$ m( }, ^% }4 {. ?3 h FOL Forward Operating Location." A" q9 u( l1 t3 `0 Y; [ FOLAN Fiber Optic Local Area Network. 9 z& E7 h& r$ b3 P1 V3 gFolded Optics Any optical system containing reflecting components for the purpose of reducing! v4 E3 I7 a' l' V0 x% \; R the physical length of the system or for the purpose of changing the path of the2 P8 e* ~% E2 i" B% p b$ t. k+ G optical axis." s# U. N3 i: S4 a" l Follow-On+ [6 J) i, p7 { Operational Test" b$ c; ~' b( }8 g: Y$ q1 p and Evaluation 7 [8 X6 }* e0 s( \: w7 ?(FOT&E)4 J+ V- s, M( C% w8 Y That test and evaluation that is necessary during and after the production period& Q) \9 \! v- l* }6 ^& f7 e" k to refine the estimates made during operational test and evaluation, to evaluate ( `* q; b3 d/ Mchanges, and to reevaluate the system to ensure that it continues to meet 0 {* g5 i' m8 p4 Z' J* D( M: ~* Aoperational needs and retains its effectiveness in a new environment or against - }1 G5 X a" O" u! M0 S0 w9 ~% Aa new threat.' s9 J) j/ V" R/ B; Y; R1 W FOM Figure of Merit.& d0 a# ~! \+ F: e1 w FON Fiber Optic Network. 1 v" _9 J7 D3 c; T7 ^6 L7 xFootprint (1) An estimated area of possible reentry or the solid angle of a detector or3 R- g+ S7 J9 h3 h3 K. c) f linear area of a detector at a certain location. * q" B3 W# W+ L0 O(2) Geographic area in which a focused satellite downlink can be received.+ j; f* x. n* s# @8 k FOR Field of Regard. . [; L! X6 e$ _; j: O9 k) eForce Closure The point in time when a supported commander determines that sufficient 3 n# M) [, |8 n( P1 q6 opersonnel and equipment are in the assigned area of operations to carry out9 e w0 J! r* Y6 _1 _: ~ assigned tasks.: f, q# M8 L2 }9 Q2 O8 } Force Development Test and 5 S1 k2 R8 c' U \# R. X( yExperimentation) T5 a; G9 n' T& D* g2 X Tests employing representative users to examine definition of materiel # ~* o+ S. d" b' V8 j: Drequirements or support/assess development of doctrine, training, organization,, k. p8 A0 T8 i! r; ]1 N( k and logistics for system acquisition. (U.S. Army).9 M! m8 D1 g1 U3 r7 Q8 u& _ Force Direction The operational management of the forces. # S7 o- D7 O$ d- E) t; wForce Integration( i; I4 M' g& H# v4 u) e# T Staff Officer8 M5 I: ?: v D, K" x: u8 ` Army individual assigned to ODCSOPS to serve as HQDA user representative for1 j5 ?- V2 O- Q) y. ]* _ a specific system. Provides continuous coordination necessary for integration of - _% a& @9 K3 ?4 R# ^a new system into the Army force structure. 3 O" f! I* z0 I( w6 W: EForce( W8 d6 w3 \- b9 G6 W$ T8 ^ Management 4 S* _0 _' u( EThe assessment of the effectiveness of the defense forces throughout an ( i$ Y4 r' {7 }0 E4 i- l3 Cengagement and adjustment of tactics and the system configuration as $ X; f4 Y# i! F" Y9 M" w0 fnecessary to effectively allocate resources to satisfy mission objectives.4 k M+ k* \" B( W! Y Force Reliability The percentage of the missile force that will successfully detonate within 3.5 $ B. q) k: |' [6 w p" U$ VCEPs of the target. : G" n9 C" Q, h* ^) ?. @+ F- e NFORDTIS Foreign Disclosure Technical Information System.3 W! P, |0 i5 e3 p p8 c4 { Foreign ' N8 Z+ J& k- `2 X! C( n* d: [Government3 V, S0 G& u$ _% A- ?+ t( @# J Information / t4 z T5 G) n! J6 G' y$ B% r! RInformation that is (1) provided to the United States by a foreign government or8 M& X4 t4 Q1 p" p$ P; t governments, an internal organization of governments, or any element thereof , z* ~" N3 B( w# Nwith the expectation, expressed or implied, that the information, the source of / R6 F; l1 U" E! r, D9 V+ \' Zthe information, or both, are to be held in confidence; (2) produced by the United$ U9 ?9 Z& Y5 i& Y7 ^ States pursuant to or as a result of a joint arrangement with a foreign4 ?/ X8 `/ Z9 Q5 M( I1 P+ F government or governments or international organization of governments . X3 {' B! M7 v6 w$ p ^requiring that the information, the arrangement, or both, are to be held in, ]' i& s+ E! x6 S5 M' s# Q% Q, I& p confidence.6 E; z+ l* z9 F6 z! ]6 O MDA GLOSSARY, VER. 4.0 F( p- d# x6 f# K) H 111 $ m' F: ]/ X/ w9 }Foreign Military2 z, d, ~) @- G: Z Sales (FMS)& A8 Y. n# M4 J& ` That portion of U.S. security assistance authorized by the Foreign Assistance Act/ ? c# ]# U; A1 f& J of 1961, as amended, and the Arms Export Control Act, as amended. The: v+ [0 F) _/ p) Q& r recipient provides reimbursement for defense articles and services transferred: Z' E9 L( y+ r# @ from the U.S. Includes case sales from stocks (inventories, services, training) by5 ?) i( C8 P2 d the DoD defense services.1 G1 [. ~, o- A5 K G Foreign Security3 x; v/ h) O2 a' L, h+ p Policy Model ; z1 q& \! i8 S' ]) f9 z/ vA mathematically precise statement of a security policy. To be adequately 6 p/ V5 v. s$ Y) i qprecise, such a model must represent the initial state of a system, the way in- t0 M7 H- e# c; M( m. { which the system progresses from one state to another, and a definition of a 6 o' @+ X- a2 N“secure” state of the system. , L, n6 G) f% c; O4 l) Z' j1 W* c% zForm, Fit, and 8 Q1 C2 }% L0 ^/ d2 L; `Function Data' F i2 l7 m% L+ L" o9 l Technical data pertaining to items, components or processes for the purpose of " B) o0 a* N" f# Bidentifying source, size, configuration, mating and attachment characteristics, 1 Z, S3 p1 x y! Nfunctional characteristics and performance requirements.3 X# P/ T/ S# ]' C2 H4 Q& j Formal! S6 i" i& r& O$ O" m2 { Qualification4 N3 v/ ] S. u( o/ k* N Review) C3 m$ F- A$ i A systems level configuration audit conducted after system testing is completed . f5 P) J4 \2 Q7 e6 Lto ensure that performance requirements have been met.9 @6 ?6 L" K! K( k: ^) @" U Formerly. D, W+ W9 w3 U Restricted Data / ?) c6 X. @+ q5 F# `Information removed from the RESTRICTED DATA category upon joint9 M# Q! q7 o. t/ \) J determination by DoE (or antecedent agencies) and DoD that such information& U8 q1 b0 I J- S- p relates primarily to the military utilization of atomic weapons and that such9 b0 B5 ]. G1 h; Y information can be adequately safeguarded as classified defense information. ; e/ `4 f( Y. |% y3 h8 l7 ]FORSCOM U.S. Army Forces Command, Ft. McPherson, GA. . j- g4 @5 [1 f" K9 s/ S4 rFORTRAN Formula Translation Language.

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发表于 2008-12-25 20:06:48 |只看该作者
Forward Edge of 3 m! H* ~- S+ E8 m: i" y1 G* K' Cthe Battle Area . b9 S; C& U# z2 h9 R) T5 \(FEBA)% A* x) W; r: }+ w$ u The foremost limits of a series of areas in which ground combat units are3 R) C% C3 v% v. z5 ? deployed, excluding the areas in which the covering or screening forces are * v& `2 t& T4 R" L8 K j2 G3 T$ l {# Ooperating, designated to coordinate fire support, the positioning of forces, or the , y1 ~5 _9 b$ F; X3 x9 fmaneuver of units.: L1 f# c7 t. B. I Forward Funding Carry-over of RDT&E funding into second year of appropriations availability. 0 g2 C7 P4 G5 H8 B1 `4 LRequires permission from high authority.# t3 z4 x+ V6 v. [+ x- E2 ?* ] FOS Family of Systems (TMD). 6 h& a' [( c* E% `! B: nFOSS Fiber-Optic Sensor System. 3 }. d# M8 @" b" v" m" x, XFOT Follow-On Technologies. % j) e4 a- v9 _4 O! PFOT&E Follow-On Test & Evaluation.. P: Q3 {6 D4 u0 Z& L FOTC Force Over-the-horizon Track Coordinator (USN term). 8 c. \+ z8 R1 d5 x1 [# c/ }- [7 PFOUO For Official Use Only.& w; T x0 x2 Y" I Fourth8 x! d- t6 Z/ H, ]: T2 Z" w- { Generation : _; _5 \6 ^0 {$ E3 I4 [' u8 [Language - H% \2 B! ~( i; N* O D8 \A programming environment that produces both screen and report utilities for 4 L' S0 s+ P$ n% x0 a" Fuse by lower-level programming environments.1 z. y& L1 S r9 W0 q' Z! ?) o FOV Field of View.* g7 ~# P( \* r' v. B% O% F# v FOV Radar [Full] Field of View Radar * O* W( N9 ?3 W) ^, BFP Focal Plane.# M6 Z/ k5 u5 e& c; v MDA GLOSSARY, VER. 4.0 F ! B6 q: ?- M" n2 t+ P9 {. w6 M112 2 W& _0 w! F5 \! bFPA Focal Plane Array.' w4 g( w A+ l& @ FPC Facilities Protection Committee. ; T2 R! D- M3 d6 |# x7 V; AFPI Fixed Price Incentive. 5 v" N7 t- V4 S. l& BFPS Fixed Radar. # m P. T2 Q- K9 sFPTOC Force Projection Tactical Operations Center (USA term). ) T" Z" L/ ~" |FQR Formal Qualification Review.1 B0 z8 e2 V8 s( k4 ~; o! w0 z. s FQT Formal Qualification Testing.3 p! `4 \4 x* _0 w. R FR (1) Federal Register. (2) France.1 r9 [4 }1 ^# F7 G) s$ J FRACAS Forward Reaction Altitude Control System. " D- N" N( O; |7 }" y: v5 sFRACS Forward Reaction Altitude Control System. 3 ?& v. P% G' L, b0 K2 A0 d* L- pFragmentation8 b+ Z# C0 v, L Warhead 5 `2 G# H& f, h7 O f5 |" WA warhead, which releases small solid objects to damage or destroy its targets. ; c/ x) t( Q+ Y- I2 S/ u8 n) J& X) lFRAS Free Rocket Anti-Submarine. 5 H+ Y" P9 r+ b9 C: C2 R2 `FRC Fire Control Radar. \0 H# n* N; c9 K/ n) [ FRD Facilities Requirements Document.( i$ V k$ g3 S9 n+ W Free Electron & f8 h% W( L2 U( f7 E7 C7 ULaser (FEL)+ P! s( J' t% C$ _+ |% B4 }8 \ A type of laser, which generates radiation by the interaction of an electron beam 0 u/ u+ i2 c R9 U- c, Uwith a static magnetic or electric field. Loosely speaking, free-electron laser2 s/ ~7 U+ _/ E1 Y technology resembles and evolved from that used by particle accelerators (“atom % \+ x& k2 C: P$ Osmashers”). Lasers, which are not free electron lasers, are bound electron- Z, d0 g: L' O# Z lasers. # J: e% ]/ ?0 [1 M: z! IFree Rocket A rocket not subject to guidance or control in flight.$ J( h8 h# E( F7 c Frequency! k$ V) a8 ]6 h8 _, }. Q U Management : Z' c1 M: d* w, jThe act of allocating frequencies, or bandwidths to a telecommunications ( C% Y; V) u4 f- s, q6 asystem, necessary to minimize the potential interference between/ _) j9 j7 i+ j% P& A/ a1 P3 L- s# ? transmitting/receiving devices. Governing agencies and international agreement & P7 I3 O1 x% `% s1 Vcontrols authorized use of a particular frequency, frequencies, or bands. 5 M& X+ K# Q P9 t% `6 ^7 qFRG Federal Republic of Germany.; s1 M. K8 e% x# G9 V) F FRN Force Requirement Number. ! X2 P; [7 O/ G6 Q8 @FROD Functionally Related Observable Differences. ( N( v5 }; B5 v5 jFROG Free Rocket Over Ground. % c7 w" _0 d6 P6 J' [6 vFRN Force Requirement Number. ( p6 E; ^) e: M' Z, w; \FRP Full-Rate Production.' O. I. B i+ ]% I7 q5 Q- k+ i6 @ FRS Federal Reserve System. / S/ C& n7 K8 y X9 ]; IFS&E Facility Siting and Environment (MILCON term)., ~% S5 h$ T! `' t& e7 }: Y MDA GLOSSARY, VER. 4.0 F( W! h& K. {' t1 h m 113 4 m; h h7 r* [4 D {FS3 Future Strategic Strategy Study. ! I8 |+ [6 N) _ ^6 G/ C0 TFSAF Future Surface-to-Air [Missile] Family.' I" M) W; A$ |, Z0 C FSC (1) Fire Solution Computer. (2) Fire Support Coordination./ s2 N R/ b: d! ^" w FSCATT Fire Support CATT [for Weapons] (US Army term).5 c% ~; B5 D4 C+ E v1 h FSCL Fire Support Coordination Line. ) _- ~/ G8 i$ ]+ { F* y. w4 gFSD OBSOLETE. Full Scale Development Phase. See EMD. 8 h+ {$ V9 m- V _' S( s3 QFSE Fire Support Element. 7 \0 Z- I' p( n& q. v' z7 A3 bFSM Firmware Support Manual. : ?7 a& t) M. E6 A0 l' oFSP Facility Security Plan. j; \" u' A$ u; { CFSS Fixed Satellite Service.- U* B& ?, L- r: h h FSST Forward Space Support in-Theater. 9 a, N A& w6 b( ~7 T0 q# |FST Flight System Testbed. # d8 ?4 a* B9 E" t: q, `$ v' tFSU Former Soviet Union. , Y1 R' V( c, F5 V% g, |9 KFSU Republics Former Soviet Union Republics. J, {. A& G/ JFT Flight Test. $ L' `% h! O( I9 H fFt Foot - M" \3 I, l5 @& p' t* _% }3 A: RFTC Federal Trade Commission. / U2 F; G. S2 u7 LFTD OBSOLETE. Foreign Technology Division (USAF), Wright-Patterson AFB, OH.+ k) z0 v, `, A3 K3 b1 ? See NAIC. ( X) G/ O! m" [" YFTI Fixed Target Indicator1 C& X6 J/ L; n8 m8 m2 Z7 z FTLS Formal Top-Level Specification." c5 p y4 q0 O7 K, w0 n! ?. s FTP File Transfer Protocol (ADP/Internet term). ( _6 {% B' V4 E9 G# @: s! _FTR Flight Test Round. 9 _# Y- `# ?* r1 Y. b4 h. R8 V: w6 NFTS (1) Flight Test Summary (2) Federal Telephone Service 8 c, `" y( F' QFTS 2000 Federal Telecommunications System 2000. 1 a8 I) z: `8 c/ G8 K& n) uFTV (1) Functional Technology Validation. (2) Flight Test Vehicle. : V8 U3 R8 n" d0 {$ WFTX Field Training Exercise. . O+ @+ d( f# |* \5 ]! G F7 ?FU Fire Unit (PATRIOT)., Y# D2 |! m3 H) U FUE First Unit Equipped.: {" }7 x \- v2 U! c5 Q8 I' i+ U) v MDA GLOSSARY, VER. 4.0 F" c* j, ~! Z- y2 R( w$ O 1145 t+ I v% S/ J Full Mission0 x. H6 [5 N- c- n Capable J$ ?" ` a, T) [Material condition of an aircraft or training device indicting that it can perform all* U' ]" A( {5 C1 ?; | of its missions. Also called FMC.. \( s9 ]8 M, H( O6 W Full Operational / H0 ^1 x6 ]) ECapability (FOC) ; c: I3 Z: D3 a/ L1 `; W# {2 |5 nThe full attainment of the capability to employ effectively a weapon, item of7 Q! |) F: Y+ `+ n, F$ C equipment, or system of approved specific characteristics, which is manned and: n7 ~' e4 r$ T. D c$ ^ operated by a trained, equipped, and supported military unit or force.' M; Y$ A+ s- M& x Full Rate0 y& m- r, L. m) |" o Production& t+ K( F( V9 U; F7 l+ q7 f# l; F Production of economic quantities following stabilization of the system design / s7 d( C0 a3 G3 d3 `, Nand prove-out of the production process.; J: K c; V7 [' A Fully Configured 9 Q% J9 n4 U* P9 c5 ~3 T8 DEnd Item # \. t- {* t. S: Y A2 Q; aThe final combination of end products, component parts, and/or materials, which/ Z* d. Q3 y7 Z0 _% \, D is fully ready for its intended operational use. Normally all production units are' m7 R5 n6 ? y. @" {2 B8 W5 u fully configured. Research and development units may be considered fully - r1 s$ K1 Y. a9 sconfigured if they are or are planned to become operationally equivalent to the( ?( }: o) N" P* w production units.

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发表于 2008-12-25 20:07:01 |只看该作者
Fully Connected0 O0 K5 c( W u3 i7 D Network (FCN) 0 |; x5 p0 I7 y5 B/ }5 IA network in which each node is directly connected with every other node. ; z }0 f9 W- EFunctional) [) T8 D$ @! M% T; _0 r; R Analysis 7 G; }5 E! r& P* L/ X& AAn approach to the solution of a problem, in which the problem is broken down 2 J5 d! g- v7 @into its component function, such as intelligence, firepower, or mobility. Each: F6 R- L" r; D4 ?, F0 J relevant function is then further analyzed and broken down into smaller 3 i% a' a5 k- N# v) _functional components until a level of molecularity suitable for solution of the! ~1 i5 w: B8 G7 Z* { problem is attained. 1 S/ ?6 r: q- z9 {9 d! x9 KFunctional5 l4 z v2 J. ]3 ^, x Baseline * _4 @ y: T% c(1) Established after the system requirements analysis/design activity has3 }# c! X) D/ L7 o' k3 a w$ m6 V completed the definition of the system functions and associated data,! f+ c3 e8 N4 J6 z9 w$ Y: W; g interface characteristics, functional characteristics for key configuration2 M. C6 C7 @9 e& S2 F& r9 X items, and tests required to demonstrate achievement of each specified ( Q5 v% x. z1 G) wcharacteristic. This Government normally controls the baseline.! F: f: K! k& z! r' a( U (2) In configuration management, the initial approved technical 3 e* a: L$ K4 R) V8 G$ Tdocumentation for a configuration item. - ?" Y- N9 r W4 \(3) Documentation describing a system’s functional characteristics and the 8 \4 ~" p" B: a2 |# Qverification required to demonstrate the achievement of requirements./ C; n: u5 S8 ` Functional 1 ], [1 d2 I, V5 AConfiguration 0 _1 T$ t. J8 j6 f& {Audit (FCA)3 S- i; T9 m5 Q The formal examination of functional characteristics test data for configuration , y6 Z" D2 I0 } }3 v& j* j Uitem, prior to acceptance, to verify that the item has achieved the performance+ X; _6 x: a/ ^' z. X/ Z specified in its functional or allocated configuration identification. / a* ^, ]6 c1 H NFunctional 8 [4 H, m& i- N& EEconomic 0 h- _5 K$ p' t" Z4 EAnalysis (FEA)' i7 M: k$ F7 R5 G# W& N: m. y/ }. X- b A structured proposal that serves as the principal part of a decision package for ) ?) E9 f; Y- O1 f- q9 p( W$ aenterprise leadership. It includes an analysis of functional process needs or- g, p% G3 z' t+ T problems; proposed solutions, assumptions, and constraints; alternatives; lifecycle costs; benefits and/or cost analysis; and investment risk analysis. It is* g, T. j1 o( _9 A7 P/ A# x consistent with, and amplifies, existing DoD economic analysis policy in DoD, ]' { M. V& \. N! ^* X Instruction 7041.3. 3 B9 `8 ~% O; G% z6 ZFunctional Kill The destruction of a target by disabling vital components in a way not 6 V4 j( |( | ~immediately detectable, but which nevertheless prevents the target from }) K+ q0 i: k: L functioning properly. An example is the destruction of electronics in a guidance 4 j0 j9 T9 P$ j* ~3 C3 ysystem by a neutral particle beam. Also referred to as “soft kill.”8 N. u4 }( E% L( D# t Functional; x4 V" [. o/ P& O Support 4 P* C8 S9 X$ o( ESystematized methodologies and procedures, or a common set of standards, + P* V4 i8 e& ]5 A+ tapplied to materiel acquisition programs. 0 G. a) V) b" H2 U# sFunctional & P0 }, b: a5 n+ p# N8 ]Technology( V" W+ r. r$ X# ? Validation (FTV) m' I+ f0 Z4 y" QProgram with the intent of proving or disproving a technology is useful for a given 4 {3 Q5 `. }0 k d! M/ [application.9 k3 A# `+ Y- m; r+ H% P$ Q MDA GLOSSARY, VER. 4.0 F, \7 L/ y- q9 g+ T5 _ 115 5 [9 z% J3 b2 _. fFunctional7 o7 U" N9 ]/ U# f+ G Testing # ^4 l; o6 ?( [1 i1 q: tThe portion of testing in which the advertised features of a system are tested for: M/ n% s% d, L* p9 g correct operation. 3 X; U- g2 [( V0 J# ?# N: z3 x5 nFunding Profile Program funding, usually displayed in columnar spreadsheet format by years,! u4 k- }6 @) O starting with previous year through current year and out-years. / z; x" J8 m' t" ]/ LFuture Years1 Y! z5 I4 I; b) d P Defense Program- J( p6 J- @ q* b! h! S, T (FYDP)- W+ Z1 n d& R# m- |# _8 E! ` The official DoD document that summarizes forces and resources associated with 3 C, T$ B3 u) Z1 n* H4 {programs approved by the Secretary of Defense. Its three parts are the4 H6 U' A9 f) r% A4 | organizations affected, appropriations accounts and the 11 major force programs 0 ^, ]0 V4 s# c: b+ D, Z! s(strategic forces, airlift, R&D, etc.). Under the biennial PPBS cycle, the FYDP is # g/ a; V9 U0 Y* S' rupdated in even years in April (POM); October (budget); and then in January7 M# k% c8 _" w u ~ (President’s budget) of odd years. The primary data element in the FYDP is the . \$ [4 @% g) }Program Element (P.E.). Formerly known as the Five Years Defense Program.6 o3 ^. d4 [* b- i6 w5 ?- y FWCA Fixed Wing Combat Aircraft.8 V& n! |, k: I1 T3 u Fwd Forward.. U9 h2 `, D3 Y8 m FXBR Forward-based X-Band Radar. 9 p2 r: |: L) _' ^FY Fiscal Year. , U# C# X) S/ Z. Y$ wFYDP Future Years Defense Program.7 f9 i0 x, Y$ s; ~# \ MDA GLOSSARY, VER. 4.0 G& c Z+ E) h; E' K3 |: J8 K 116 4 @! S }" c9 F$ e$ ^6 zG Giga (one thousand million).7 z1 p% }% a: h6 r* O; U g Gram.' s) \7 H% _. _ [3 d+ Z G&A General and Administrative costs./ `- d6 W( O; C G&C Guidance and Control. " w1 @2 x9 F& u! H0 AG&O Goals and Objectives. ) x* w+ {0 j: u6 O& mG/A Ground-to-Air ( G. j) p% G( q5 ?& X' KG/G Ground-to-Ground.& }( o2 z0 @5 u: W$ o GaAs Gallium Arsenide. * j& e) P# N p7 Q" U* NGalosh The Soviet Anti-Ballistic Missile system built to defend Moscow from missile( u/ B% w1 c# N# _. M- K attack. 2 i7 g/ w6 I% Q0 e: zGamma-Ray Electromagnetic radiation resulting from nuclear transitions. Although incorrect,9 P# }' ?- Q, N5 P- g high-energy radiation, particularly “bremsstrahlung,” is sometimes referred to as - p9 ?6 j9 Y7 u9 G: w$ Q% ~; Ygamma radiation.$ @: A- O. B0 t! c Gamma-Ray " u! ?* R4 y: m1 \9 P+ mLaser 3 f. ~- m3 I* y, u$ k( m/ \A laser which generates a beam of gamma rays; also called a “graser.” A . Y0 ~* L# A: n& ^. H$ _gamma-ray laser, if developed, would be a type of x-ray laser; although it would* K8 X x( y- a! o$ O employ nuclear reactions, it need not (but might) employ nuclear fission or fusion * J: f( p5 n8 V( Xreactions or explosions.( S k3 L2 ~7 X; i! i GAMS GPS (Global Positioning System)-Aided Munitions. 2 o5 C5 J( w" k" |" o% i5 PGaNMPA Gallium Nitride Microwave Power Amplifiers. (A demonstration program to develop# Y U2 D Z, X7 w7 I GaN based transistors and integrated circuits for power amplifiers in systems" ? D* p& j: q3 p1 x6 x7 C such as Ground Based Radar. Goal is to reduce total weight and size by a$ V2 T# n/ ^ H3 {% D1 I factor of 10). " o t7 d3 z0 Q5 m$ v8 p% y. |" \GAO General Accounting Office. " E5 ^: o8 M" J7 ^+ CGARDIAN General Area Defense Integrated Anti-missile Laser System.3 c9 O c* h: F0 j9 L6 j GAT Government Acceptance Testing. 1 w+ ]" Q, x" d2 \GAT CALL Guidance, Apportionment, and Targeting Call (JFACC term).& [3 O3 l ~, j5 w6 }4 v$ L GATE Graphic Analysis Tool Environment." @% d0 Q8 v. Q" m( t( Y Gateway An element that contained a node on the SDS backbone network as well as on 0 C. S! z5 j1 s1 [( y4 `- isome other network(s) and would have performed protocol and format4 V j; X5 ^* A- D) r' { conversions necessary to accept messages from one network and retransmit# h: V/ _! H9 V them on the other. . t( `' N Z! p' L/ oGATS GPS (Global Positioning System)-Aided Targeting System.' |4 [. W9 [ k' r& c" r GB (1) Ground-Based. (2) Gigabyte.( P `7 J: E+ \/ z GBD Global Burst Detector. 9 F! e0 ]0 E/ D* n. V0 w, lGBDL Ground-Based Data Link. - B8 T' k) t3 S+ b8 a( y$ lMDA GLOSSARY, VER. 4.0 G ; _# [ z& [5 ?; Q4 @117 & E1 a* ~9 ^3 ^GBEV Ground Based Experimental Version. 6 R# O+ V7 P8 _' ?2 HGBFEL Ground-Based Free Electron Laser.; @$ M X3 \; o1 z7 V GBHE Ground-Based Hypervelocity Gun Experiment.! V$ W! G2 L; g9 Z. u GBHRG Ground-Based Hypervelocity Rail Gun. 6 `. M" F) ?. v" kGBI OBSOLETE. See Ground-Based Interceptor. 3 b5 Z Q K' B eGBI-P Ground-Based Interceptor – Prototype.- C, M5 x* c0 m GBI-X Ground-Based Interceptor Experiment.4 O% ~ H \$ t5 D9 P' R. l% B$ ~% { GBKV Ground-Based Kinetic Kill Vehicle. 7 z' ?; z* S* u E+ _: q4 ?GBL Ground-Based Laser. 6 u: I/ S, b( j6 uGBLD Ground-Based Launcher Demonstration.4 Y4 {+ c' P$ F M/ }6 @9 v GBLRS Ground-Based Laser Repeater Station. - ^, k2 d( z# F( w, q$ k* E8 PGBM Global Battle Managers. ' {1 e$ s W6 M+ S2 O7 ZGBMD Global Ballistic Missile Defense. ; n' h( [% _5 O; K/ m) L" X/ |" OGBMI Ground-Based Midcourse Interceptor.9 {6 I3 S' d: C GBOS Ground-Based Optical System. ! x8 G# q) U% i. w' y. VGBPST Ground-Based Passive Signal Tracking.4 T( o" e1 }0 t! \; G7 C# g) k GBR See Ground-Based Radar.3 V2 o. b8 t0 Z4 F8 W$ ^2 W8 ] GBR-M Ground-Based Radar-Midcourse. , D" E1 M9 M$ J1 h7 P! `6 jGBR-O Ground-Based Radar-Objective. % g8 z0 ~- j1 Z4 l6 n# A% _' p. IGBR-P Ground-Based Radar-Prototype.( l3 j# _% g$ E0 o GBRT Ground-Based Radar Terminal.& F( R. a7 N& \0 S( F GBR-X The experimental version of the GBR. % i2 k9 o i/ i$ d4 R% z$ t& _GBRF Ground-Based Radio Frequency.

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GBRI Ground-Based Rocket Interceptor.# r& l6 R; Q% z& C9 b/ [! m5 _ GBRT Ground-Based Radar Terminal. 7 a! G+ ^6 O& oGBS Ground-Based Sensor. : l7 n; D* m$ W8 J5 EGCA (1) Guidance, Control, and Avionics. (2) Guidance, Control, and Airframe.$ Z! H" ?- g9 x GCC Ground Component Commander (JFACC term).4 w4 [6 Y" U) W! m GCCS Global Command and Control System. 2 U- e6 L+ L! V. \MDA GLOSSARY, VER. 4.0 G # V" d3 O9 ?; t1182 Y( d5 s$ I8 d$ f GCI Ground Control Intercept. , T, N0 z* I7 f4 S! xGCN Ground Communications Network.& a! B9 W& e9 K0 L& j0 a' u- \. i GCS Ground Control Station. ) f3 e) L/ o3 n" |( k0 ZGD General Dynamics. 0 f t6 ^* i/ z1 c1 \. g4 BGDL Gas Dynamic Laser. $ l4 P( i- M" t; a8 kGEDI Ground-Based Electromagnetically-Launched Defensive Impactors. # t5 b, ^: ~$ ~+ n9 iGEM Guidance Enhancement Missile (PATRIOT).+ f6 i2 H: {; K General Manager+ I1 V7 |& T$ G0 l+ r1 N; T Program 6 l% q0 _2 ]1 K7 a3 `% j. SManagement & g( c8 N1 Z5 ]; n. U0 k- nDirective (GPMD)# }# y4 n+ j& j# x OBSOLETE. The primary document used by the GM to direct the Service BMD 4 Q# c: E9 I& }* K: [3 ]PEO on the specific actions necessary to fulfill BMD program requirements. ~4 ^- {" }8 w( y) l: E& pGeneral 8 h+ @8 L" i' I |/ oSpecifications* g& a! ^: b1 J; v8 D A general specification covers requirements common to two or more types,; _4 y1 A" v+ S classes, grades, or styles of products, services or materials; this avoids the ]) c) t9 b7 a; m2 G8 j- x# V- }9 @repetition of common requirements in detail specifications. It also permits) [% t8 W: ?, P( l5 m2 z; @ changes to common requirements to be readily affected. General specifications6 Z# D% [2 G4 }, R9 q; w may also be used to cover common requirements for weapons systems and1 S5 b# I8 M5 D% c$ T8 t7 ^& A9 A subsystems.% ?" Z6 n8 d. t y' o$ H+ D6 u Generic Rest of0 L I: l- I8 n2 Q World Target p: M% B6 P1 o7 x5 Y! J (GROW) 4 d% F7 h' ?; H* \Strategic target being developed for GMD program.+ G5 @: c9 h) s5 x GEO Geo-synchronous Earth Orbit.; x) H4 a3 Z* c3 W+ p% q# q GEODSS Ground-based Electro-Optical Deep Space Surveillance System.5 q3 h: \: D; P* D3 e0 O8 n3 v- u9 C Geo-stationary- O9 q3 A6 `$ ]$ ?" q Orbit (GSO) * ^# l/ m& I' {, w, JAn orbit 35,784 km above the equator. A satellite placed in such an orbit ( r6 _* ~) a0 ~2 A3 ]& mrevolves around the earth once per day, maintaining the same position relative) a3 ~7 a( |3 O( `% \5 s. Z6 H to the surface of the earth. It appears to be stationary, and is useful as a# }9 J' f% C+ j8 G communications relay or as a surveillance post. & B' V' f3 q$ }2 D& I" N9 {5 H6 ?GEP OBSOLETE. Ground Entry Point. IFICS. 0 Z* T8 Q3 o9 ?/ l* uGES Ground Engineering System.! P/ @, k, x2 k9 q, R GFE Government Furnished Equipment. See Government Furnished Property. % _7 K- w* M% G' K" qGFI Government Furnished Information. ( D% [9 b1 k; C7 f5 u; s) d7 K8 uGFM Government Furnished Material. ( L- `1 x. f$ \9 S) ?. t) LGFM/P Government Furnished Material and Property. See Government Furnished' E: Y# Z S7 j. {8 l/ c Property. & O a# Z3 R3 n( ^( MGFP Government Furnished Property. h) R$ t8 E3 N; I; ^GFS Government Furnished Software. See Government Furnished Property. ! |0 s& w" Y, T! HMDA GLOSSARY, VER. 4.0 G6 }/ O( |: D& Z 119 : g) N1 B3 s, p [0 H& Y. u5 q% XGhosting This condition occurs when two or more targets reside close to the same plane 9 t% H: b: F' `+ \also containing two sensors viewing the targets so they are within experimental: _. Q7 O1 Z+ Q determination of having the same hinge angle F. Thus, ghosting depends on 2 Y) @* L( K' B& wLOS error and positions. 4 c) c& [& j+ f9 N8 }8 i2 B, fGHz Giga Hertz (1 x 10(9) Hz)., X+ o Q1 p- a3 n) D GIDEP Government/Industry Data Exchange Program. " m; Q2 L- @" dGIF Generic Interface. 4 c, u V! C( G. y$ OGII Global Information Infrastructure.& K! I# c" U8 y- Z( j GIP Ground Impact Point. 8 [4 r6 _- Q" l# c; v" `( RGIS Geographic Information System.2 F$ I( h8 e/ q- f GITIS Government Integrated Technical Information System. $ ~) @, \+ |8 X) S( JGLCM Ground-Launched Cruise Missile. ; y3 `7 G. P n. o' dGLP Ground Launched Probe. See Brilliant Eyes Probe. / g% k, l4 q# }- oGlobal, F) Y* a4 X2 [( ~ Environment 9 x( b4 j: P8 \" yThe ISTC Global Environment is responsible for the creation, propagation, and# N. ?& t) _. X" m maintenance of test scenario common knowledge, how subsets of this 9 e- s" c) L8 U5 T$ Q2 I4 hinformation will be determined, and how common knowledge will be disseminated8 Y* m1 h2 a% a to the various element representations (nodes). The Global Environment + D1 N% j9 ]: q* cperforms functions which are common to the scenario such as timing, health,7 j+ {% Q7 l8 z( g& E/ K status, state vectors of objects, and effects models.- ]6 }3 | V K" ?6 H Global * ]* F1 [! e, n, YPositioning . k, z2 \2 Q( Q: t9 T' eSystem (GPS)3 q4 p% h8 ]9 u3 A The NAVSTAR Global Positioning System is a space-based radio navigation 8 e9 c* V8 p* @' t. lnetwork providing precise positioning and navigation needs of all the military / p2 `; I8 w- v, ~! r6 T, F5 _. oservices. In the fully operational configuration, there will be 18 satellites in six 4 W* I( s) w, C Rorbital planes with an orbit period of 12 hours at 10,900 nautical miles altitude.+ D# \7 q) p' r Each satellite transmits three L-band, pseudo-random noise-coded signals, one ) Y5 o( D) S+ n u# i( r9 qS-band, and one ultra high frequency for spacecraft-to-spacecraft data relay.5 s+ z, Y, }; X* E9 r! P Global Protection 4 y; w1 E* T( n2 k9 FAgainst Limited9 E( D1 V/ G$ c Strikes (GPALS)# x ^! P2 G, ~6 X5 u OBSOLETE. GPALS was an architecture denoting an anti-missile system + c+ {5 F- N. e; v1 n' T i9 D2 f( c. Zdesigned to provide protection against limited ballistic missile strikes, be they . t2 _% `9 ]( l; o) u4 O( a: rdeliberate, accidental or unauthorized—whatever their source. GPALS was0 w& V3 @, z& R) t composed of three interrelated segments: (1) theater ballistic missile defenses, 5 R/ y5 A, L' v$ m$ K+ Yand associated space-based sensors, to protect U.S. forces deployed abroad,+ o9 J$ [ q( b) a- n. s and our friends and allies; (2) ground-based defenses, with space sensors, to 9 D! W6 g3 k/ _) e# q* W- @- uprotect the entire United States against long-range ballistic missiles; and (3) 2 j: m& ~4 n6 F- {interceptors based in space – Brilliant Pebbles – capable of providing& W. N( l% S6 \; Q# E6 g7 w- @ continuous, global coverage by intercepting enemy ballistic missiles with ranges # O4 _: I3 Z4 N8 L& [9 `* _/ x0 zgreater than several hundred miles. + J7 x( m: Y6 r0 \9 `* n9 C* bGlobal Protection # q' v' @1 |8 n6 m5 ~% PAgainst Limited 7 \# ?, n+ c9 MStrikes (GPALS) 0 O q; y4 J& m: K3 oProgram9 _4 j! M; `0 a( t/ L OBSOLETE. The GPALS Program consisted of six Major Defense Acquisition! @" K- Y% Y- E1 Z Programs: GPALS System/BMC 3 & X8 y; V9 \! m y' `' `& g, National Missile Defense (NMD), Global Missile 0 i' [6 p7 \7 @; q$ ]$ TDefense (GMD), Upper Tier Theater Missile Defense (UTTMD), Corps SAM, and % @; `- |( P. H2 ?) EPATRIOT. Army PEO GPALS was re-designated PEO Missile Defenses in 1992. 7 N; C1 S1 `2 ]GLOBIXS Global Information Exchange System. : V* D% h9 Z) lGLONASS Global Navigational Satellite System.6 Q. I5 z! @; x: p5 z, x$ a u% m MDA GLOSSARY, VER. 4.0 G1 K4 j" y8 n1 m: A, e. s 120* S) \+ d# @2 y) J7 c GLOW Gross Lift-Off Weight.! _- V; e2 t7 j9 w) R* f GLP Ground Launched Probe. See Brilliant Eyes Probe. % O2 |- T- \0 z$ E* XGLS Ground-Launched Sensor. ' r( G4 i" k2 I0 WGM (1) Guided missile. (2) General Manager. / f K/ r; |/ k' \* I6 NGMACC Ground Mobile Alternate Command Center.8 O$ g3 B- F9 x% k B" l GMAOC Ground Mobile Alternate Operations Center. / \% c7 C1 e6 F4 X6 G6 m/ L' l$ _GMCC Ground Mobile Command Center. ' d# g0 z0 p+ J+ r3 U6 m! JGMCP Ground Mobile Command Post. " \/ j6 \# a/ SGMD (1) Ground-based Midcourse Defense (formally National Missile Defense) (2) . r) ?" O$ z' w. Q4 CGlobal Missile Defense (OBSOLETE).1 w4 ]0 v; S. |, Q& T) V GMT Greenwich Mean Time.8 D2 f: F, Z, J; f; C GMTT&C Ground Mobile Tracking, Telemetry, and Control.5 l! f! O( T8 P+ F0 h2 {% H: r GN&C Guidance, Navigation, and Control.7 b4 V% P2 u! n5 y6 a4 ^ GNC&P Guidance, Navigation, Control and Propulsion.7 r8 g4 [6 G# H3 j GND Ground. 8 t' g5 D. x" V9 m1 _( cGOCO Government Owned, Contractor Operated. ; @+ w Y4 p" d0 Z; F9 ~. NGOES Geo-stationary Operational Environmental Satellite. 1 D+ W) l' e9 w N/ nGOI Government of Israel./ q: k9 V4 J3 R( Y+ n6 B GOJ Government of Japan.

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GOSG General Officer Steering Group.9 @' s R( H: u1 Z# q% K( T7 y$ d GOSIP Government Open Systems Interconnect Profile (CALS term).0 X Y1 h+ p/ U' ~" q X$ W GOSP Government Open System Protocol (CALS term).: {( _0 O& c9 d! S- j GOTS Government Off-the-Shelf.1 H# F. R6 U( ` Gov’t Government. 2 }" [! j. l' q6 F+ w! g3 N- IGovernment7 @* A1 h' W6 L( g: g Furnished ( z3 q" [) z. m) x7 DProperty ; W* p y$ H' A8 W1 E: K5 a: CProperty in the possession of, or directly acquired by, the Government and , U8 k* g0 A; s# M) {subsequently made available to the contractor. (See FAR 45.101.)2 [) g: o. I( c( E. H0 ` Government 8 t7 A2 N) ~/ yVerification+ S6 n+ {" s, @ Management0 L. K3 P, t) `. s& R) T1 d1 Z. z Plan (GVMP) 8 v, z# M4 f. X s/ q2 KA management document that provides the overall framework for BMDS7 P( |& a5 C5 b+ C' G/ r$ ^* Y verification. It includes processes for implementation, organizational 1 p+ U4 H) b: G2 c$ \relationships, and stakeholder responsibilities. It covers the full scope of BMDS : W' s$ w' o' x: C6 K' Zverification and identifies how all BMDS verification activities will come together to4 G7 [" ]" x d/ i/ g# Z2 S confirm BMDS capability.$ I: n0 P% S% v) t( H" ?8 H MDA GLOSSARY, VER. 4.0 G 4 J. O- s, _: C& u9 c" d- ]7 b121 6 c, [% T# [+ rGP Group. . t5 {) V. _$ GGPALS Global Protection Against Limited Strikes.9 X) ?4 b% E# t+ L; Y5 } GPC Global Protection Center. Q* ]2 T8 u' @7 AGPMD General Manager Program Management Directive.2 f/ \$ h" Q# y. i2 }; t GPO Government Printing Office (US). d; i! q3 f2 e6 V1 x GPP General Purpose Processor. 7 s7 [ @' S9 u4 z7 Z6 |2 U5 FGPS (1) Global Positioning System. (2), Global Protection System." p( y- V$ P3 f GPSIU GPS Interface Unit. 7 l! a, e& C2 ]7 q4 vGPU Guidance Processor Unit (US Army term).& n. c' ]6 Z9 x6 w- V( E Graceful 6 w8 y# S' A3 \ s4 X% D) B# U4 GDegradation+ [: I3 O m7 R0 z0 T A condition in which a system continues to operate, providing service in a # j4 V X0 n; Z$ [0 cdegraded mode rather than failing completely or catastrophically.+ I+ B6 ]( s* a2 w GRASER Gamma-Ray Amplification by Stimulated Emission of Radiation. (See Gamma- 4 U$ _# s7 z. w$ J. T% M% S+ |Ray Laser.)7 ~, _$ G, `7 j( U) I# t GRC General Research Corporation.: k7 T. Y: P$ S; h Green Code Interface Software. ; z/ l0 `9 v/ e! mGround-Based K7 x! o9 _) A4 U5 p' ^ Defense* i& _. U8 Z' @! I8 N( m The ground-based sensor and weapon systems of BMD. 6 P8 S) o; N6 C" P2 xGround-Based 3 ?- y" M$ ~ T$ PInterceptor (GBI)7 R( H* b1 [" b8 } A kinetic energy exoatmospheric interceptor with long flyout range to provide,& @- T; m U$ Q0 S7 X; ?& V4 Y% f7 R where possible, a multiple engagement capability for defense of the U.S. with a# H r$ H- A7 p U/ }; s# { relatively small number of missile launch locations. It is designed to engage # I9 g$ t! O! U& opost-boost vehicles and/or RVs in the midcourse phase of flight. / H' Q: d0 }. s4 l0 a$ f: q(USSPACECOM) (Successor to Exoatmospheric Reentry Vehicle Interceptor7 @' E; Z3 `6 }6 H9 `* p- M Subsystem (ERIS).) See EKV.6 }5 ]3 Y$ w: v8 J# H. K Ground-Based - Y$ G" k# Z$ G2 [- sInterceptor : J0 d% \# l. n" k% ]6 l% [7 EExperiment I, G, k. b( f2 d z5 f (GBI-X): A; R& ~ X, f6 Z) w7 R" v# s Designed to infuse advanced technology and promote competitive environment ; v, h+ f% I5 ^0 pfor GBI.( |2 @6 [) ~; R4 l Ground-Based" M: R% \& V2 N1 N5 V1 w# u' M Radar (GBR) - z d% Q9 Z1 a" s$ a# r8 L0 |A task-able, modular, multi-function, phased-array radar that provides " H6 b% d& E* j/ b. Z6 L5 u( xsurveillance, tracking and engagement planning data in post-boost, midcourse, # ?/ G9 o: c% d0 ~5 Tand terminal flight phases within its capabilities. It also provides target0 c9 R; |3 l- t+ z/ @* E3 _1 G discrimination, in-flight target updates (IFTUs), and target object maps (TOMs) to* b( |) J( L- b. `" C' ] interceptor vehicles. See THAAD. (USSPACECOM)0 q5 h" m* [/ Y8 G9 C) a Ground-Based 1 `( v; r. H. X n ]Radar Terminal 0 F! `; ?3 I+ S(GBRT) - L9 h, s4 m! x; @The sensor for the NMD system. An X-band, ground-based, phased array radar) N/ v$ J, d1 U5 Y capable of detecting, tracking, and providing discrimination information to a 5 }, J9 ] r% x7 M m+ T7 Fground-based interceptor.) z" n+ V2 r" s( e3 S+ c& O Ground-based' _, e. Z! B. C, R9 E. B Surveillance and 8 b* O. I G) O, aTracking System 0 z+ Q5 Q o8 l/ X(GSTS)% ]6 K% `) x$ D. [: E" K n A fast-response rocket-launched sensor, which can support the SDS midcourse 3 T. W* q& R" \1 w3 `6 \0 n/ nsensor suite by employing multiple Long Wavelength Infrared (LWIR) wavebands, o! t2 T `. v and a visible waveband sensor to provide tracking and discrimination of % h/ W' a8 O1 [9 H# i+ Wpotentially lethal targets.8 N* S1 U2 Q- v7 j3 e _ MDA GLOSSARY, VER. 4.0 G& i$ y6 s1 Q# t, E. u 1222 |% k$ M* c- X( d7 N( _ Ground Entry X& A" ]* o3 l5 F9 sPoint (GEP) * I& j( P- w v6 L/ {; I/ x0 UOBSOLETE. GEPs provide the communications interfaces between the SDS " W0 D% _, s4 _) C1 t. ~8 Ispace orbital/sub-orbital elements and the C2 E. See IFICS. v# p' ` R- A/ |# F+ J Ground Mobile* A. k9 _/ n! ^2 l8 G, F Regional0 U g1 k; P8 m# e Operations6 Z x) r& q$ |& U% ` k4 J: X Center$ n3 K1 G/ y6 _1 i) ]8 Y6 S) v (GMROC) , w; a, B# ~# O( h: Z+ M$ fTransportable ground segment of the Regional Operations Center. , l9 ^6 u5 x* {. @9 qGround Zero The point on the surface of the earth at, or vertically below or above, the center" _6 i+ W Z2 O! W1 u of a planned or actual nuclear detonation.- j* n+ d% n& t: X GS Garrison Support (US Army term)." U. m' d6 \. c GSA General Services Administration (US).- W0 [3 h5 p# H" ~9 J# g& d GSDC Ground Station Demonstration Lab.7 U3 e7 h+ g3 k9 @ GSE (1) Ground Support Equipment. (2) Government Support Equipment. 5 j, l+ O* c0 B3 y9 IGSFC Goddard Space Flight Center, Greenbelt, MD.9 f9 ?( v6 Q+ i1 B& V9 v GSII Government Services Information Infrastructure. - O* W1 D; C4 c/ U( D& G6 OGSM Ground Station Module. * K9 ]. n0 S. U0 Y3 sGSO Geo-stationary Orbit. 4 U8 Q. j; C( n! A, q- ^; j5 rGSR Ground Station Radar.0 o* f: d5 G' v' V+ L2 m! Z. r5 q2 Z GSTS OBSOLETE. A fast-response, rocket-launched, Long Wavelength Infrared; P9 ]7 z% M. r% c" J (LWIR) and visible waveband sensor, which would have enhanced the' P( e. x! R; G: M: z$ T/ g information available from the SDS’ midcourse sensor suite by providing tracking8 M+ T% E) L5 O% \* {: f8 g and discrimination data on potentially lethal targets. # I' R8 o j: y5 ?" Q. Y) B. BGSTS (F) GSTS Farm. i$ n0 ]1 g6 a3 Q9 H$ ?GTA Ground Test Accelerator.2 m" g: L4 T0 f3 Q GTACS Ground Theater Air Control System.7 J4 W: ]' X5 m) d! u: a6 J GTE GTE Corporation. 7 A O, c6 J y* VGTF Guided Test Flights. , N) Y& k8 P+ v6 D* eGTM Global Track Manager. 3 K5 J4 }4 W/ t( u- g+ L! rGTN General Technical Note. * h6 y$ e! G. K/ B% LGTR Gulf Test Range, Eglin AFB, FL. / F8 O4 f9 G, S9 O2 d6 N3 `$ ^GTSF Guidance Test and Simulation Facility (PATRIOT), Huntsville, AL.2 o" H8 b6 e! x3 {/ K GTV Guided Test Vehicle. ) W3 K6 P2 m+ H/ J- v7 \GUI Graphic User Interface. $ A# i8 y* y. \* ?' N! Y, NMDA GLOSSARY, VER. 4.0 G . d5 r( }3 h: Q b! l123. k* d: l* R Z2 a' r+ R Guidance (1) Direction, altitude control, and navigation (where appropriate) of sensors , J' s. R% @. i2 y: N) zor interceptor vehicles.1 a7 X, }% I0 ]& ^0 L# A4 T& n, d) V (2) The entire process by which target intelligence information received by a # A; J9 ~& U! _5 s/ J$ r1 Bguided missile is used to effect proper flight control to cause timely" x; P5 v: P1 u% Q- r" U direction changes for effective target interception./ r6 X# }% {7 R6 [ Guidance6 r; J4 ]* v/ O0 [9 W- S$ F Enhanced3 Y/ K f" H) |3 x$ R& R4 K Missile (GEM)( N8 X1 ?- V2 q0 C# W- I5 F3 d A companion program to PATRIOT PAC-2, which includes enhancements to the; K- V4 m8 I7 L- [3 |' c radar to increase intercept range and performance.4 _! a; H/ P4 P8 _' V$ T Guidance- s: [( z( }# o4 d* w9 G System (Missile)8 P. I! W! _8 w A system, which evaluates flight information, correlates it with target data,9 r# W! I% [+ F8 B. y1 [1 W$ \ determines the desired flight path of the missile, and communicates the : o( t# m: f# T* Hnecessary commands to the missile flight control system. % W0 F& k2 F1 R7 n3 c3 aGuided Missile An unmanned vehicle moving above the surface of the earth, whose trajectory or 0 g2 K6 \- Y8 s1 n5 B, Nflight path is capable of being altered by an external or internal mechanism.8 a7 K* U) S, ]) P; [5 P GVSC Generic VHSIC (Very High Speed Integrated Circuit) Spaceborne Computer. H7 [7 [3 N5 s. Q9 T* D0 QGWAPS Gulf War Air Power Survey, 1994 [a DoD-sponsored survey].& F8 w, ~$ ^5 \8 C9 D5 v: g4 R5 ~ Gwd Giga watt-days. # L: ~2 Q3 t$ Z. ]$ ~7 pGWEN Ground Wave Emergency Network.; s% M$ d$ ^" ]; t* G GZ Ground Zero.0 }: v# P$ q) h' k8 [% O4 V MDA GLOSSARY, VER. 4.0 H 4 C2 n0 {/ T5 y8 K124 s! x1 i9 f: [3 C# e3 g! {& b; o2 l# yH Hour. - R5 I6 ~0 K7 a* W l: X% u2 N2 DH&S Health and Status.( b, `, h; M2 x9 d H/W Hardware.# }+ E0 D$ r# U: V HA Higher Authority. 6 y0 d( A* A$ r3 A( D% ]4 SHABE High Altitude Balloon Experiment.! u1 ^: P4 t1 p+ l HAC House Appropriations Committee (US). 5 C3 O: O; ]8 l D/ K& O. IHADS High Altitude Defense System.5 A- e! O5 l8 n HALE High Altitude Long-Endurance. . D) @/ h) I+ d @0 ]" l" i3 \HALE UAV High Altitude Long Endurance Unmanned Aerial Vehicle. & M- i2 G* f* i. _' UHalf-Value0 b3 v }& _) g+ D, M Thickness (HVT)6 X( I- j% V. w7 ~. k7 E& n; x& L$ S The thickness of a given material, which will absorb half the gamma radiation+ R. Z2 A9 u6 i, l2 i% P incident upon it. This thickness is inversely proportional to its density and also ) ?1 U# K$ z1 x _3 w3 vdepends on the energy of the gamma rays. . T7 v, |8 m) h! D' nHALO II High Altitude Observatory II - u* @% b2 g9 H f! y# T1 ] WHAMS Hardness Assurance, Maintenance and Surveillance. + o4 T8 @* v/ HHandoff This occurs when information on positions, velocities and tracks are given by one # ^6 A& y; _! y3 u( u3 {sensor or system to another and the first sensor or system continues to track the% c5 ]# f5 U* v% c$ ] objects., N/ O2 f) F+ b7 n+ G/ R. J Handover This occurs when information is passed on to another sensor or system in which 7 v& t5 M8 s* n2 P% d/ f9 fthe first does not continue to track. * w+ _8 T' r/ THAOI High Altitude Optical Imaging.

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HAOIS High Altitude Optical Imaging System.0 A y% N: z6 U/ _. A HAP High Altitude Probe.; p+ _4 x* V' d Hard Kill (HK) Destruction of a target in such a way as to produce unambiguous visible- e! ^* i' Q! s7 b, k$ W evidence of its neutralization. 3 d( n# t; a* b5 ?& J+ GHardening Design and manufacturing process and other measures, which may be employed 8 s$ j0 F; R! {4 kto render military assets less vulnerable. / b! b& Y& S: P3 @+ N1 dHARDMAN Hardware/Military Manpower Integration (Navy ILS term). , R" E' C0 ^9 l$ H9 ?: e/ g4 ~Hardness A property of a target; measured by the power needed per unit area to destroy* W f$ {/ B9 m8 m s6 z the target. A hard target is more difficult to kill than a soft target. 6 r, D% v/ O S4 X3 z, v0 cHardware-in-the-! ^; Q/ C% p: O Loop (HWIL)7 W- U- S- S8 q6 g) K+ L% @# J: }9 E2 s Tests in which BM/C3 computer and communication test systems will be in9 O* F: W' A1 { communication with some of the hardware test facilities developed for other BMD# X1 V6 v, j7 S% I0 K4 | technology programs.+ O8 M T% K0 w P Hardware I" R; p+ @: z) G0 W0 iSecurity * Q: Q }+ E3 u" Q& e' RComputer equipment features or devices used in an ADP system to preclude! O7 d4 ~. q1 u3 Z* f unauthorized access to data or system resources./ C9 T- F z: h0 i# i HARM High Speed Anti-Radiation Missile.% U+ i3 o' M" J" ]9 H% _- c MDA GLOSSARY, VER. 4.0 H% |0 i( \2 Y) c8 A1 O! u 125 7 N! J" @3 |! a! Q4 ^HASC House Armed Services Committee (US). 1 N& M) a \5 ?4 N6 I UHASP Hardened Ada Signal Processor. # g8 q4 R; w* {5 x9 [4 QHATELM High-speed Anti-TEL Missile. 5 G# Q( q$ s6 ?- HHATMD High-Altitude Theater Missile Defense. (U.S. Army)4 |/ d) z+ C4 { x4 ]! }3 Y o- E HAVE STARE Name assigned a proven sensor capability. . j9 A. c% n- SHAWK Homing All-the-Way Killer.+ O" J3 Y( x/ [1 y: T: o6 d. H& Q HBCU/MI Historically Black Colleges and Universities/Minority Institutions. * ~; u- a& W* `' D! hHBHO Hard-body Hand-over [algorithms].3 I) K1 ^8 |' D HCO High Consequence Option (Safety Engineering term).( i5 C- a4 ?$ K( S3 r) b HCT Mercury Cadmium Telluride. " o1 Q4 a; h$ {4 x# B1 E( LHDA Hybrid Detector Assembly.# Y8 C8 G% ]* Q& M7 S* h, Y3 f HDBK Handbook. . n$ L9 P* `$ {7 u. F) ]HDR High Data Rate.& S9 f9 b5 ?, Y+ ~8 Q) P HDX Half Duplex (TelComm/Computer term).% M$ d: [" H' ~) N1 `2 ^6 K HE (1) High Explosive. (2) High Energy.2 ~: W" R, ?8 c' z Health and Status( L2 y9 F) o$ i3 |# [/ a (H&S)- A% l: ~, C. f+ x0 G Health and Status pertains to a unit’s ability to assess the conditions of its 1 h% j. S: K5 c, N. d2 G2 vsubsystem functions. The term H&S is used for units in remote locations, such + a7 R$ Q" o+ u5 k8 |4 C) z' Las satellites, where ground controls must interface with BITE to determine6 _# B1 a- p6 F& _/ f" W- a8 v operational status of the satellite and its equipment. 7 D( A( m2 ]5 ], Q1 [# |2 eHeavy Replicas+ }* T, F+ y% {1 f (HREPS) 7 W: B4 Y3 N. [9 k+ M* D1 \0 ZDecoys, which by virtue of shape, size, and mass, closely approximate an RV’s: o Q' K+ t" U' a# r signature. HREPS have significant off- load penalty. 3 X! G9 b: h/ j$ jHEDI OBSOLETE. See High Endoatmospheric Defense Interceptor. R- S( y/ `, S3 K3 S HEDR High Endoatmospheric Defense Radar. 9 P7 \' _3 d( Z. N. IHEDS High Endoatmospheric Defense System.+ U3 v) a/ q8 Y6 z HEI High Endoatmospheric Interceptor. + G( L. _) E+ Z s) i% @HEL High Energy Laser. ; o c* f" X1 n( D) cHELKS High Energy Laser Kill System. & ^* p( D, s. K5 S4 MHELLO High Energy Laser Light Opportunity. * Q* z) Q& ~) N3 VHELSTF High Energy Laser Systems Test Facility. # [; ]: P- g: }9 n4 vHELWS High Energy Laser Weapon System. . _) k" u5 |5 G. _HEMP High Altitude Electromagnetic Pulse.; A: }9 j0 B( S4 P: C& A3 @% M MDA GLOSSARY, VER. 4.0 H / r7 B% g. |/ e- P; x126 & ~7 G3 k, \" _- `& RHEMTT Heavy Expanded Mobility Tactical Truck (US Army prime mover).9 N+ C' x) ~; |" @6 P Hen House Soviet area defense radar used as a component of the Moscow ABM system - a0 I5 P9 q: v4 }( X3 ithat provides VHF coverage of space to monitor orbiting satellites and early - M) `: I: s, U' @* T5 ]7 v4 V/ zwarning of ICBMs launched from the U.S.' {5 z. T* c6 O* X HEO See High Earth Orbit.2 |' Y, B: v, Q0 l) ]1 n4 Y) {: O HERA (1) An improved surrogate TBM test target.3 }' }. m( \; k (2) Two-stage, ground launched solid propellant theater target vehicle. (MDA 7 u( h5 q8 N5 G* j5 aLexicon) ' ?/ T9 L( M& L5 kHERO Hazards of Electromagnetic Radiation to Ordnance (SM-2 Bk IVA).& a, y$ t9 d! r HESP High Efficiency Solar Panel. 4 q: ]# N8 R- z- B) k* ]* ]HEU Highly Enriched Uranium.5 T7 r7 y1 y$ L( [( Z HF (1) High Frequency. (2) Hydrogen fluoride. 7 ^% ~1 O$ p2 Q2 T) _6 ]- NHF/DF (1) High Frequency/Direction Finding. ( O0 I. L) M! I; B(2) Hydrogen Fluoride/Deuterium Fluoride. (Chemicals used in IR chemical 7 s) s# O) a0 J7 z: f3 o6 w' Flasers). . z- W* Q3 p6 h( BHFCNR High Frequency Combat Net Radio.4 u* j F+ o+ x" `: g HFE Human Factors Engineering. ' F, e1 {1 g9 sHgCdTe Mercury Cadmium Telluride.& m9 q% P; `2 ^2 v% z0 w: ` HHB Headquarters and Headquarters Battery.' `( L W% W' Y( m7 o) Z) p2 G" g) R HIBEX High-Acceleration Boost Experiment.5 ^( V- y9 ?# D* r, J6 B% i HIBREL High Brightness Relay. 8 C& [% \! b+ Q8 }5 ~HIC Human-in-Control. . o; u. o4 F! j" G' dHICOM High Command (Navy term). }" a' R- W/ o0 r S# {/ M4 T HICTB Human-in-Control Test Bed./ H+ Y, e: `; x5 G8 H1 D HIDACZ High Density Aerospace Control Zone. 5 o& `* W; x; d# P, JHIDAR High Data Rate.$ I; n4 G+ U) i x High Earth Orbit [1 |2 \4 d" v(HEO) 7 C4 P1 g. P# c; V' OAn orbit about the earth at an altitude greater than 3,000 nautical miles (about 2 m( N. S& ~% N# h4 d5,600 kilometers).4 F& |6 N( e7 X9 u2 D High( u" s& z) ~5 O1 s! }+ B& d+ ] Endoatmosphere , y% [6 Q h9 @5 MThat portion of the earth’s atmosphere, generally above 40 km altitude.5 f8 w8 O* D4 F; j" a) W* j4 d+ y High ; s! V8 ]1 B- k6 H! [Endoatmospheric 1 J* m: U/ d5 ~7 f" c) q3 UDefense% W) ? r- E/ c( [; X8 Q& T Interceptor (HEDI) / t# u& V2 T# s4 `6 b9 s& pOBSOLETE. Interceptor concept designed to engage RVs within the (upper or + O! l% O1 S7 V( l, uhigh endo) atmosphere. (Predecessor to Endo-Exoatmospheric Interceptor - P) d. X) q" L! L& m3 x$ b. e6 Z(E2I).) ' T. U, F2 b r2 LMDA GLOSSARY, VER. 4.0 H ! e9 L9 b# D6 x9 l127+ @4 N3 d' X; T High Density ! D3 a8 ~! S$ u' \1 r) W1 NAerospace2 ~8 j2 w1 H- m. J" c) X Control Zone 4 f. ~; r P/ k: K. @3 s(HIDACZ)3 }) s1 G# o" g# Q Airspace designated in an airspace control plan or airspace control order, in 5 J! t- S/ a# ^& \, Vwhich there is a concentrated employment of various weapons and users. A 2 b5 J' d$ d; m9 w1 t: q+ zHIDACZ has defined dimensions, that usually coincide with geographical4 u _0 o. U% a0 ^& A& ] { features or navigational aides. Access to a HIDACZ is normally controlled by the5 N+ ]! t1 U0 I$ J' I9 } maneuver commander. The maneuver commander can also direct a more 2 G- B3 I S" K- W( u \% q* _restrictive weapons status within the HIDACZ. . l R, f) Z5 O' N( Q Q4 YHigher Authority: ~1 Y6 s$ S, p8 A, ^ Interface ; K" }3 w. _: V7 n Y; ZPolicy, strategy, doctrine, readiness conditions, and rules of engagement from& h. V! x3 e) t6 l4 k higher authorities for use by the defense system in conducting system 4 u. J+ d% ~0 `& A8 Q8 V' D$ i% ~* joperations including specific orders specifying actions such as testing, defense4 f4 Z! Q4 P9 r) T- V8 s6 ] enabling, pre-delegation of authority, etc. Also the reporting of situation 7 J/ t/ Z$ q" L; J# u" Jassessment and system readiness to higher authority.6 q4 ^' `. e0 Z3 i; f High Order7 |6 Q* k- s: e4 v* H Language (HOL), y' t' G( L9 F; n4 j5 P A programming language that requires little knowledge of the computer on which- R$ \. ?2 d: t1 V$ }- w( f a program will run, can be translated into several different machine languages, 3 b& S0 K$ g9 o! lallows symbolic naming of operations and addresses, provides features . n+ B7 F. ?0 C( fdesigned to facilitate expression of data structures and program logic, and6 S" P3 S7 U& _5 s8 \8 P usually results in several machine instructions for each program statement." B! t5 W/ O X9 W$ _$ O6 }9 l HIL Human In-the-Loop.# J7 x* Q! G5 G7 F$ ^% M HIMAD High to Medium Altitude Air Defense.: b5 |& h. P0 f5 C# k% W8 @% H HIMEZ High Altitude Missile Engagement Zone. + R* g3 m [, x3 ?0 {. m& q5 EHIP Hot Isostatic Processing. & U u! E7 O/ T5 M: FHIRAM High Resolution Infrared Auroral Measurements.. ?* y6 v& H H2 K, {, P2 J6 D HISEM High Speed Environmental Multi-burst Model.' X* p1 ?# H E HIT (1) Heterojuncture Internal Photomissive. (2) Homing Interceptor Technology. ~8 K7 R2 N+ C$ n3 D N$ L HK Hard Kill.: Z# R+ O. h$ ?! S7 b3 p$ V$ L! N HKV Hit to Kill Vehicle. * c4 c( z( a. F# l% mHLD Hardware Description Language. - W* X" z- h, \1 w( Y! sHLLV Heavy Lift Launch Vehicle. 5 |; p$ x6 F ~ W! q1 @HMC&M Hazardous Material Control and Management.1 K7 o- g' c, p8 i H; Y HMI Human Machine Interface.: C( B% B4 `0 p4 l U- n HMMWV High Mobility Mutli-purpose Whealed Vehicle (USA term) (pronounced Hum Vee). 3 {. i# T) f9 {+ g- rHMPC Hazardous Maintenance Procedure Code. 9 Q* q; u) i! R1 r, e3 I/ i" lHMSC Hughes Missile System Corporation. + W" E2 a( Z+ IHOB Height of Burst.- i4 Q; `+ X) Q. }" E HOE OBSOLETE. Homing Overlay Experiment. (Predecessor program to 0 A3 x/ B" a7 J$ }Exoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS).)! \: G. }- L; E$ x, S9 P9 l: \ HOL High Order Language. : X7 f K: y4 S0 V# zMDA GLOSSARY, VER. 4.0 H & H2 [. U+ C+ r0 {. e/ J, f1284 \: C6 R- i9 U- X Homing All-the-9 @9 O T( L6 f6 d* P) ] Way Killer$ S0 r' w3 z* h8 X9 n (HAWK) 5 v' U' \2 h' V* E. B7 ~(1) Upgrades to the HAWK interceptor and radar system to provide the ' _: R8 Q( {2 E% I/ _Marine Corps with a mobile point theater ballistic missile defense . @$ h6 O1 |: r7 U7 Icapability. # O/ `2 I! Z8 p3 e(2) A mobile air defense artillery, surface-to-air missile system that provides / x1 s& X ~( ]2 ?2 Knon-nuclear, low to medium altitude air defense coverage for ground# p) H- @0 B4 i3 ]7 T forces. Designated as MIM-23. 7 r2 A! g: G( Z9 L1 p X/ B% d3 }Homing Device A device, mounted on a missile, to aid its guidance to a target. The homing( |: b. h6 S" w# |$ K- a9 N device uses sensors to detect the position of, or to help predict the future 6 A$ r* s% Z- _position of a target, and then directs the missile to intercept it. The homing( C# {$ R, y/ O& j! P device usually provides frequent target position updates during the flight of the( B; Y; r6 z; Q% J8 F+ N missile.( P0 Y! Q4 S3 [3 w Homing $ U" l9 \7 |. e8 C- BGuidance + g6 d8 H+ Z4 W" n( g& S6 NA system by which a missile steers itself towards a target by means of a selfcontained mechanism which is activated by some distinguishing characteristics of : T7 }0 C/ U9 ^5 a; u- wthe target, such as an infrared signature.! y' v9 G( x# _2 s; T; Q HOMS Homing Overlay Mission Simulation. 8 `: Q2 f6 F( A. pHOST Hardened Optical Sensor Testbed.& K" [2 f8 C% p6 H; N5 Z2 K6 I Host Installation A designated DoD facility that provides non peculiar SDS support of SDS0 O$ d1 M! T, t; y3 x elements.+ l5 ~" o( Q& w4 t7 z0 d$ A Hostile . d3 A0 B/ a' |5 x, dEnvironment0 n% g7 d: W9 @. P Those environments that result from a BMD system engagement of an enemy1 J% K( p+ m0 W6 f# i: M( q8 p threat or collateral conditions resulting from deliberate hostilities. Hostile : {3 r: C* T5 Aenvironment categories currently applicable to National Missile Defense are h# U+ b m. u3 c Nuclear, Battle Debris, and Electronic Warfare.2 B' n6 |+ u2 t2 J% E; H4 U- @ Hostile Track The classification assigned to a track that, based upon established criteria, is6 Q! W& z) d8 h determined to be an enemy threat. 8 i/ R* _9 a. fHost Interface The interface between a communications processor and a host computer. ' b+ A$ _4 j5 q* g7 BHost Nation" N; B$ {; C) |5 f& T) z' f Support, _: X- J3 W' j Civil and/or military assistance rendered by a nation to foreign forces within its9 u U% r4 h, X territory during peacetime, crisis or emergencies, or war based on agreements ) ?: i/ w% W1 _7 ~concluded between nations.$ i0 S3 |+ }2 p t i+ q hp Horsepower. ; @7 d8 S8 y4 @9 Z; x# THPA High Power Amplifier.6 Y4 r$ k$ i5 W- f1 K, e HPC High Performance Computing. 7 I5 x% l6 e3 x# z8 d( xHPCC High Performance Computing and Communications. 1 ^2 x/ c: e& U) U. ~! O4 g8 OHPG Homopolar Generator. : `) o7 v( U& p* m3 E0 iHPI High Power Illuminator (Hawk).0 y2 @ A5 Y, ` HPIR High Power Illuminator Radar. ! A- ?! b X G, g1 RHPL High Power Laser.5 |+ C$ ~+ X3 s7 k HPM High Power Microwave. 5 }; ~0 H8 e6 o! w+ y7 z2 s, k7 ?HQ Headquarters.5 s: b7 G9 B! b1 Z' S# g. l' {9 P MDA GLOSSARY, VER. 4.0 H* b i& ^' ?( E5 `( x: j 129 , s1 e& D V3 ?& x( XHQMC Headquarters, Marine Corps. 4 X1 f: [0 r% }0 L' }4 s# V) zHRDS High Resolution Display System.% n3 O% E+ n2 z& q7 F4 I4 i HREPS Heavy Replicas.; _% N+ q' q$ g4 g# h HRR High Range Resolution.* l# H: h p$ P0 U1 l! s HRSA HICTB Requirements, Support and Analysis. ( J7 N2 g$ t, Q% m% N2 {+ i! [HSDB High Speed Data Bus (TelComm/Computer term).8 g7 r& g+ \& [' c5 T# v HSFB High Speed Fleet Broadcast (Navy term). & W% e* A; S, W+ ]HSI Human Systems Integration. - X; i0 j( Q2 ?1 K$ M, b1 zHSV Huntsville, Alabama. % V& L8 c6 u" u; K+ w8 vHTICIA High Technology Crime Investigation Association.3 Q8 T3 o1 w X: v' v/ Z1 }% u* { HTI Horizontal Technology Initiative., U' D( U& {) [# b, a e HTK Hit-to-Kill. + m/ c/ y6 X! b' U7 [/ T7 l( a ^2 }HTMIAC High Temperature Materials Information Analysis Center. 0 C y( b( ~9 e9 p1 W; ]HTML Hypertext Markup Language. ' {6 X6 t$ o& e! q, wHTPB Hydroxy-Terminated Poly Butadiene., T8 S; ]7 J% s p1 f) u HTS (1) High Temperature Super-conducting. (2) Hawaii Tracking Station. 7 C6 T8 I. K" m7 Z6 wHTSA Host Tenant Support Agreement. ) O/ Q% V5 f- kHTSS Hardened- sub-miniature Telemetry and Sensor System.3 G' J' c2 v9 V% M) V% i* } HTTP Hypertext Transfer Protocol.1 d {% B/ X2 ^( ?+ y HUD Heads Up Display. ( c& L1 v9 d; u/ hHuman Factors A body of scientific facts about human characteristics. The term covers all & p1 v" W, s, ^0 |biomedical and psychosocial considerations; it includes, but is not limited to, - y) F. }$ C. R* \% q4 \" r- Wprinciples and applications in the areas of human engineering, personnel- {& @9 L1 c/ ^% Y selection, training, life support, job performance aids, and human performance; e2 H+ b# b( u, ~" Y evaluation.' B2 ]6 W5 ~- i# |5 t6 g. W' g2 m Human Factors$ q- D2 o: G5 P# D0 U8 G% G Engineering4 ~0 ?! F8 H2 B The design of man-made devices, systems, and environments to enhance their ; u3 Z( d9 `% Z+ W: ?9 K0 guse by people. Also called human engineering, human factors, and ergonomics.

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