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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." b- y+ `" D6 W( j ELS Earth Limb Sensor. 3 r* l* t, V) ^* F/ a! n; WELSEC Electronics Security. # `1 v+ J0 a) f" f0 mELSI Enhanced Longwave Spectrometer Imager. 3 M* g6 T8 a0 u* h& S; }- lELV Expendable Launch Vehicle. 7 F. T' q5 @8 @9 L! y. l* MEmanations 1 s/ C& t3 O6 B+ J- oSecurity& Q3 G$ w3 D' J: i/ o1 w8 K- @1 Y (EMSEC): c' Z/ N% D- r+ y$ K The protection that results from all measures designed to deny unauthorized 0 [5 @4 T* ], z* ^6 j6 Q3 U( Ipersons information of value that might be derived from intercept and analysis of! A R l/ k" P, h( k. D; c compromising emanations./ V. q; u: j# h/ ], r3 M EMC (1) Electromagnetic Compatibility. (2) Early Midcourse.( X) ~$ k* C1 W- B2 Z' U# B EMCON Emission Control/ U2 V: D, V+ } EMD Engineering and Manufacturing Development (previously referred to as FSD).' O6 `& t) g1 d7 v6 Q" ^8 X! Z; X( g* V EMDCT Expanded Memory DCT. 7 @1 }) }. C1 dEME Electromagnetic Environment. 6 ~: T& m/ F F9 T1 O; Q$ v gMDA GLOSSARY, VER. 4.0 E 6 |/ G9 D7 l$ v7 X6 J+ J' Z939 D4 \+ I: E- f. l, W' ^ _ @ Emergency% R+ m$ y% }% g% m! B) B Capability ) u* ^3 B( H0 V7 G; t" c" w6 K N7 o(replaces & s7 Z6 l* x: o1 d0 R+ tContingency: u' y+ F/ W7 @ Capability)4 t: m$ B6 D$ ?( l BMDS elements or components that are still in development or testing that& h& H% R7 N% D provide limited ballistic missile defense capabilities. MDA, working with the0 m* u7 G; H8 T4 _8 b3 V* K Services, will develop plans, which cover the potential use of prototypes and test+ J9 x) l: }4 y( P# R7 X3 `, K. l assets for contingency deployment should the SECDEF determine that an) Y" I, T3 G# q# H) A" |2 d6 I emerging BMD threat requires emergency fielding of a BMDS capability.' B+ u/ N& }. ^5 n" Y! Y EMF Electromagnetic Field. 0 S1 y- T9 R' H9 ^! SEMG Electromagnetic Gun. 3 M( W+ s3 W7 g2 S0 q- G2 w; K0 tEMI Electromagnetic Interference. 1 C& B6 s' h* S- x- m7 p, _' EEMIP See Exoatmospheric Midcourse Interceptor Program.: b$ R3 `4 ^) s$ a6 u: K Emission Control 4 A/ ?1 `& X3 d, G8 E3 s# m(EMCON) . U0 E% I/ h* aThe selective and controlled use of electromagnetic, acoustic, or other emitters; r3 `! @9 h9 }& x2 V3 t1 E, F to optimize command and control capabilities while minimizing: a) detection by : | O: Y6 B) I3 I2 _1 P0 @* aenemy sensors, and b) mutual interference among friendly systems. EMCON , [5 i4 X3 E. V3 Q, I l# Vcan also be involved in military deception plans. Also called EMCON. - n/ I, b5 a: j) IEML Electromagnetic Launcher. A device used to launch hypervelocity particles. 8 \& @& R& w: b, M( x: _2 hEMP Electromagnetic Pulse. ^3 J5 R" p6 H, n6 v m EMPSKD Employment Scheduling (USN term). ' X+ d4 R% R# T" }EMR Electromagnetic Radiation.; v* @4 C4 p* Q) K3 z; J/ ^( D( L+ p EMRLD Excimer Moderate Power Raman-Shifted Laser Device.- z. A3 d1 s" ^4 \ EMSEC Emanations Security.8 Z+ w) }) _$ ^' J- y0 t" b7 ^ EMSP Enhanced Modular Signal Processor.7 k* o. `, J6 U9 b( Z) I% X1 M EMT Engineering Management Team.) d" d1 N# l6 j" l* _; Y j( ^ EMV Electromagnetic Vulnerability.+ O L% S* q' P, p; Q& w, @8 l1 g ENA Engineering: Architecture and Analysis. ( h! U6 d6 _/ z3 E6 gENCATT Engineer CATT (US Army term). 7 a, \! i( ^" }' N. eEnclave Isolated resource – an SDS asset that has lost connectivity with other SDS 0 H* U }3 q# `6 ]assets with which it normally has connectivity, but is still capable of coordinating $ g) ]6 N8 l/ x0 Q& q8 Rwith SDS assets to conduct ballistic missile defense. Various combinations of2 i3 }8 `, {& d/ b% N _$ s. o connectivity losses are possible; for example, (1) an operations center has lost# q# p# l+ Q* K! z: G- S% J- L/ U connectivity with Higher Authority, yet can still provide sufficient C2 and can still , a5 ]$ t% B# Aconnect with sufficient weapons and sensors to conduct an engagement and (2) ) ~+ ?/ x' o; e1 o# \; v$ |% D6 ^an operations center has loss of connectivity with another operations center with2 S! X, c- s8 _, d7 }" x5 r which it normally shares data, but can still conduct an engagement. ' x/ i5 I+ v" t7 h" c ?* ?4 yEndgame FOV The field of view of the interceptor’s sensor during its final maneuvers after target + G ~% e5 A' x/ D; {, \0 iacquisition to intercept the target. May be less than the acquisition FOV.3 k7 O `4 z" | End Item The final production product when assembled, or completed, and ready for% l* h; D3 v% R* r issue/deployment. / I' |' U5 O6 f) b; F* A/ LMDA GLOSSARY, VER. 4.0 E4 s) O" W3 T* j! r& E0 W) f 94 . L4 @7 `: l- p( MEndoatmospheric Within the earth’s atmosphere; generally considered to be altitudes below 100 : l6 M3 a" ]. O; ?km. An endoatmospheric interceptor reaches its target within the atmosphere. $ l9 S/ W6 j6 l6 L& c9 |! o" b H9 G& \5 FEndo-7 Y9 X- ?; Y8 H( }2 \9 T( i" Q0 } Exoatmospheric & B) q2 @$ Y7 g5 M5 I- u* MInterceptor (E2 I)! B6 q$ O+ x4 I+ [6 F, V, S A ground-based interceptor capable of engaging RVs either endoatmospheric or " @) C& z) Z8 `) x2 ^3 P% ^4 G7 E0 ?exoatmospheric. (Successor to High Endoatmospheric Defense Interceptor; _% g* r3 J8 R6 L (HEDI).) 8 Y" V+ ` I) x( I. DENDOSIM Endoatmospheric Simulation. : }& [4 e- E5 a1 {" |4 hEndurance The time an aircraft can continue flying, or a ground vehicle or ship can continue 1 V- n/ L2 L) r, P! Y6 y3 a4 yoperating, under specified conditions, e.g. without refueling./ R/ M, s! }. Y" a ENG Engineering.$ M/ x2 j. A1 } M8 X' {) I- V ENGAG’T Engagement.$ N1 Y0 C/ r* r Engage (1) In air defense, a fire control order used to direct or authorize units and/or 5 r: a4 |1 x+ ?( K& Oweapon systems to fire on a designated target. 6 [: K* l) Z2 m3 ~2 K(2) In air intercept, a code meaning, “Attack designated contact.”/ N! E$ w, j, o p& E l Engagement (1) A period of hostilities beginning when the first ballistic missile target 1 C3 }9 ?- @% E6 Tundergoes fire from the first defensive weapon. ; u- J" ~% t9 X, Z(2) A period beginning whenever any hostile object is identified (designated)- e5 f& r9 g3 h- } as hostile and ending after the last hostile object has been attacked. 0 `! u/ {8 O7 j1 ^" p, M* O(3) In air defense, an attack with guns or air-to-air missiles by an interceptor0 w" [) @1 O: L) r aircraft, or the launch of an air defense missile by air defense artillery and & z. g2 K* w, |. x% p* qthe missile’s subsequent travel to intercept. 9 g4 i6 ^* u1 B+ fEngagement/ H: y5 l* K% e# n; y Authorization" _) a, w! P' F1 }* i9 N/ o" O The authorization given to USSPACECOM to use weapon and sensor systems 0 R- |/ t" F9 b- Junder previously coordinated and authorized rules, procedures, and conditions.7 x0 _( N9 M; {, J' B Engagement8 ?! ^4 M) l" X- g Control" ]- o9 ?5 p$ A2 J* M/ _! s (1) That set of coordination, assessment, decision, and direction functions/ B* G: }& ]2 E) ]$ Y3 w) ^& ^/ P normally implemented automatically to execute the selected battle plan, ! J: S5 K% a- G8 z: A3 ]military strategy and tactics within partitioned battle spaces (i.e., a 7 m; U- W3 r$ q5 K# |2 k* K$ A% Rspatial/functional subdivision of battle management). Includes the 2 X' K$ {. Y+ y# Gdetermination of: what specific objects to intercept in order to implement 8 X. K0 C. s. athe selected military strategy, and which specific interceptors to assign to $ T& ^; x1 q2 S2 Eeach attacker to implement the selected tactics within the rules of: A$ J# z- k# w, u4 M4 C$ [7 z& k2 E" x engagement.. P3 ~3 ]$ b: o (2) In air defense, that degree of control exercised over the operational . t& p2 T) n) V' B$ g8 yfunctions of an air defense unit that are related to detection,& D2 F: Y6 G2 n9 \- X3 @ 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 , m9 \4 q3 S& u3 MPlanning" k7 k& G; f# X' F4 A A set of rules and parameters to be used in developing weapon-target ! }/ s2 X4 {0 w" m" Oassignments and for sensor resource management. (USSPACECOM) 9 s; V$ J+ E1 Y/ _& Q" Y0 tEngagement 7 g: b0 a0 l4 t- C& j; [3 }Surveillance R- H' c2 ~8 W2 L The surveillance required to support RV negation in the midcourse tier.8 I2 a- p# m1 D7 G, n+ X Engagement 1 w; I% q0 A- O' V% sTime6 t2 E4 z8 y: x3 ~ The time that a weapon takes while engaging a given target. This includes not + G- O4 Y; W9 U/ r0 monly firing at the target but all other necessary weapon functions involved that8 @, j, a" p/ K$ d2 W7 V8 o" b are unique to that particular target.( L) ]2 e/ a2 i5 e i MDA GLOSSARY, VER. 4.0 E. t! J& e9 `, F: s2 p$ K- ]: l 95 . a& j& @6 d: k/ XEngineering and% m! @8 C" P5 N0 _ Manufacturing# s: W0 t5 @4 k. ~( Q/ a5 Q Development; v8 ]/ Q, c+ h8 Q (EMD)$ V$ t7 H! v/ Q2 h The third phase in the acquisition process, following Milestone II. The system& {* S6 s, S$ h1 q" S( _ and its supporting items are fully developed, engineered, designed, fabricated,/ r! w+ w$ X( s6 t tested, and evaluated. The intended output is a pre-production system that ' _4 D3 D, M- o! a+ o8 m1 n" Jclosely approximates the final product; the documentation necessary to enter the$ i, e8 a. q" T2 b$ i production phase, and the test results demonstrating that the production product, J, j) |' J6 @& P8 P8 @9 U, B will meet stated requirements. + X8 i1 M, }0 E3 R) {Engineering R6 j4 c6 {/ t& B' d; Q Change Proposal p2 J7 `' d4 x3 u9 j+ Y# Z(ECP)1 F2 q0 y# D( [1 v, n4 A A proposal to the responsible authority recommending that a change to an/ Z2 H' p( L' j' p0 ]2 @% g' I, a original item of equipment be considered, and the design or engineering change4 D% \) n: S, O. k) f be incorporated into the article to modify, add to, delete, or supersede original6 `9 o8 I( Z1 t1 E0 G* d parts.) f- J* m0 Z/ E1 ` Engineering: y" z$ F: b2 [5 v( P b Development, A& Z [, N: U A funding category including those development programs being engineered for; V5 B( u7 m0 _/ x; Q: t service use but which have not yet been approved for procurement or operation. 0 Q' b6 S0 ~' m" p, c- D7 eMoney under budget activity 6.4. ; B4 i! Y1 g% |1 l6 ^9 gEngineering 8 Z2 Q* A' b# f3 W0 u+ H: j. W6 d5 SDevelopment * W: \+ Z/ X9 D/ eModel % ^" J4 x, x/ K1 REnhanced Target) {8 C% J6 h* `9 } C2 J Delivery System$ k7 Z& j) |5 b$ p7 t2 d+ ^. C (ETDS) - E$ N3 u# e! P iAn advanced prototype used during the Engineering and Manufacturing # I5 b: `, |' Y2 P8 w" ODevelopment phase (EMD) to resolve design deficiencies, demonstrate maturing* |1 V5 ?( U" v8 U performance, and develop proposed production specifications and drawings.: ~! j% h! i: o Target delivery system being developed for future GMD testing that will 1 K. X# a3 Z2 v8 c4 d2 K0 |complement existing systems, provide flexible, modular configurations, and will 8 M. X' X+ }: [2 @% Ibe launchable from land, air, or sea modes/ r2 c7 w: p6 S6 N+ [8 ]8 a/ f ENNK Endoatmospheric Non-Nuclear Kill. 0 z& y1 [8 U# V9 iENSCD Enemy Situation and Correlation Division (JFACC term).. P) s/ T( d# W+ f, r. { Environmental . ], L. M& l2 v- jAssessment (EA)2 j" N4 R0 L* c2 p A concise public document whose primary purpose is to provide sufficient1 w1 A. x$ q# W# _) [- b$ X+ O analysis of environmental effects of an action to determine whether to prepare / Q. B7 q& N3 g% ^0 i. w2 Oan environmental impact statement or a finding of no significant impact. * d1 c+ E: W3 f( Q1 M" ?6 w1 EEnvironmental% F( G# p/ z; n, t7 L! w Impact Statement) u, [8 s; W' F$ M. p } (EIS) 4 W7 a1 @6 s) | M) v* JA detailed written statement analyzing the environmental effects of a major1 K7 L+ [; K6 Q/ H, b4 w Federal action. . f1 {( ]3 g Q- |Environmental 3 v. ~8 h5 |/ G+ f% ]Security' V# o% M, [7 B2 K' k) T A specialized form of physical security that prevents technical penetration, e.g.,& |; @7 g, }& K2 t2 X5 g% | penetration by waves of electron beams.1 s# R2 G$ x" y Environments The media, conditions, and/or physical objects in which a BMD asset is immersed % u' ~8 M5 u! H6 u# [: p8 wor surrounded. For BMD systems and elements, the comprehensive ) ]& q1 F! b# |environments definition consists of natural, hostile, induced, and storage, . E9 Q& y; S$ Qtransportation and handling categories. w5 ?# g4 g9 V9 t6 E: u EO (1) Electro-Optical.6 B- d6 ]1 i {; m/ g8 O6 @1 m (2) Engagement Operations. 5 \& L2 v. j# j! }' l(3) End Office." S6 Z6 N7 v/ _# D9 q5 c (4) Eyes Only.. D) z6 D& u d2 R& o V EOA Early Operational Assessment. u O+ L W- h- n EOB (1) Enemy Order of Battle.7 D3 |$ b k6 q (2) Electronic Order of Battle.5 d) q3 m, N/ ], l% X! { EOC (1) See Element Operations Center. , A5 B7 ^& Z( T* K& k* o(2) Emergency Operations Center' t, R# F4 W3 c7 X MDA GLOSSARY, VER. 4.0 E4 a/ B1 F1 |2 ^4 V7 f. Q2 ] 96 L1 B) }" a& ~+ u, }EOCM Electro-Optic Countermeasure. " N x$ Q+ m& {! K9 g! n% rEOCT Element Operations Center Test Bed.0 K$ Y' _: s# \; d( x3 V" p8 _ EOD Explosive Ordnance Detail/ k6 T( a7 z2 k0 D& C EO/IR See Electro-Optics Infrared./ K8 F) _7 K. A EOM End of Message.5 X& v" C3 V4 N* J EOP Executive Office of the President . K. W9 a8 a; p! p; W nEORSAT ELINT Ocean Reconnaissance Satellite (US).5 m# }, U% Y) h, j1 y$ S" b7 W2 d EOS Earth Orbiting System (NASA term). * v$ d1 l/ I0 _* M$ a0 oEOSH Environmental Operational Safety and Health. $ x: Q! e+ Z& I' EEP (1) Engagement Planning. (2) Evaluation Plan 5 X5 Z. Q. Y4 r2 [& fEP Cycle Engagement Planner Cycle (NMD BMC2 term). 1 o4 H, I1 Q! Q4 \3 qEPA Environmental Protection Agency.* U9 _6 `( T7 L) ^: E/ Y; Q EPD Engineering Product and Development & I! j" P+ B, A9 O2 uEphemeris/ ' m5 l$ ^* O6 Q5 o( q* [Ephemerides 6 ?9 m& B9 p( t. E* w L! q7 P B(1) A table showing the positions of an object in space at regular intervals of 5 }9 z9 q/ e, [2 Q2 P" ttime. * k! x" j: ^) F* q3 K' |* K(2) A publication giving the computed places of the celestial bodies for each * @4 g I+ M. [; D% P# C2 r/ `day of the year or for other regular intervals. A I* k/ v+ s# T/ oEPITS Essential Program Information Technology and Systems.: [* n% B7 _1 J EPL Emitter Parameter Listing (USN term).# d/ n+ o4 l( f) q& } EPLRS Enhanced Position Locator Reporting System. / \+ B0 Q5 b* B$ ]$ O# h5 OEPO (1) OBSOLETE - ERINT Project Office (US Army term). (2) Element Program$ m9 ?0 i; @9 a- I3 j6 Z, B Office.; x3 y" m5 T9 [# h% s) c EPP Electric Power Plant (PATRIOT).9 j" `$ h% N" G }! E7 u EPROM Electrically Programmable Read-Only Memory.3 h/ k# [5 z3 H, T0 D EQEC EurQuantum Electronics Conference (See CLEO). # J. ]- I1 ^! ?) T; G2 U4 S& wEquipment# n+ R2 {" |: L& _ Operationally $ a. X* N4 o* ~2 f. \Ready 3 B: L! |% H0 z0 S' p: X- u. I! RThe status of an item of equipment in the possession of an operating unit that8 X `: `& I1 ^ indicates it is capable of fulfilling its intended mission and in a system ' H! k- s& k* v4 k ^configuration that offers a high assurance of an effective, reliable, and safe6 x* {7 Y5 {- G2 B performance. % s4 Q* \6 G* @8 J- g, VER (1) Enhanced Radiation (“neutron bomb”). (2) Extended Range.# i; y5 ~& @6 c0 L S ERA Explosive Reactive Armor A# W8 g- e/ d7 S3 a- k2 ]. g ERADCOM OBSOLETE. Army Electronics Research and Development Command. (Now . v- t/ m. e9 |Laboratory Command (LABCOM), Adelphi, MD.) 9 Q/ h X2 G2 Y, b4 W' k: VMDA GLOSSARY, VER. 4.0 E 6 N3 R% r: O2 g3 c$ p! E97 4 ~; D/ K5 F7 M; D+ E3 SERCS Emergency Rocket Communications System (US).. F) m+ O3 Y2 S9 s2 v6 i" z# s ERD Element Requirements Document. 4 g& Q' N3 k" `( Z1 i0 pERG Executive Review Group." m6 |; `3 o$ n' \/ H1 W ERINT OBSOLETE. Extended Range Interceptor. Now referred to as PAC-3.4 T$ ]1 T6 w' o. t! { ERIS OBSOLETE. Exoatmospheric Reentry Vehicle Interceptor Subsystem. " e7 \* g/ q9 @2 o, P) x: \& a! v(Predecessor to Ground-Based Interceptor (GBI).), u5 i0 n. N. v) K8 _7 z ERIS(F) OBSOLETE. ERIS Farm. % Y& C& R6 q; J! ]ERP Emitted Radiative Power.9 ?* p; y* x$ L; {! |. x ERR (1) Element Requirements Review. (2) Engineering Release Record. * d) O" e! I ]: @3 X/ E% k. NERS (1) Early Release of Submunitions. (2) Emergency Response System.- w4 t3 s. n+ F5 ]: e; j ESA Electronically Scanned Array. 7 u* m5 t9 ]7 k% k2 m2 F9 y" bESAD Electronic Safe and Arm Device. 9 k% V& L$ ?- c0 a& N* S" bESAR Extended Subsequent Application Review. % M6 g4 H( U4 W6 U7 yESC Electronic System Center (AFMC), Hanscom AFB, MA.# D5 o- Y+ A8 H3 k/ d ESCN Existing Systems and Center Notebook. . G8 R' m2 e- C; @( a5 `4 BESD OBSOLETE. Electronic Systems Division. (Now Electronic Systems Center,6 b) Z+ a: I! S1 b. V, y4 R Hanscom AFB, MA.)' l0 Y' d' z& O% [8 L7 P: _. j- X ESH Environmental, Safety and Health4 U0 e/ T9 _+ Y$ E5 B$ i" b ESI External Systems Integration. & n% k) Y3 E5 V$ A4 [ESI ICD External Systems Integration Interface Control Document.; T# c# G0 B+ A! x' A1 \4 ? ESM (1) Electronic Warfare Support Measures. (2) Electronic Support Measures.( ~6 v. a0 b* o# T9 L, w2 n ESMC Eastern Space and Missile Center, Patrick AFB, FL. 5 z3 n1 I0 c6 u9 CESNet Energy Sciences Network. . C8 f" F" x' X, ~% C$ oESPRIT European Strategic Program of Research in Information Technology.# x. n/ B+ Y2 n& S) @" b ESQD Explosive Safety Quantity Distance. % p2 s+ F; C6 K( ]ESSM Evolved (Enhanced) Sea Sparrow Missile. ) n& w( p7 F! {/ N+ \, AET&C Extended Tracking and Control., `" l2 |6 v" R: c ETA Estimated Time of Arrival. 6 U" x: b3 ]8 J2 i: H$ ?! Z @; KETC (1) Electro-Thermal Chemical. (2) Estimated Time-to-Completion.4 N4 p# A( z+ T% i" Y. o4 U ETD (1) Estimated Time of Departure. (2) Electronic Transfer Device. % e( R s$ H& I) h& |+ X+ iMDA GLOSSARY, VER. 4.0 E3 Q3 u' P4 Q: J 98% H, u* i. s" b( E ETERTS End-to-End Real Time Simulator.( S6 x5 r& v% V ETESD End-to-End Sensor Demonstration.- F, e2 {* E, a4 `$ q ETI Estimated Time of Intercept.7 f+ L+ h: @2 `. L ETIC Estimated Time for Completion.: F: g6 y' G. F! Q E ETM Engineering Test Model 6 [6 p0 M0 E; N2 G8 [" O/ t3 p2 pETR (1) Extended Test Range (Pacific Test Bed) (2) See Eastern Test Range. (3): H2 `( y" b7 X( S9 q) A0 a( U6 \ Environmental Test Round. (4) Estimated Time to Repair.+ q, a. N2 C' e. [ ETS (1) Experimental Test System. (2) Experimental Test Site. 7 Q) P& Y! T+ Q K4 I: h& N) xEU European Union [formerly European Community (ECI)]9 [: L, L0 |2 l6 s EUCOM European Command. See USEUCOM.3 H) O" \; b7 p) t6 v EURATOM European Atomic Energy Agency. v+ `7 }0 P2 {4 tEUREKA European Research and Coordinating Agency.' ?4 k+ ]8 n& J) h EUT Early User Test. [, H, S- G7 S: L EV Experimental Version ) A8 c3 T4 @( M; g }# v+ P% }EVA Extravehicular Activity. ; {+ n' D7 w1 \$ }( ]6 I* m( G" q/ nEvasive MRV A reentry vehicle, which maneuvers for the purpose of evading defensive" G' C- P- W! o; l, w' f! p weapons.. d& M! J* Y) w" H5 { Event Based & S* Y3 S: ]! `4 H3 tContracting( X* ?9 W$ a& y! c$ N. |# H- L Support “event driven acquisition strategy” by linking specific contractual events O* z& K ^6 q# B/ `! N, {: l0 G to the “exit criteria” for the acquisition phase, or to intermediate development & g* r' \# `. S. N8 F0 V4 Z2 P, l- Nevents established for the acquisition strategy. . e @0 {/ D, g3 H( c) Z" uEvent Driven # r' S: [) B+ g5 B" bAcquisition ) A7 e- K O# P7 |1 a6 x% e, ?Strategy( h' i( p; m" J; C8 M8 H, E An acquisition strategy that links program decisions to demonstrated 9 X. @9 F+ U+ kaccomplishments in development, testing, and production.. a0 w! n y: j+ j9 Y# n: V Event Validation A sensor element internal process that results in a determination by the operator 1 U f& Y6 _) Z4 F+ Sthat 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; A0 p9 ]! g0 {* L% R7 J Verification - a5 ~4 \# T) n+ o+ H# i& X7 v( ], lThe process by which it is decided, from SDS external data, that the event ! `. z7 z/ m! F5 O0 hreported is real.0 z9 L+ h% X% l' v, T+ u+ D MDA GLOSSARY, VER. 4.0 E , O }( ^" N- O: M# _99 6 E- R& G {- O" ~* m+ YEvolutionary 9 |( G+ P7 u x* M9 R* lAcquisition $ @. a5 @. b; a) [: E7 X(1) An approach in which a core capability is fielded, and the system design has ' D4 ?7 E/ N6 R+ E6 Z* s" _0 z/ Ga modular structure and provisions for future upgrades and changes as 9 k6 I3 G. M! s( H7 _% Vrequirements are refined. An evolutionary acquisition strategy is well suited to/ U% Q8 |# u* h" a high technology and software intensive programs where requirements beyond a / b2 ]0 ?. T1 d5 jcore capability can be generally, but not specifically, be defined. w8 e, w- N3 q8 P(2) An acquisition strategy that defines, develops, produces or acquires, and. z% P0 z5 A+ ~: M3 h5 ^ fields an initial hardware or software increment (or block) of operational capability.) T/ h' C3 A6 e8 G3 O It is based on technologies demonstrated in relevant environments, time-phased ! D: [( @/ V1 X {+ m* f* f4 Krequirements, and demonstrated manufacturing or software deployment! c: p2 [/ J( Q" g0 W capabilities. These capabilities can be provided in a shorter period of time,4 N) i' j7 C7 J/ y followed by subsequent increments of capability over time that accommodate: _! K* D2 E( I improved technology and allowing for full and adaptable systems over time. Each) z5 i# E$ |3 l5 e+ E8 h+ M increment will meet a militarily useful capability specified by the user (i.e., at least ! W, o% P$ K7 t$ M" U: `# ], I5 N A1 Wthe thresholds set by the user for that increment); however, the first increment" r& H# `8 @- O7 r may represent only 60% to 80% of the desired final capability. (MDA Lexicon)+ r/ c$ T9 w" ^, L h. Q6 f Evolutionary w* m9 k3 }$ \: h, K. wRequirements 3 a" p, H8 R: o( MDefinition ( C* d( F2 `3 b$ j* `9 T0 nMission needs are first expressed in broad operational capability terms, and then & o: u# Q- `. U, ]; yprogressively evolved to system specific performance requirements. 4 Q4 p/ J0 A- h; M9 o8 d5 L/ a$ EEVPA Experimental Version Performance Assessment. : k) m; B5 k+ p& V3 NEVPA/TEVS Experimental Version Performance Assessment Test Environment System. O5 J" X3 h( b0 I) z% c) u! V* PEVS Enhanced Verdin System., y* h) w4 T& B" g% @4 D EW (1) Electronic Warfare. (2) Early Warning. / X3 M% k7 L% F8 \$ ?2 A4 u/ IEW/AA Early Warning and Attack Assessment. 1 {9 m6 c7 D6 e9 v7 m% qEWCC Expanded Weapons Control Computer (PATRIOT). ! n% K" {3 T. o- hEWDA Energy and Water Development Appropriations (US). , T/ l$ y7 o6 K6 y0 m4 f# {; j6 |: OEWG Event Working Group. , E. J( d( s; LEWN Early Warning Net., d a$ _' o+ Q# X6 i. H EWO Electronic Warfare Officer.- V4 {4 G5 a- {( G) Q' C EWPE Electronic Warfare Pre-Processing Element.9 F( [8 q; v' O0 c0 K EWR Early Warning Radar. N4 I2 t1 B' x6 u EWS Early Warning System. : o" x4 g' d% u6 x4 VEXCEDE Electron Accelerator Experiment.8 v1 P4 h/ j& e, v Excimer A contraction for “excited dimer”; a type of lasant. A dimer is a molecule ! ^/ F' G6 i6 z9 ~, ~7 s# tconsisting of two atoms. Some dimers (e.g., xenon chloride and krypton fluoride)- `3 o9 d3 {5 m8 E are molecules, which cannot exist under ordinary conditions of approximate7 Y" D/ m. [+ h) h thermal equilibrium but must be created in an “excited” (e.g., energized) condition - S! r( D6 i; n0 v/ e# x6 c2 @by special “pumping” processes in a laser. ; [( z2 J" i/ d/ p) |( bExcimer Laser ! x! I( a% H- G(EXL) " G! E0 K5 c0 y4 c5 D- ?9 jA laser in which emission is stimulated when a gas is shocked with electrical8 @. N5 a7 H6 ]6 Y& q, H( M energy and the excited medium emits light when returning to a ground state. / v7 p# S- v7 x* BMDA GLOSSARY, VER. 4.0 E7 Q! w# P: ?' W 100 / W9 p% H7 H% ?; ]8 a0 QEXCOM Executive Committee. " H, d) K: i8 g$ i {5 hExecutable; \+ y7 `' T1 V! h# n Program ( q0 K9 W* F$ w; ~. L8 N s* i) j1 hA program is executable if the PM has adequate near-term approved funding. , Y* i- p r4 y% QExecuting Agent The individual within the executing element assigned responsibility for managing( \# H% k* }' @* K7 m8 P2 z. M; Q MDA funded programs. 7 ~9 q6 [4 H6 {1 [. cExecuting ( m% H# w2 y# N4 W3 mElements 9 I! H- X. B* u+ q! aAgencies or organizations (DoD or non-DoD) that are managing BMD-related " ~9 M: h, \7 P1 Rprograms.) X. g# I' ]' ^8 J& L8 S: h' l9 s Executing) g% Z. |" a6 N* u3 @* ~ Responsibility 6 j- I3 q* s3 X4 V) kProgram Manager responsibility. : T9 L) a3 @8 c1 P6 f# IExercise A military maneuver or simulated wartime operation involving planning, , R- {& A: a/ Upreparation, and execution. It is carried out for the purpose of training and" J; K5 m) W7 ] J; n0 d7 G6 o' u evaluation. It may be a combined, joint, or single-Service exercise, depending6 a" ~% M5 A8 F& n. @( s2 A* ^ on participating organizations. See also Command Post Exercise. ( D6 \& [# e- E/ s1 P+ {# F* IExit Criteria Program specific accomplishments that must be satisfactorily demonstrated 4 l1 S4 a" R0 f: Cbefore an effort or program can progress further in the current acquisition phase / f; s! |- J- ^+ ]- v D! Y; N- Uor transition to the next acquisition phase. Exit criteria may include such factors ( [& W/ P: N2 {5 O: \as critical test issues, the attainment of projected growth curves and baseline* M9 v; h& j$ y( U. N3 Q parameters, and the results of risk reduction efforts deemed critical to the 1 F( J3 j: W/ ]9 @decision to proceed further. Exit criteria supplement minimum required . t9 q' ^7 {" s: A6 I/ Iaccomplishments and are specific to each acquisition phase. ! p' m/ H# O+ ?% S1 hEXL Excimer Laser.4 R6 e R! D/ L [! M( j& Y Exoatmospheric Outside the Earth’s atmosphere; generally considered to be altitudes above 100 " a8 u4 S9 L: Jkm.4 y. i; _& \; g. j$ p! q1 x/ c Exoatmospheric & S/ L& D6 @9 X: S% G9 wReentry Vehicle # M, G) m5 t# V: {& fInterceptor) p6 n x) f8 O; r9 Y5 v+ K3 U Subsystem) H( y3 H; H7 I$ H% n7 {1 } (ERIS)' f' `$ u. l$ p OBSOLETE. Interceptor designed to provide functional test validation of GBI.8 s5 U( F& p+ ~% y7 N$ M Exoatmospheric$ X8 Q. c- G, d. i Test Bed (XTB) 4 i3 M$ L; d4 y, n- W, xFlight qualified and range integrated vehicle to support other programs such as ) ?4 N- F D6 e7 ]GBI-X.8 f T, M$ M+ f0 B. A* S Exo Decoy A decoy that matches RV signature exoatmospherically. Exo decoys can use ( @* U/ t1 D+ t( u6 c( Tradar and/or optical means to deceive sensors.* @ I0 t- F5 z6 p7 x4 ]/ T4 k' T Expert Systems Software programs, which use artificial intelligence techniques to capture and4 x) t# I9 }$ J) b& c* a7 _4 I apply the non-algorithmic knowledge and procedures of human experts. ; ?" l: F5 T. {Expired ) K5 |3 v2 h! T; R* r* i1 N' e/ H. eAppropriation 9 ]9 G- Q: L% e' i! W+ M9 o1 j" lAn appropriation that is no longer available for new obligation but is still available: J' W5 N& f, J2 h) g8 l for disbursement to liquidate existing obligations. Under current legislation no ; e0 Y& E8 L" U5 S O. ~* Ndisbursement may be recorded or paid after a five-year expiration period.' B5 U- v6 A2 h8 t5 L2 o Maintains all original accounting identity, e.g. FY, appropriation, PE, etc.0 W' ^. \- K9 |) _: h EXPLAN Exercise Plan.6 |/ y" ^! \2 T8 U: c Explicit 4 a+ v5 P# a+ J/ cCoordination2 ?8 x! o. ^, ~; u% y A battle management technique which communicates results, decisions or 0 H# E4 |& y& E* h$ N/ mcommand from one battle manager to another, usually from a higher command3 V' c; w4 p$ e. g, n9 v to a lower command.' x5 ?2 a' Q4 v" x/ I7 `& I MDA GLOSSARY, VER. 4.0 E# F1 S/ F& x* e4 s 101+ g D- h/ [( H/ `- u Extended 8 j2 T5 v# _ c; M X. ]- LPlanning Annex: i Z+ }: b. B/ O0 t/ g7 T A document providing program guidance for an additional 10 years beyond the% W% n; r7 [. D% e POM. + N4 i( b# i: ^MDA GLOSSARY, VER. 4.0 F 9 j B) H& |" n$ n. Q# N103 " Q7 X0 g% m- g# g5 O$ r2 |1 p, xF (1) Fluoride. (2) Fahrenheit.. j3 V: z7 ~2 A: l. s F/O (1) Fiber Optic. (2) Follow-On.- f9 h# {/ K' C0 F. v FA (1) Field Artillery. (2) Feasibility Assessment.0 R9 ?$ Z) d3 S+ _) b) f' y$ J FA/RD Functional Analysis/Requirements Definition. 0 @/ `9 [. j9 Y2 UFAA Federal Aviation Administration.3 {0 w: @6 Z6 | FAAD Forward Area Air Defense (US Army). 9 a7 e' I0 X T% IFAAD C2I Forward Area Air Defense Command, Control and Intelligence. * j1 v$ S* D+ t1 ]4 u- N, KFAADS Forward Area Air Defense System (JCS term). 2 r6 E4 ]3 j8 C1 P( sFAAWC Fleet/Force Anti-Air Warfare Commander. ' @; n- l, D/ TFAB Fly Along Probe.( G% E8 q/ v7 I7 |. j Fac Facility (MILCON term). ) n4 L$ K# B6 r0 y7 G/ f* O; xFACP Forward Area Control Post (JFACC term). , J; |! F6 o u2 w+ `9 y, m$ _. EFACSPMF Federal Agency Computer Security Program Manager’s Forum.$ c4 u) {4 `6 z% W( N1 L% y FAD (1) Force Activity Designator. (2) Feasible Test Date. : [( {3 {, r' L- K1 i) XFADEC Full-Authority Electronic Controls. 4 N+ r! y3 o/ O6 S2 v. g( i- }FAFB Falcon AFB, CO. 0 ?) e. t+ @7 l$ f- i& fFAFBR Falcon AFB Regulation+ P: N- D7 d5 G Fairing Structure to protect the payload during ascent phase. / x. y: {/ |0 ^; [" rFAIT Fabrication Assembly, Inspection/Integration, and Test. + k& [9 M/ X8 h, {' G5 @FALCON Fission-Activated Light Concept.' }& q8 S8 }6 n9 L% }3 M FAM Functional Area Management.! O I' {; }$ y8 a8 ^ FAMIS Financial Accounting Management Information System. 2 s$ @( {" N+ \& [# y! K) YFAMP Facilities Acquisition Management Plan.7 ?6 c7 D4 H2 |& T FAMSIM Family of Simulations (USA term).' O5 f& X* |& r FAR See Federal Acquisition Regulation.! W# r! m/ k8 c5 Z Far Field The region far from an antenna compared to the dimensions of the antenna and , e$ q# L8 N1 `" r2 ~4 `: Pthe wavelength of the radiation. 5 q, u2 j1 o/ L. w# s6 `FAS (1) Fly Away Sensor (TCMP). 8 e! Y4 Q0 n. e& P( k& ]) \5 e(2) Federation of American Scientists.* a2 g7 Z: B& A! ^; @1 S |( I FAST Facility Allocation Study Team.7 H# ]& Z Y; z) F3 U MDA GLOSSARY, VER. 4.0 F" r/ N" O# \4 R0 W$ X! S$ t 104 ' R% C+ W; b: N% e) M9 aFast-Burn ! g& q7 C3 l: U5 f+ M0 zBooster (FBB)7 _1 J+ G! G0 d, [& G. Q A ballistic missile that burns out much more quickly than current versions,* R) p5 @% ^7 F; {4 K: } possibly before exiting the atmosphere entirely. Such rapid burnout complicates" h. }2 |: H, e; W a boost-phase defense.4 @& X# K& p: z: ] FAT (1) First Article Testing. (2) Factory Acceptance Test.3 r. T, {) K& T- i4 t: @2 A Fault Tolerance The ability of a processor to maintain mission effectiveness after some) h" z* q2 ]4 u9 x subsystems failed.5 w+ w* t7 y, n. A Fax Facsimile./ z% |1 J4 V" A0 q FBB Fast-Burn Booster. 8 k$ A7 H! _* k& W [3 Z$ i, MFBIS Foreign Broadcast Information Service (US).+ T* [2 t; ?" Z7 i2 n& N6 b FBM Fleet Ballistic Missile. " @4 J0 _) q8 m2 t5 |3 b9 X; n8 dFBMS Fleet Ballistic Missile System (USN term). % E [; ?+ h: q* G& AFBP Forward Based Probe.; q9 \6 Y" U$ g! O' T FBR Forward-Based Radar (US Army term)./ H. B) L9 ]( l+ q7 X: v5 h FBS Forward-Based System. 4 f, B3 {* H; Q1 y7 NFBXR Forward-Based X-band Radar.. ?' M% t# O2 v+ M6 Q% V8 a- r FC (1) Fire Control [of weapons]. & e: t& b( }' K(2) Fund Code.1 ~% J7 ~; i7 K5 n% T FCA Functional Configuration Audit. : u+ |0 r& F. [) cFCC Federal Communications Commission. 5 n7 R3 ^1 \+ c4 XFCCM Facilities Capital Cost of Money. 3 O- D2 ?/ @% }8 QFCN Fully Connected Network. % a9 j4 ~2 ]$ J7 {+ g) P" k% S- A' k2 eFCO Field Change Order. D Y; X4 M: E2 l3 R9 D' iFCRC OBSOLETE. Federal Contract Research Center.5 T4 G. M/ g+ N% m/ v) R FCS Fire Control Section.

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FCT Foreign comparative testing. 5 a) F) @- w5 L; A) i& zFD First Deployment.0 K0 f' b& ?# a4 B FDA Food and Drug Administration.3 X1 d* [ a0 Y7 P' r8 a9 R/ I FDC Fire [of weapons] Direction Center. / Y1 o1 @. {0 g; l% k4 @FDG Foreign Disclosure Guide. E. c4 s' @. Q' a/ j" Y2 o2 B" IFDM Function Description Manual. * F+ ~* n( i3 d3 P4 YFDO Fee Determining Official. 3 k# F# `4 C. F& ?% F" qMDA GLOSSARY, VER. 4.0 F% w L e1 ~5 u* A 105 ( _6 E( E* f( ?! U+ SFDP Flight Demonstration Program.+ a! \. g# h( l FDR Final/Formal Design Review. ' q, f1 ]8 a- |! v: tFDRU Final Design Review Update (MDA PAC term). # U, O0 ?& ^; w2 s6 c m. OFDS (1) Flight Demonstration System. (2) Fault Detection System. 6 ~2 ?/ ]0 L5 s" mFDSV Flight Demonstration Space Vehicle.* W v, {! a" u, M& O3 ^% ? FDT&E See Force Development Test and Experimentation (US Army).3 s z1 A8 ]7 H0 m. b* m FDX Full Duplex (Telecomm/Computer term).3 H7 ^3 m" g- A4 U! K; _/ E FEA Functional Economic Analysis.0 A5 T; A- U& [1 f i# O3 ?$ P Feasibility Study A study of the applicability or desirability of any management or procedural! Q4 D1 x M2 r, Y0 D system from the standpoint of advantages versus disadvantages in any given ( f( S% e- Z w8 c+ ccase. 6 n9 k* q( _) r6 L5 HFEBA Forward Edge of the Battle Area.! y$ E2 G7 \. p6 B) S, x- j4 s FECA Front-End Cost Analysis& D0 ^8 p. g0 Q7 h! y4 u$ R FED Federal. l7 q1 f, y! T; h" _! k2 VFEDAC Federal Computer Acquisition Center. 9 u" [; \: S) X# J& OFederal ; u( g7 l) m F1 R2 }7 \Acquisition + ~3 e2 f4 I% Z% t8 O6 s' f9 n6 ]Regulation 4 p+ K' X! p/ o0 [The primary regulation for use by federal executive agencies for acquisition of1 ` M6 O5 k7 I Y supplies and services with appropriated funds. It directs the defense program# B5 ^) s- @1 y7 O' N) u manager in many ways, including contract award procedures, acquisition# D% ]4 v! N5 g2 y) j, K4 w7 A planning, warranties, and establishing guidelines for competition. The Military9 a3 X! X4 V0 g; @ Departments and DoD issue supplements to the FAR. The DoD supplement is" w6 j- V/ }1 @; T g# T) E* C/ }. Y/ A called DFARS (Defense FAR Supplement).9 X: @1 ^! n# e0 k2 | FEDSIM Federal System Integration and Management.8 A1 J( R) A( j9 w7 g ~9 c1 w FEL Free Electron Laser.$ ~$ P o* A+ e8 P0 @* d FEMA Federal Emergency Management Agency.7 C" ]: l( Q0 L } Fenced Funding An identified aggregation of resources reviewed, approved, and managed as a+ j: C( V* `& B1 `; E' x distinct entity. The proposed program must be implemented within specified , |) i8 p" x8 e7 p- t8 u% B0 a6 mresources. Examples of fences areas are: Intelligence and Security, Support to# d3 Z7 _: k) ? Other Nations. Y1 f& a! r+ c' uFER Financial Execution Review. 7 @! N- U& F0 E- ~& WFES Facility Engineering Surveillance Plan. 6 ?- I i' P2 |0 d8 ~4 Y( aFET Field Effect Transistor.# X. b: ^; H# G% P, k. V8 x FEU Flight Evaluation Unit.7 j6 X( h5 G7 e. ?, ]" l FEWS Follow-on Early Warning System.+ ^" ?+ B; k! I- `! q0 a& ? FF Fire Finder Radar (US Army.0 I. T2 [8 E. m5 n MDA GLOSSARY, VER. 4.0 F 0 o6 y! ?; H. K/ b' [106 $ r1 f7 o+ K( @+ IFFBD Functional Flow Block Diagram. 3 c: t; E+ h `7 qFFCD Full, Final and Complete Disclosure (Treaty negotiation term). # a4 {! T. Q) h6 l1 JFFD Fraction Failure Detected.6 h* }% ^' D; a6 X6 ~3 r FFH Fast Frequency Hopping.2 y' b% c5 _ Q9 \( Z r. D! O2 ` FFP Firm Fixed Price. * \; i: v6 I1 B- Z5 P# o; CFFRDC Federally Funded Research and Development Center. " l2 V% ~: L$ SFGC Functional Group Code (Navy ILS term). / v, W7 w7 G7 \0 P; w6 XFGEP Fixed Ground Entry Point. 4 c$ C& |2 ]3 ?: L, q( _; xFH Flight Hours.2 ]7 [( M, y& ]% u& \1 G: y$ y1 ]( t FI Fault Isolation. - c, |) b& m- {) nFI&A Fault Isolation and Analysis. ! F# s. q2 y" U$ P. zFIDO Fighter Duty Officer (JFACC term). " x: Q# R3 G) O/ R- O7 QField of View( C1 L+ s# ~; `+ U* F (FOV) ! _% [1 S/ o! B; }( [1 }* Q$ _" lThe angular measure of the volume of space within which the system can $ c `. M/ N% {; V+ R- `3 trespond to the presence of a target. : k# j6 ~3 K8 Z) |' AFighting Mirror " W7 T- O3 {2 P' i& ~( p3 I& d(FMIR)2 `" P+ i9 J3 i3 ~6 { Part of the GBL System. The low orbit mirror, which receives laser energy and C- W6 Q0 l1 U5 J7 |( h: Areflects it to the target. " {2 M G* A# |3 j! i- pFigure of Merit0 M; _; {7 c" s( c" o$ V (FOM) ' H1 z2 P/ y. x7 F' Q1 ~( RThe numerical value assigned to a measure of effectiveness, parameters, or ) B( t! g6 e5 p. ^( j6 M$ K. ^# w# _other figure, as a result of an analysis, synthesis, or estimating technique. 2 D, Y7 C( J* v+ B& ]# Z" YFIP Federal Information Processing.' i- _- ]; r4 s3 y+ x FIPS Federal Information Processing Standard.0 l1 {7 J1 A4 o1 a Fire Control The control of all operations in connection with the application of fire on a target. 8 O5 P: O- P' j. q% a3 g! lFire Control& d0 t5 D/ ^+ e, p4 I) r& H& p System + ]; x( K* F! n9 LA group of interrelated fire control equipment and/or instruments designed for % c+ S+ {' @( _$ [; Tuse with a weapon or group of weapons.# s. O a, b- A* x# d8 K1 k Fire Support2 ~5 j: C6 c. n, D% w Coordinating ; t% _. s; K% {1 n5 Y9 ZMeasure4 W/ l p! |# q' j9 D A measure employed by land or amphibious commanders to facilitate the rapid1 J' b5 t/ i. p$ w engagement of targets and simultaneously safeguard friendly forces.1 J( c- z$ I) f' E7 J( }4 f Fire Support) A% g* x2 V- m Coordinating Line8 Z) g H* e# n. q, H (FSCL), c0 `$ r' r# w9 K7 ^% U: ^3 |6 [ A line established by the appropriate ground commander to ensure the3 s9 X$ G4 m t5 V7 R0 Y coordination of fire not under the commander’s control but may affect current - W- n( X3 d7 x6 P: x* g$ ?tactical operations. The fire support coordination line is used to coordinate fires5 d. K4 F! I# C$ d" S of air, ground, or sea weapons systems using any type of ammunition against - P* j- {1 N2 E; Ysurface targets. The fire support coordination line should follow well-defined : E& E6 M! _2 Xterrain features. The establishment of the FSCL must be coordinated with the - ~( I9 O4 G% @$ i4 W3 nappropriate tactical air commander and other supporting elements of the FSCL % `0 }* _" @$ j' K; m" S2 _without prior coordination with the ground force commander provided the attack: c4 a/ o2 {1 } will not product adverse effects on or to the rear of the line. Attacks against/ ^! T* Z8 h! _; {* V surface targets behind this line must be coordinated with the appropriate ground 8 o! J {. _1 i$ S H+ Wforce commander.3 P( G" J C- N$ U0 O' V6 P3 e& L MDA GLOSSARY, VER. 4.0 F5 F: n7 e2 L% ^2 N% T1 a. p 107& s7 t* k3 y( R$ b# r& L Firing Doctrine The ratio and manner of assigning numbers of interceptors against given ; D4 Z" A3 `: v" x& m0 h( s- V; Zattackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are 2 F& v/ f! d- F% }) bexamples of different firing doctrine. The priority of targets being defended and 9 C3 q, T A9 r) ^) \the number of interceptors available relative to the number of attackers drive * d) b5 `2 ?1 t1 zdoctrine. ! n: ?, Z" p9 ZFiring Rate The number of missiles fired per site per minute.7 u" f* j/ \& N9 M4 y' ~# C FIRMR Federal Information Resources Management Regulation.( ?& S" v) j/ I' C. \ FIRST Forum of Incident Response and Security Teams. " @9 _+ H7 t% H' D" B3 {9 eFirst Article First article includes pre-production models, initial production samples, test8 ?' B- z' m; J' s) v' E* I% [& m samples, first lots, pilot models, and pilot lots. Approval involves testing and * B `+ V: G7 l+ g4 V p1 ievaluating the first article for conformance with specified contract requirements% H" b5 B8 f- q' m before or in the initial stage of production under a contract. 8 R0 E. C5 y4 P* DFirst Strike The first offensive action of a war (generally associated with nuclear operations).' d! I0 s5 c& K" T8 O; F8 B First Unit 8 w8 R# U3 @, j' m7 eEquipped Date ) N2 l3 t3 g. vThe scheduled date an end item and its support elements are issued to the; s: x) @# Z3 ^( k& m8 i8 @ initial operational capability unit and training in the new equipment training plan 9 O- |+ }- C7 Y# thas been accomplished.0 ]+ I! `8 L( x O FIS Facility Installation Standard.' ~) M/ R8 b8 h/ A) _9 w8 { Fiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which; |* t& g7 N4 P0 B2 ~ provides the fiscal constraints that must be observed by the DoD Components in 3 u# L X8 ?$ a; ithe formulation of force structures and the FYDP, and by the OSD in reviewing ; P+ S3 a2 n5 x3 ~1 Pproposed programs. R/ J% c* r9 |1 g; Z! CFISSP Federal Information System Support Program. 1 r7 a1 m% Q8 FFIWC Fleet Information Warfare Center (USN term). 9 f% ~# l" w" m! B9 H; mFIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern M% \) c0 q/ p- ]1 ]Extension). 3 h3 c# g) a2 P" k) JFixed Costs Costs that do not vary with the volume of business, such as property taxes,3 {& L- I- T/ y/ V3 ?4 x) q insurance, depreciation, security, and minimum water and utility fees. . c/ F' J0 Y) C D. SFixed Ground 0 ]/ F3 D+ U2 {& h9 ~1 bEntry Point0 y/ C; m: s& X8 g (FGEP)) ~: F' o. P& ]$ z The subset of GEPs, which are not transportable. GEPs provide the& d2 s t9 v. f communications interfaces between the SDS space orbital/sub-orbital elements , c5 x4 R( d% B- t6 {; H+ dand the C2E.9 o$ x5 Q8 r+ e& C! D8 s Fixed Ground; Q. Q. ^' ^" k$ n Station4 k( X- h) k, X All hardware, software, and facilities located at a fixed ground site necessary to ) E3 @4 j& r3 @9 s; creceive, process, support, and analyze mission status and data, and disseminate4 s4 d* L2 b" @# \ operational messages. : D! ^+ ?. O, F" m5 l8 H& `FLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor( ~( O, g3 T3 N! i( V program to Extended Range Interceptor (ERINT).) + Z8 t4 N" X& NFLC Federal Laboratory Consortium. ' m% \% v7 L0 W8 sMDA GLOSSARY, VER. 4.0 F : J, s0 N, S) l% a) V) S4 D3 P5 Y108 2 L1 ]1 ^7 a! O, @$ [; bFleet Satellite " o8 j( ^8 x, a% l4 [* Z0 d! [$ CCommunications2 s* \" o( m$ Z ~ System 6 D+ q# Q1 V1 g6 E0 k% ^(FLTSATCOM)3 V- K6 }) Z7 M1 p0 t Operating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost3 v- K* W* Q; A$ ]( J terminals with simple antennas for use on highly mobile platforms. It has a 0 G$ V; c- q" hrelatively small capacity because of its much lower operating frequency. It / T% U& f$ j# f) F) O5 X- _$ rprovides a satellite communication system for high-priority communication ( U1 Z5 d# h0 M! c( Y% i/ Erequirements for the Navy and Air Force that encompasses almost the entire y. B: F3 G! iworld. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF% w/ U; o, J3 v5 g2 w and SHF bands. The Navy has exclusive use of 10 channels for communication7 B; o" J. f% G$ ~+ I with its land, sea, and air forces. The Air Force uses 12 others as part of its ) m/ L& ~7 l9 k7 y- ?* `/ t& U }AFSATCOM system for command and control of nuclear capable forces. The 9 J' L" x; J- K1 E. C) v- P- n( [. Asystem has one 500 KHz channel allotted to the national command authorities. 3 ~ b$ l! d1 y/ h9 rFlexible & |+ M" M6 M5 G5 ]9 T! d, \! UResponse ; T' n ^( [7 N! x5 r7 YThe capability of military forces for effective reaction to any enemy threat or3 }& E) b. l K+ O# V5 s: H% _ attack with actions appropriate and adaptable to the circumstances existing. . u7 n: x7 ~, ~2 f4 _FLHER Funds and Labor Hours Expenditure Report. ' k, D/ a' i9 a4 U; ]$ lFlight / Y/ d- \2 N/ ]3 T) @+ PDemonstration 7 l6 k e7 Y" k- ] ZSystem (FDS) & _2 m. N& [, J3 K7 r" I# S2 [Part of the SBIRS Low Program Definition and Risk Reduction (PDRR) program 3 q- w3 c# M" V2 e6 T4 Rphase. The FDS will consist of two satellites and a ground system being built by! X+ G: ?/ c2 K- G TRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test, `* O" k$ p2 I# ?9 X8 T8 Z program to demonstrate operations and performance of a SBIRS Low concept, " I3 l! Z. [2 B3 ucollect target and phenomenology data to support the objective system design,; Y" e# w6 I. Q* ~+ f% r0 }5 x: m0 n and validate cost estimating models." l0 J1 m9 v) z5 K6 {) d. j Flight Path The line connecting the successive positions occupied, or to be occupied, by an9 L3 _3 @7 @* a1 ?9 z: L+ U- k9 P aircraft, missile, or space vehicle as it moves through air or space. (It is more2 f: E1 M! O1 s4 z7 u; O$ i commonly referred to as trajectory for space vehicles, especially ICBMs.): J. [5 y9 S! l Flight Readiness' S2 T0 n0 j5 p4 A7 M Firing U- h, P# |; j( D- L A missile system test of short duration conducted with the propulsion system 8 o# o, c; x0 q) Goperating while the missile is secured to the launcher. Such a test is performed4 }, P+ }0 H( V' U) ^+ r( a/ r to determine the readiness of the missile system and launch facilities prior to 9 ~* A2 n3 r x5 [3 fflight test. ' N5 M) X2 c7 uFlight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching. " U' ^* O' [; }Flight tests are planned to achieve specific test objectives and gain operational ! F# p: {9 `' p. G6 q. v; g Dinformation.4 r6 `" ^2 \" f3 I% ~8 z Flight Test W" W- s1 }, j, b7 B d2 J Vehicle (FTV); p' y9 i3 U7 D: V Prototype of airborne or spaceborne hardware used to validate a technology $ c4 n) m( g) K, h6 {concept.

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FLIR Forward Looking Infrared Radar.* B/ J5 O7 n; b* p6 l FLOT Forward Line of Own Troops.8 s2 N5 _& M! o. w- ~ FLT Flight. K& I- j( w+ j0 S! E1 S4 b FLTSATCOM Fleet Satellite Communications System. % b5 H' C' F8 `) cFluence (or # p: m$ w* A+ @ j' f8 S' tIntegrated Flux) * ~% W/ G( r. x: Q5 wThe product (or integral) of particle (neutron or photon) flux and time, expressed" q, t/ j+ ]( f" k in units of particles per square centimeter. The absorbed dose of radiation (in% h8 X% T H% _. `+ s" Y9 w* P" G rads) is related to the fluence. (It should be specified whether this is incident or ) b5 l7 L" P1 G6 \& Zabsorbed fluence). : u- D# A# Z) K# d z. pMDA GLOSSARY, VER. 4.0 F & q7 i) B9 ]5 v109& j) v1 C; e) l% l7 A9 s, i Flyaway Cost The total cost related to the production of a usable end item of military hardware. 1 a! P: g7 q- K( uFlyaway cost includes the cost of procuring the basic unit (airframe, hull, chassis, # i) A7 S: G6 w4 j1 V }# D J$ xetc.), a percentage of basic unit cost for changes allowance, propulsion/ m0 k4 u6 X ^: ?! P& B equipment, electronics, armament, and other installed government-furnished / r6 {! i8 a b3 V7 B/ ~equipment, and nonrecurring production costs. Flyaway cost equates to- b1 z+ ?% |3 ] Rollaway and Sailaway cost. 0 l# \$ A/ `! @FM (1) Flare Multiunit.1 y* y! U+ s3 a* M4 @% y (2) Frequency Modulation.& e0 E( x$ W1 b (3) Functional Manger.. U9 c0 v) {! h K0 ]5 f (4) Force Module(s).! }5 C4 D/ h+ G& w (5) Field Manual. - X5 }* Y2 g% A( n7 ~; Y9 yFMA Foreign Military Acquisition. 0 w5 t$ H4 `0 \+ W# B5 S1 H/ R! RFMB Financial Management Board. / i @' x" ~, B8 D7 g n& DFMC Flexible Manufacturing Cell.5 A% H6 j0 |" s7 Z FMEA Failure Modes Effects Analysis (ILS term). $ W8 {% W5 s$ ] L5 uFMECA Failure Modes Effects and Criticality Analysis (ILS term).( E/ x; [2 V& p' Q' K FMIR Fighting Mirror.! i1 R- B! p7 u5 M6 Z) c3 j7 F: c2 @ FMP Foreign Materiel Program. 1 ^9 o- R0 X# u- L$ JFMS (1) Flight Mission Simulator (PATRIOT), Huntsville AL. , q3 b' M0 I4 c/ T3 R' Q. u(2) Foreign Military Sales. ' W3 \$ C" }+ I7 ?1 PFMTV Family of Medium Tactical Vehicles (USA term)./ o$ ?3 b3 f8 t/ {# r$ z FNC Federal Network Council' H: S( e2 \0 R$ H$ B0 } FO Force Operations (PATRIOT).. X G& X Q, ` FO Link Fiber Optic Link.3 p$ C; P) _. c7 I8 Q FOA Future Offensive Aircraft (UK RAF term). 0 G& A7 @9 v" o% z) E. ^) O$ aFOB Forward Operations Base.& f& ?6 D* u+ t9 M FOBS Fractional-Orbital Bombardment System.: z3 h' R9 Z9 S( b FOC Full Operational Capability.0 X W8 l+ I7 A- e8 h3 o: b Focal Plane The plane, perpendicular to the optical axis of the lens, in which images of points: S0 U1 o. }' E' T6 V+ F in the object field of the lens are focused.7 r' B# ?$ R/ P- U- f: D Focal Plane+ D! U& g4 ]2 \! F Array (FPA)& H& f+ M1 H/ x3 g. r An FPA is a matrix of photon sensitive detectors which, when combined with low - I. Y* J4 b: ~: u$ |noise preamplifiers, provides image data for the signal frequencies of interest.; K) F7 y. _8 o l, S1 w1 ? FOFA Follow-On Force Attack.& |9 i8 I2 X- ~ FOG Fiber-Optic Gyroscope. 3 C$ A2 U* a. B1 BFOIA Freedom of Information Act (US). . ?1 A$ f. l7 g5 t* y/ N; [! A: \MDA GLOSSARY, VER. 4.0 F 3 z6 \7 v( q9 @4 ?7 ?+ P% n110( R- a5 h) v" b FOL Forward Operating Location. , S3 Y+ P% l5 L% P+ o2 h# cFOLAN Fiber Optic Local Area Network. . X% ^) `6 _( tFolded Optics Any optical system containing reflecting components for the purpose of reducing& Y/ s- S$ n" q6 v" ^* H the physical length of the system or for the purpose of changing the path of the& f9 F/ @9 r" x) y9 Y. X optical axis. 3 ^' d `5 p; b9 O2 k# P# P" aFollow-On ! i7 K" u A7 I; E& k) O* AOperational Test ; L5 W( Z$ C G9 mand Evaluation$ M# {2 t5 f% _( K% ] (FOT&E) + ?& i' A1 M6 i0 W; l0 SThat test and evaluation that is necessary during and after the production period/ y# P/ D- k! w' S) k to refine the estimates made during operational test and evaluation, to evaluate 1 f' t5 u: z- {4 z( s- Uchanges, and to reevaluate the system to ensure that it continues to meet & [8 e* Q) e) coperational needs and retains its effectiveness in a new environment or against / N! e9 c* u6 O0 _8 F# W) Wa new threat. 0 G4 E+ W; [/ NFOM Figure of Merit. 0 n0 [0 B$ C. N9 G! ]$ `6 OFON Fiber Optic Network.4 F; @' N! U( v5 } Footprint (1) An estimated area of possible reentry or the solid angle of a detector or1 ]2 T# T+ r. s C; P: Y" k linear area of a detector at a certain location.1 R3 g" {% k# ~3 ^- I/ P6 X (2) Geographic area in which a focused satellite downlink can be received.) }( C4 m% r | A4 C' O FOR Field of Regard.$ z% H4 E. l5 h& ~. [4 p Force Closure The point in time when a supported commander determines that sufficient 9 ?3 g9 Y4 W( Z* i" y& b# `9 ~1 Zpersonnel and equipment are in the assigned area of operations to carry out , S" a$ I9 p! x, ^+ Kassigned tasks.3 Z: y% \+ n6 y( u) f2 y8 e Force Development Test and ; m" D5 |7 J _Experimentation: ]+ G% c, j& N4 f8 X Tests employing representative users to examine definition of materiel / h& [$ I! x0 J/ Q7 irequirements or support/assess development of doctrine, training, organization,; t& l7 t" _" J* Z2 j and logistics for system acquisition. (U.S. Army). 6 d/ Y X( D1 c$ O& m# ^! f2 m7 _( n7 iForce Direction The operational management of the forces.& V3 z) X: D' M% _2 A; ~# z Force Integration 9 f/ ]; J& K; l# m) \# @Staff Officer; g+ g0 T! J* V9 v Army individual assigned to ODCSOPS to serve as HQDA user representative for * s. a3 ~8 w+ S. V& }) na specific system. Provides continuous coordination necessary for integration of / @' f; Z9 K$ b2 ja new system into the Army force structure./ Q2 M5 f1 n# l! Y Force( e! P" @2 }& U Management% m# B/ I, }$ ]6 a+ ~ The assessment of the effectiveness of the defense forces throughout an 0 R* E2 h( r( E* Z2 P2 T5 k; Vengagement and adjustment of tactics and the system configuration as ) e6 h# ?6 f" B$ w! t; ]- snecessary to effectively allocate resources to satisfy mission objectives. . T. U3 S9 m8 W/ U; P" J0 c. J5 H- fForce Reliability The percentage of the missile force that will successfully detonate within 3.5 T" @' C3 c! F- C- E CEPs of the target. 9 }$ {: F5 m4 j0 K2 K/ JFORDTIS Foreign Disclosure Technical Information System. 2 k. m; {- N( {7 X1 j+ |0 kForeign / y( s( u: F$ u. x5 |Government, ^" w! [6 [" a; f" u' ]% `% [ Information e9 ~6 q5 c+ _3 k- l% f Information that is (1) provided to the United States by a foreign government or2 ]3 ?# F. k! d governments, an internal organization of governments, or any element thereof1 R0 N7 s: c1 E& ? u; ~2 e/ f with the expectation, expressed or implied, that the information, the source of 4 C n% D* x8 m0 E# r( A8 ^* Ethe information, or both, are to be held in confidence; (2) produced by the United { C! k- c" w6 NStates pursuant to or as a result of a joint arrangement with a foreign , p: ~, b/ x q1 `8 egovernment or governments or international organization of governments0 k0 ~1 j7 \% A! r requiring that the information, the arrangement, or both, are to be held in* U5 @# @& Y0 `1 N' n1 s confidence. ' _: _- w9 i# T9 y/ Y5 JMDA GLOSSARY, VER. 4.0 F $ n7 Z2 h5 @6 a. j6 u/ G111 & M( U" ^# q1 L, f% g5 pForeign Military; m: s% c2 k9 C0 q. R) y Sales (FMS) 3 L+ I# s) f8 ], e. AThat portion of U.S. security assistance authorized by the Foreign Assistance Act* J, R4 X' I8 s9 l! C of 1961, as amended, and the Arms Export Control Act, as amended. The- H+ M0 w. V4 {$ X0 D recipient provides reimbursement for defense articles and services transferred ! J8 S2 Y$ s3 C. w' e6 Dfrom the U.S. Includes case sales from stocks (inventories, services, training) by % Q( T8 @8 M' pthe DoD defense services. % n# b o# \7 j9 \0 j2 W' ^Foreign Security& q; q& L! }' |" V, \4 }1 n; h9 V, |7 { Policy Model + _7 v/ Q" H, ?- j8 }( u" Q9 o: RA mathematically precise statement of a security policy. To be adequately 8 P! W5 o* R! ^precise, such a model must represent the initial state of a system, the way in 5 N- }+ x1 k) kwhich the system progresses from one state to another, and a definition of a " `% M. i0 j" M: n# \# E& X3 M“secure” state of the system. + K( S; d2 T3 A9 R2 YForm, Fit, and( y; P: `9 \; M& }( ^+ x* E Function Data7 N0 @: d1 H" \1 K/ `1 ` q Technical data pertaining to items, components or processes for the purpose of $ |- k' _+ l6 d" d& oidentifying source, size, configuration, mating and attachment characteristics,0 j* k# R& s5 B1 L+ l8 F: z! u functional characteristics and performance requirements. ( D O) a7 P. w' m( x# [Formal3 ?0 o6 [) |+ ]* a: [, A# S Qualification ' t9 ]5 G* J/ W5 s5 u* `Review3 v8 g7 E$ Y/ `* p* e A systems level configuration audit conducted after system testing is completed/ B7 P+ g( K, f( o to ensure that performance requirements have been met.; O2 @4 j H+ d* k; X* l Formerly% C1 d4 w% f( h. t% J3 L k Restricted Data 2 O7 D8 C" Z# X; `: OInformation removed from the RESTRICTED DATA category upon joint& p9 I. s( j, V/ D( k: L! Z determination by DoE (or antecedent agencies) and DoD that such information # H( b4 U. x. y5 ?- S/ Wrelates primarily to the military utilization of atomic weapons and that such: y2 o1 ~- K- M8 A# a0 M# d4 V information can be adequately safeguarded as classified defense information.2 Z' r: m# _! P FORSCOM U.S. Army Forces Command, Ft. McPherson, GA. L& t5 J. G5 v$ M a# Y, Y FORTRAN Formula Translation Language.

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Forward Edge of. e' f; y; V& @7 y. l. `! H' j the Battle Area- L1 _" P M f1 t' V (FEBA) , B/ V, F# @: J1 z+ {: q* ]5 QThe foremost limits of a series of areas in which ground combat units are - L: |6 ~/ C5 R# t V# tdeployed, excluding the areas in which the covering or screening forces are 4 g/ j; n7 x5 {8 _# Joperating, designated to coordinate fire support, the positioning of forces, or the ; I% Y3 t6 s1 Z8 w; xmaneuver of units. 2 W0 A3 k+ ~2 }6 oForward Funding Carry-over of RDT&E funding into second year of appropriations availability. & S% S# R9 J8 n3 O$ URequires permission from high authority.! E0 M) ?8 x) a' z FOS Family of Systems (TMD).4 p5 x; I' G5 R | W; l# m9 N% D' ~ FOSS Fiber-Optic Sensor System. % p. z& K2 P8 h6 q& z* e' rFOT Follow-On Technologies.8 v$ q" l# e( V FOT&E Follow-On Test & Evaluation. : e3 G( f9 v; E0 PFOTC Force Over-the-horizon Track Coordinator (USN term).3 Q7 u% d- k" ], |* [ FOUO For Official Use Only. . P0 o+ d, c E) Y/ Y1 tFourth 9 G* n4 v# y& W0 J% C3 U2 |( hGeneration: V+ l a G$ S4 O# J Language0 b& v/ l- z) S9 E) y A programming environment that produces both screen and report utilities for2 H, V9 R: M9 N2 R use by lower-level programming environments. & j5 K' c, R+ X( E, B7 r, K3 oFOV Field of View. . E8 s. n/ J$ F* |FOV Radar [Full] Field of View Radar9 t$ {# X) D* Y# ~2 S3 x4 N FP Focal Plane.. e2 i: N5 t, M7 f' x# ~ MDA GLOSSARY, VER. 4.0 F . {# X. O3 g0 `5 j9 c( H1126 b8 @1 ~$ q5 [$ e" ~ FPA Focal Plane Array.8 N8 h3 k6 Q! j! R FPC Facilities Protection Committee. ' z4 ^' v# N2 }FPI Fixed Price Incentive.6 S4 O5 S/ c n6 Q: y3 m: E FPS Fixed Radar.6 d4 O9 J0 o( }: D" `: \ FPTOC Force Projection Tactical Operations Center (USA term).0 }( B$ u# R8 y; [ FQR Formal Qualification Review. 1 h. l6 ~ J: b1 nFQT Formal Qualification Testing. 2 ]% U9 ?, [; X7 s7 m2 p; pFR (1) Federal Register. (2) France.0 \& b% L0 f3 g FRACAS Forward Reaction Altitude Control System. % u* O( G% x6 u2 TFRACS Forward Reaction Altitude Control System.) s! b0 a& l3 l# H2 a# m Fragmentation# }0 N# U$ b2 Z* u7 c Warhead. a3 P8 R, S7 @" _* U0 N A warhead, which releases small solid objects to damage or destroy its targets. V: W# A$ v0 p5 v! y, W FRAS Free Rocket Anti-Submarine.3 S" Q7 R2 N8 @0 _, H FRC Fire Control Radar2 Y" i& a$ ?) V) P' u5 \8 S/ X FRD Facilities Requirements Document.2 H# o" t4 [: P$ w2 F) j Free Electron& E2 Z) s& q1 E Laser (FEL) 1 Z$ Q/ \/ ~: j2 |& IA type of laser, which generates radiation by the interaction of an electron beam& s( `! d6 w# U' S& ^5 M z with a static magnetic or electric field. Loosely speaking, free-electron laser # q- C2 g9 a' ^5 V, Y5 \technology resembles and evolved from that used by particle accelerators (“atom0 U Q* r( g0 e smashers”). Lasers, which are not free electron lasers, are bound electron1 F4 e ?0 l) r/ { lasers. 8 y3 H; A2 S8 A. A& BFree Rocket A rocket not subject to guidance or control in flight.4 C" j: r' |$ p. T+ o; W5 Y! m* t Frequency % v8 @2 `8 i) a2 }: t0 J/ n( SManagement ' t1 B4 |7 j7 e. \- K; \0 VThe act of allocating frequencies, or bandwidths to a telecommunications ) p3 Q, m4 f2 a9 N/ A7 j0 \0 Osystem, necessary to minimize the potential interference between % F, N+ l0 m5 `* Z7 J: Ptransmitting/receiving devices. Governing agencies and international agreement" K" h8 G% t$ m/ d: V* f controls authorized use of a particular frequency, frequencies, or bands. ' y& R- A$ ~6 b* f- `FRG Federal Republic of Germany. ! |1 I! Y/ x: E. D0 F) I# ?FRN Force Requirement Number.6 d7 u# K+ E' a- N2 {' f! Z FROD Functionally Related Observable Differences.. F& s% ?1 I B FROG Free Rocket Over Ground.0 H1 ~8 o; a7 R) s4 y1 T FRN Force Requirement Number.2 l' `* k, v9 E7 g9 ~5 ~ FRP Full-Rate Production.) S/ `, {) k2 f FRS Federal Reserve System. ; Y/ n! X$ U, u% c7 YFS&E Facility Siting and Environment (MILCON term). 3 {# _) X5 d+ Y" i5 ~8 o9 A0 _) U* ?MDA GLOSSARY, VER. 4.0 F& |4 c; Q1 A" U 113% B& R4 D+ a; k. L9 M/ G+ V+ x! A FS3 Future Strategic Strategy Study.; m% u- X" ?, u. G9 s) j9 O FSAF Future Surface-to-Air [Missile] Family.4 Q1 v7 e# ~+ o* q( q. g3 ] FSC (1) Fire Solution Computer. (2) Fire Support Coordination./ M9 {7 @0 W9 j' [" x t+ R7 x% @ FSCATT Fire Support CATT [for Weapons] (US Army term). - v6 c1 m6 P" {2 j- FFSCL Fire Support Coordination Line. 7 `) K) ~6 m5 Z' P: oFSD OBSOLETE. Full Scale Development Phase. See EMD.0 ^% J% _/ n* ?* E; K% Z FSE Fire Support Element.' x) `8 X! B* W( Q. i; S, m FSM Firmware Support Manual. ' | i" |+ ]+ L$ h! vFSP Facility Security Plan. % I& p. b) M1 p& Q+ M5 OFSS Fixed Satellite Service.0 \3 g1 Y" ~: s. I/ u" `1 Z FSST Forward Space Support in-Theater.5 Z9 v, n' j6 Z2 i FST Flight System Testbed.7 D; ], U; y/ F+ _ FSU Former Soviet Union. 8 t, W! ^! |0 m* u, C/ O8 OFSU Republics Former Soviet Union Republics. " N3 V$ B$ `4 S& a# oFT Flight Test.7 d& ~7 r- ]3 s Ft Foot) J: p# G0 e& u/ X5 D FTC Federal Trade Commission.* F% Q2 d s& b/ n1 h FTD OBSOLETE. Foreign Technology Division (USAF), Wright-Patterson AFB, OH. . ]( a! B0 N8 i y- P# ~7 pSee NAIC. % K4 W" L7 {: l6 {! A; ~FTI Fixed Target Indicator 5 L1 x4 s9 s! QFTLS Formal Top-Level Specification. 4 }3 g" x) K h" t/ i( d1 GFTP File Transfer Protocol (ADP/Internet term)., N% a7 I8 M; j1 [$ b' M, Z9 s, _4 s FTR Flight Test Round. ; {8 }0 R8 R5 _ y8 I: O/ i+ d) z, nFTS (1) Flight Test Summary (2) Federal Telephone Service0 g) M! E; h' ]7 a FTS 2000 Federal Telecommunications System 2000.( o" P1 z; o. L: O% H FTV (1) Functional Technology Validation. (2) Flight Test Vehicle.* M$ u2 z- {7 ~) ` FTX Field Training Exercise. 6 N9 X$ T1 c" a+ `1 F4 vFU Fire Unit (PATRIOT). 9 R# }$ w& ?# Y* l* l; [0 qFUE First Unit Equipped. ! T. d7 y; B# {) J" dMDA GLOSSARY, VER. 4.0 F6 `& Z! x7 A4 x* f 1149 @7 b6 i3 [3 t7 _0 C& @" k Full Mission 5 y9 X/ }0 Z2 C$ P$ T, qCapable8 r z! T7 e" D2 `/ u' e Material condition of an aircraft or training device indicting that it can perform all1 x3 x3 b) V4 n5 G8 @# R0 ? of its missions. Also called FMC. ! W& [; A7 L. Y. l# d2 Y- ?' _9 m" f5 kFull Operational6 l! l9 ^. k* K' e8 D/ U Capability (FOC) & N; q3 [+ h5 PThe full attainment of the capability to employ effectively a weapon, item of & W# |+ i8 c$ y0 c Zequipment, or system of approved specific characteristics, which is manned and: L, E' ~' T) l2 F5 m9 t operated by a trained, equipped, and supported military unit or force. $ B8 g' Q. Q( I9 uFull Rate l. N1 W8 R! o& RProduction . W, e) s3 n6 z$ }Production of economic quantities following stabilization of the system design5 Z+ \" C# p5 a Y, D" p" s! ` and prove-out of the production process." r4 I) F8 ?# b. g4 a! K- l8 g5 T Fully Configured 6 z# E( _7 k2 h# e; AEnd Item3 O( D j! b) T" o! E The final combination of end products, component parts, and/or materials, which " v" B/ U7 ?# T4 E6 `5 Wis fully ready for its intended operational use. Normally all production units are ) a+ g2 J: l5 Z- Q( lfully configured. Research and development units may be considered fully4 z7 H( ^: P' c; h configured if they are or are planned to become operationally equivalent to the 9 F0 s& q/ J$ t% q! Jproduction units.

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Fully Connected" O4 b1 {0 j. S( O1 `0 G3 h Network (FCN) 8 p* k) J# U* ] mA network in which each node is directly connected with every other node. : A& p' o1 j/ b" SFunctional* f1 f7 _! t% F5 M! t( p Analysis a. v7 G" |* X) x' D6 w+ iAn approach to the solution of a problem, in which the problem is broken down8 }! |6 X$ c; B+ _0 r into its component function, such as intelligence, firepower, or mobility. Each o6 V W G/ d" [0 u& |5 A) Urelevant function is then further analyzed and broken down into smaller# d0 O* J6 B* L+ u functional components until a level of molecularity suitable for solution of the 0 E( e3 z# Z+ f1 I4 Y! a# d( Bproblem is attained.- D% S* ?/ {9 d) s9 M2 n Functional 7 t1 T9 y$ b2 b4 C: c7 x: I. i. VBaseline 7 K4 l1 T ^* w; I) v(1) Established after the system requirements analysis/design activity has ' @5 i; C7 A) H- V8 E4 Xcompleted the definition of the system functions and associated data,5 O; x9 W5 s( X- p( K s interface characteristics, functional characteristics for key configuration & R9 `& R' A& x$ `! xitems, and tests required to demonstrate achievement of each specified # M1 a9 l, U7 ?' s9 |- {* U% w4 I0 Acharacteristic. This Government normally controls the baseline.2 j ~' ?; H+ i (2) In configuration management, the initial approved technical3 l+ M( p3 I s" s9 | documentation for a configuration item. ' p) Y! z: t+ X+ K( n+ j n(3) Documentation describing a system’s functional characteristics and the 7 l4 H9 F4 a# v( r) iverification required to demonstrate the achievement of requirements.5 ]& P( X, h M( D+ [6 b; \% ^ Functional ' Y1 t7 o6 s( \. H SConfiguration $ \+ P, p1 E7 x! x. o8 JAudit (FCA) 8 k; f$ \- ?- r2 Q! t# N* K" wThe formal examination of functional characteristics test data for configuration * |& O" p- f5 A! ~item, prior to acceptance, to verify that the item has achieved the performance 1 \% f2 x; w/ O0 V' H8 L, X4 E+ q- Ispecified in its functional or allocated configuration identification.3 U# `3 l9 F5 Q8 }( ^3 w2 j6 i Functional 4 |" L& J% h- M4 j$ ]& A) { REconomic# D1 w9 P) y0 h' ]- Q/ m Analysis (FEA) 7 V* q J9 Q9 `( r% {6 C5 |0 cA structured proposal that serves as the principal part of a decision package for 3 t4 {% X# D1 |/ @. c$ b8 l6 Ienterprise leadership. It includes an analysis of functional process needs or! ~& Z% G( r/ Z+ t9 u problems; proposed solutions, assumptions, and constraints; alternatives; lifecycle costs; benefits and/or cost analysis; and investment risk analysis. It is 0 L7 u3 N7 b9 p1 M, V; _' A4 Nconsistent with, and amplifies, existing DoD economic analysis policy in DoD3 F% }" {: j$ F1 b1 @8 ~" N6 G; F N Instruction 7041.3. l8 {- [6 P% X- i( bFunctional Kill The destruction of a target by disabling vital components in a way not 2 D4 @& S" p" \2 N$ simmediately detectable, but which nevertheless prevents the target from& H0 Y- E) I9 D functioning properly. An example is the destruction of electronics in a guidance5 e5 {* h% o0 L; b! N A system by a neutral particle beam. Also referred to as “soft kill.” 8 d+ j" Z4 J8 y& ]$ f& NFunctional 8 {. ?; p/ ]( ~$ zSupport ) G3 L' E5 `2 V; x$ Y& M7 tSystematized methodologies and procedures, or a common set of standards,) ?% l; E8 u9 k$ i2 ` applied to materiel acquisition programs. 4 R6 b0 S' \! \9 CFunctional( N; S# t6 c2 E# y5 R/ h Technology6 q* b+ M3 h8 Z k% }% | Validation (FTV)1 C8 ^$ T0 p2 q2 T8 Y Program with the intent of proving or disproving a technology is useful for a given1 S7 ?5 ^2 ], e% ]. z; |( u- S: o3 f application.0 G, E. V F/ J4 |0 c" ]1 _8 C6 v MDA GLOSSARY, VER. 4.0 F, W3 v+ d3 \7 f Q 115 4 ?# \7 \4 W+ W8 GFunctional $ G& @( {* Z/ ]- YTesting+ u, a% m6 z0 U1 h The portion of testing in which the advertised features of a system are tested for" G) K& w0 F# A& P' z6 ^5 q" t3 C correct operation. # S# a% r7 S7 j. b1 ~5 L, h! J6 _Funding Profile Program funding, usually displayed in columnar spreadsheet format by years,& g! g0 f3 `) L starting with previous year through current year and out-years. % \" m- Z$ P7 G# `3 N0 t% nFuture Years / Y% d4 p+ b: C6 a8 ]. `Defense Program y, F/ k" R9 _" ]3 Y; T/ n v (FYDP)! x7 b5 w$ F5 O8 ?& V The official DoD document that summarizes forces and resources associated with% D7 F- W( K7 A& u6 y! f programs approved by the Secretary of Defense. Its three parts are the+ D& L8 l# u4 W& {$ I) J; ?; n- b2 f- U organizations affected, appropriations accounts and the 11 major force programs& [- N" G' W0 j$ q- M: } (strategic forces, airlift, R&D, etc.). Under the biennial PPBS cycle, the FYDP is: t. h! \; |. A! h& i; v$ |6 ?' \ updated in even years in April (POM); October (budget); and then in January + {; e2 o* b& D3 V2 }(President’s budget) of odd years. The primary data element in the FYDP is the+ x. T5 ?6 p6 ?, W- `( | Program Element (P.E.). Formerly known as the Five Years Defense Program.9 p1 Z5 G2 U# c: T& p FWCA Fixed Wing Combat Aircraft. - \) E6 ^$ F0 k7 Q# C8 kFwd Forward. ) Q9 d- E, W$ b, m2 q9 KFXBR Forward-based X-Band Radar." z$ R+ A" i+ i. r' D FY Fiscal Year. 2 {7 v j# ~4 ?+ t+ ? _$ fFYDP Future Years Defense Program. 2 H( ]: J( p' S4 {# SMDA GLOSSARY, VER. 4.0 G/ K1 c1 ]+ m/ O/ z3 w; a1 I( j 1168 m. R6 O, h7 t1 ?9 i& X G Giga (one thousand million). / a# v& B: n, Sg Gram. 5 \* P' S6 j6 m1 s4 YG&A General and Administrative costs. ) b8 [# r. U9 {% \& E: KG&C Guidance and Control. & ] F- `3 z3 j- h1 VG&O Goals and Objectives.+ w# W+ K7 ^3 o, K { G/A Ground-to-Air5 a$ a M& M/ b, L0 p% f/ g' h G/G Ground-to-Ground.6 {! b. N6 Z5 ~/ _7 y+ X% e GaAs Gallium Arsenide. , l" E7 N- j% L, R# aGalosh The Soviet Anti-Ballistic Missile system built to defend Moscow from missile 9 z, l9 o5 r& \. }attack., h% k* s. {1 R. ` Gamma-Ray Electromagnetic radiation resulting from nuclear transitions. Although incorrect,* W+ H3 v& X3 O% B7 e) o# E) X high-energy radiation, particularly “bremsstrahlung,” is sometimes referred to as - s i5 b# J0 F8 r) p: K8 Dgamma radiation.3 _! h; O. H1 B* | Gamma-Ray $ y) z) y) [& x. i6 @6 a! yLaser 4 @9 e1 W& }% c I8 @2 ~: wA laser which generates a beam of gamma rays; also called a “graser.” A) u- i7 v' t7 k6 l; X4 C/ ~9 W gamma-ray laser, if developed, would be a type of x-ray laser; although it would6 s* r, F5 h r: F% I G employ nuclear reactions, it need not (but might) employ nuclear fission or fusion 8 D9 e# p6 b2 u L4 G! c: \6 a3 _reactions or explosions.) `, }8 D$ H( Q" ^ GAMS GPS (Global Positioning System)-Aided Munitions. : H4 f8 [; r0 _5 z( x8 gGaNMPA Gallium Nitride Microwave Power Amplifiers. (A demonstration program to develop % M( L6 K5 ]4 ]- a9 {- QGaN based transistors and integrated circuits for power amplifiers in systems % ^+ [& z2 L- I I5 M1 T `! ]such as Ground Based Radar. Goal is to reduce total weight and size by a# Y* r- q+ N( r+ j factor of 10). 7 A, X5 L5 z1 j- GGAO General Accounting Office.0 y* a2 E( _/ e0 _ GARDIAN General Area Defense Integrated Anti-missile Laser System.4 F& t$ o+ }. u( p! w GAT Government Acceptance Testing.7 X( |: z6 d) @$ h8 ` GAT CALL Guidance, Apportionment, and Targeting Call (JFACC term). * g. y. i) ], t8 [) U) HGATE Graphic Analysis Tool Environment.. U) Q, F) u3 I; G Gateway An element that contained a node on the SDS backbone network as well as on ! C/ h5 D& r' ^- F3 p o( l" qsome other network(s) and would have performed protocol and format 1 w4 N C' o$ w- G' ~, [+ aconversions necessary to accept messages from one network and retransmit 9 c5 t% B! D" x7 R2 ^9 a" o1 a7 g- c6 Fthem on the other.' p" m3 _9 ? _5 N. L4 m GATS GPS (Global Positioning System)-Aided Targeting System., ], A, ]6 }$ n) s GB (1) Ground-Based. (2) Gigabyte." Q- o3 y, |: y GBD Global Burst Detector.! _" a4 J' s9 @+ i2 v+ ] GBDL Ground-Based Data Link.0 x+ C5 k; g }1 I5 O/ m2 z MDA GLOSSARY, VER. 4.0 G& o' b7 z% S2 T& E/ U% v 117% y1 e+ R) k2 T7 s5 w" m4 X GBEV Ground Based Experimental Version. # d9 k$ I) Z6 t6 u' W5 jGBFEL Ground-Based Free Electron Laser. 5 R2 \* M& t: t+ b8 DGBHE Ground-Based Hypervelocity Gun Experiment. ) p: G, r: m* S8 d& K2 }+ \- q' l6 FGBHRG Ground-Based Hypervelocity Rail Gun. ! `; q# q3 t# Y$ { V7 QGBI OBSOLETE. See Ground-Based Interceptor. . A6 V8 f% A- wGBI-P Ground-Based Interceptor – Prototype. ; D4 H% |& |! Z! d3 c3 DGBI-X Ground-Based Interceptor Experiment. ! s. T0 ~- o% R9 O1 `+ bGBKV Ground-Based Kinetic Kill Vehicle.: D# E- b( K. @8 Y5 u7 B; ? GBL Ground-Based Laser. ; Z# j7 l6 l; n0 e' o: n8 M. UGBLD Ground-Based Launcher Demonstration. # {6 d( G$ \4 c5 Y7 X3 B! {GBLRS Ground-Based Laser Repeater Station.* ?, r/ o) X4 g) o- ], ~4 a GBM Global Battle Managers. 5 N1 [+ i3 E0 F& e5 l+ [* H }GBMD Global Ballistic Missile Defense. / P2 b3 I7 S0 X( {GBMI Ground-Based Midcourse Interceptor.4 |+ U6 }/ s- k, G3 S6 C GBOS Ground-Based Optical System., @* I% D/ ^1 c1 h8 @. s GBPST Ground-Based Passive Signal Tracking.7 J. N6 G2 C+ A' a# X0 d5 W GBR See Ground-Based Radar. , U* T7 b% h) A" c0 w" qGBR-M Ground-Based Radar-Midcourse.6 B; m% b2 b# y- _ j GBR-O Ground-Based Radar-Objective.) e1 @& q% t7 ^ GBR-P Ground-Based Radar-Prototype. 2 U3 f7 S* r$ \' S7 G$ F( Y$ n# Q2 J; @GBRT Ground-Based Radar Terminal. 9 Z) B$ y% R3 H! ?* Q3 rGBR-X The experimental version of the GBR. ; s5 ]! }4 V3 o& g+ {+ i w; q. CGBRF Ground-Based Radio Frequency.

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GBRI Ground-Based Rocket Interceptor.: G, z+ s! o( Q6 v* B9 ? GBRT Ground-Based Radar Terminal.6 ^) t2 ?# b. q. i" K5 e _& t6 r2 {$ f GBS Ground-Based Sensor. 0 Y/ m9 {, }" }$ Y# s' QGCA (1) Guidance, Control, and Avionics. (2) Guidance, Control, and Airframe.: y+ k/ F6 k. u1 i l GCC Ground Component Commander (JFACC term).2 [2 Z0 f$ `7 q GCCS Global Command and Control System.! f5 l! b. X+ ?0 O+ e1 z0 g+ M: U MDA GLOSSARY, VER. 4.0 G 3 X5 g% b: L8 B. ^$ ~118 6 I. Y: A! x' w* L5 pGCI Ground Control Intercept. 9 Q! O( K# c" b; A) M LGCN Ground Communications Network.9 u. m: y# H! [6 s8 c$ U GCS Ground Control Station.- ` L" W, \) d) [6 Y' x GD General Dynamics. - K( W i% E2 A1 g. U7 X" qGDL Gas Dynamic Laser. ; L1 z* R! E! o2 D% d7 R. xGEDI Ground-Based Electromagnetically-Launched Defensive Impactors. / V7 K& q& M+ V- G* nGEM Guidance Enhancement Missile (PATRIOT). % s2 r+ }6 |2 o* `" eGeneral Manager 8 W* a% S7 r/ ?7 g: I# tProgram. m; h' G+ y, Y1 |8 O+ `8 v Management" {5 j! {! @1 ], F5 f Directive (GPMD) 7 c( f3 O" i- b+ R$ K5 y2 aOBSOLETE. The primary document used by the GM to direct the Service BMD + |2 s! k; y" f% o' ~PEO on the specific actions necessary to fulfill BMD program requirements.: M; \6 q% ^7 w! j+ @ General 9 d/ p. Y# h5 |1 V* Y/ q. QSpecifications : Y2 _9 o1 j6 H( ~& ?1 c' AA general specification covers requirements common to two or more types,+ t1 Y5 J5 x% {3 }* v classes, grades, or styles of products, services or materials; this avoids the. [- O0 ]5 @: @/ p9 J, t2 p5 A3 B& e repetition of common requirements in detail specifications. It also permits * k% O W7 R- K: Y% _changes to common requirements to be readily affected. General specifications3 m' C: e$ Y" E' r7 ? may also be used to cover common requirements for weapons systems and: }; A0 O% p+ r6 E6 Z* Z7 Q" @ subsystems.2 X* s' w5 _( I% S Generic Rest of ( X% f$ O/ t" ~" J. ^5 e( Q: Y! kWorld Target + [7 z1 ]0 }. _: j3 N(GROW) 0 B( ^5 L2 \% J: o4 A8 W7 ?" mStrategic target being developed for GMD program.+ j7 T, c" i( ~2 n GEO Geo-synchronous Earth Orbit.5 A+ P0 r; o9 i' y* k. {9 ~! o GEODSS Ground-based Electro-Optical Deep Space Surveillance System. ' Y) @3 R: ~" m1 `2 n# c! U$ V' `Geo-stationary* c3 }& I k, g/ Z7 A9 [6 v Orbit (GSO), z- Z) W5 K& x5 Z& U2 v4 p& w An orbit 35,784 km above the equator. A satellite placed in such an orbit- l9 F; D n+ O( T, @" f/ S revolves around the earth once per day, maintaining the same position relative2 i0 B9 k$ @7 Y; e* a" x to the surface of the earth. It appears to be stationary, and is useful as a% U* U! {2 U {# r4 c communications relay or as a surveillance post. : W& }( `! `/ zGEP OBSOLETE. Ground Entry Point. IFICS.# N9 P3 A% _6 t* f4 L GES Ground Engineering System." e& o# V2 f4 j. o: O+ z GFE Government Furnished Equipment. See Government Furnished Property. s# R2 |) N% o5 W GFI Government Furnished Information.- H8 L6 R" w( c' `1 c6 M GFM Government Furnished Material. : C9 n) l. d* A cGFM/P Government Furnished Material and Property. See Government Furnished, `$ I8 H8 D d Property.! X- e( M1 C# p2 {/ @ GFP Government Furnished Property. 0 x" ^) a- Q) g" W) ^ z7 o DGFS Government Furnished Software. See Government Furnished Property.3 }& ]3 l6 H. B5 ]+ i. b, q MDA GLOSSARY, VER. 4.0 G7 a& E; M( I7 p. j 1197 I6 ~) I! r# ^ Ghosting This condition occurs when two or more targets reside close to the same plane$ x# k% ~4 Z" e also containing two sensors viewing the targets so they are within experimental# c+ M$ n0 @$ s2 U: B1 ] determination of having the same hinge angle F. Thus, ghosting depends on 1 G1 l V$ k1 d- P, N; FLOS error and positions.4 I5 @5 p/ y4 X0 l5 Q) W8 A# a GHz Giga Hertz (1 x 10(9) Hz). , G6 s* o5 @5 C: `4 B, C8 pGIDEP Government/Industry Data Exchange Program.* K- T, a+ D" Q( s' Z3 e6 _ GIF Generic Interface. " N' |6 o+ y3 U zGII Global Information Infrastructure. $ |6 a( K1 E4 o2 a9 wGIP Ground Impact Point. 0 S: g: o8 x9 u- z) YGIS Geographic Information System.! _5 w% T* q8 M1 ~% P GITIS Government Integrated Technical Information System.; M; W& K q# \) Z. s5 P, p GLCM Ground-Launched Cruise Missile. , ~ d3 K# G6 EGLP Ground Launched Probe. See Brilliant Eyes Probe. , r/ v& E' v4 c5 v+ I$ ?Global8 h5 ~! } t) e9 S: w Environment . |3 i$ T8 [" S( j" |The ISTC Global Environment is responsible for the creation, propagation, and ( N( M7 w1 L) A6 W( v% Kmaintenance of test scenario common knowledge, how subsets of this7 O* X8 D* T/ L, z( Y0 N) Z information will be determined, and how common knowledge will be disseminated " U% e& c2 _' x8 X( F9 ~. ^7 Hto the various element representations (nodes). The Global Environment ! _& i; |3 R: B, M' b) ]performs functions which are common to the scenario such as timing, health, * Z* i$ x: O, f! `1 Gstatus, state vectors of objects, and effects models. 2 U9 h7 c/ u9 x7 b5 \# N' f# PGlobal 0 Y2 W/ W* t) |& R# S# cPositioning ' D- W5 o, M7 E# D2 R' I( ~& _System (GPS) # t, o4 F+ E" w& bThe NAVSTAR Global Positioning System is a space-based radio navigation- f+ F1 G* `1 O u* K network providing precise positioning and navigation needs of all the military # E. u" g! P& V6 R( _services. In the fully operational configuration, there will be 18 satellites in six ) O, S: \, z; a, yorbital planes with an orbit period of 12 hours at 10,900 nautical miles altitude./ w0 q. K2 \5 e9 r) H Each satellite transmits three L-band, pseudo-random noise-coded signals, one/ L( b( j( B2 y% J4 a S-band, and one ultra high frequency for spacecraft-to-spacecraft data relay.' @( i! h5 m. ?9 {# { Global Protection+ L! ^% N: @" M Against Limited 7 C- Y& Z e) u& T# w- V$ F* SStrikes (GPALS) & K$ a5 I6 C. ~! h6 e! xOBSOLETE. GPALS was an architecture denoting an anti-missile system - q7 Y0 R- t/ A! ~0 wdesigned to provide protection against limited ballistic missile strikes, be they ' W' Y7 O/ ?4 R9 c/ j0 g7 K8 L/ s/ |deliberate, accidental or unauthorized—whatever their source. GPALS was 6 m) ^( r0 ~3 Y/ ]9 \% n) Z2 Dcomposed of three interrelated segments: (1) theater ballistic missile defenses, 0 }( @) U, v0 P' F" _5 Gand associated space-based sensors, to protect U.S. forces deployed abroad,' W0 _3 q3 A/ A. Q) M( Q0 d5 q/ N ] and our friends and allies; (2) ground-based defenses, with space sensors, to8 s V5 _ }' ?( G/ t protect the entire United States against long-range ballistic missiles; and (3) ) Q ^9 ]# ]7 \& V+ G3 q4 hinterceptors based in space – Brilliant Pebbles – capable of providing. @" J+ T, k( g- U& F6 U ~6 T( ^1 x1 N continuous, global coverage by intercepting enemy ballistic missiles with ranges2 S9 y' H1 ~2 n( x greater than several hundred miles. + r8 D! {+ \% A$ {2 F$ l! ^Global Protection: F8 f% o8 K7 @4 j Against Limited& k2 ^4 b6 [ t" V Strikes (GPALS) y% e0 E+ ^; R! O( w8 A9 M/ u3 E, RProgram/ \, n: i5 {/ |( s OBSOLETE. The GPALS Program consisted of six Major Defense Acquisition# B \' X4 V/ x4 H9 h8 d Programs: GPALS System/BMC 3 : T [5 ~5 Y# A1 E* }, National Missile Defense (NMD), Global Missile $ J& @ W+ a1 ~$ UDefense (GMD), Upper Tier Theater Missile Defense (UTTMD), Corps SAM, and ! J- L1 E4 {9 m( {+ S5 b/ O+ qPATRIOT. Army PEO GPALS was re-designated PEO Missile Defenses in 1992. 2 d6 k" y. Z, X: r3 `$ i) P4 UGLOBIXS Global Information Exchange System. * D- }/ n" q3 \9 kGLONASS Global Navigational Satellite System.1 X. C h9 z% p s9 A! t0 H MDA GLOSSARY, VER. 4.0 G 1 d- x- C8 @8 z6 f120( X8 D' ~! j* q; Q, l. z GLOW Gross Lift-Off Weight." k, Y8 V. b ~- x7 E' [( B GLP Ground Launched Probe. See Brilliant Eyes Probe.3 x: \- a* C( {8 T+ Z& M9 @ GLS Ground-Launched Sensor.8 M [6 V) T) i GM (1) Guided missile. (2) General Manager.* q8 {% {: A5 | ]/ u9 Q c. l3 k GMACC Ground Mobile Alternate Command Center.9 O2 q0 e9 h( A8 L; u9 `. n4 ` GMAOC Ground Mobile Alternate Operations Center. * \$ S0 C8 C! F/ g- |# a* NGMCC Ground Mobile Command Center.9 O0 f+ d1 G, R6 P- B# @8 u GMCP Ground Mobile Command Post. 7 b8 u+ s* I3 g9 J" g o& v- @GMD (1) Ground-based Midcourse Defense (formally National Missile Defense) (2) 9 N& @& R( p# p9 V& i# _* F& GGlobal Missile Defense (OBSOLETE).6 r2 O, O( M: [% L9 m7 k: F GMT Greenwich Mean Time.5 p: k: {9 T. c5 ? GMTT&C Ground Mobile Tracking, Telemetry, and Control. ^, h( Q8 _8 }3 `( I; j+ P% BGN&C Guidance, Navigation, and Control.3 r" _# v5 v6 L/ I GNC&P Guidance, Navigation, Control and Propulsion. - w! @& X0 i8 [0 ~/ [. g, WGND Ground.) E7 S' P/ H' k" d5 Z( E; o GOCO Government Owned, Contractor Operated.- l0 H2 o# q/ K1 M GOES Geo-stationary Operational Environmental Satellite. # ]; w) m" D( V2 a" @# N9 OGOI Government of Israel.* e0 W* X/ v- L8 F GOJ Government of Japan.

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GOSG General Officer Steering Group. 6 Y% s6 f( G0 e8 S# {8 @GOSIP Government Open Systems Interconnect Profile (CALS term).. M3 o/ c c* S" O. q/ v: O GOSP Government Open System Protocol (CALS term). |6 Y% P3 H& J' _4 O GOTS Government Off-the-Shelf.$ Z7 G: x7 H, ^4 {+ I4 i& S Gov’t Government.1 L. a) z: j: |0 H! I Government2 n/ b% E& b/ f4 | Furnished# @* K d* T4 |3 [& S$ M0 C Property % t6 H! l9 o9 y; ?5 ~: t& R+ E {Property in the possession of, or directly acquired by, the Government and2 ^( Z8 {4 ~: }6 b+ x subsequently made available to the contractor. (See FAR 45.101.)# O/ W: E: K& p Government* }$ A) `: Q9 ?8 `, E- p6 M* A Verification6 w6 s6 o8 ?4 c# @# ~7 Q Management& L, ?( a* r; q Plan (GVMP) ( I0 L0 n$ o, c9 n# xA management document that provides the overall framework for BMDS ; @' c+ F b8 i9 D. Gverification. It includes processes for implementation, organizational& {' D2 ^- l: h% h% ]. T relationships, and stakeholder responsibilities. It covers the full scope of BMDS & O. Y5 V$ y: Q+ @6 j: T$ Averification and identifies how all BMDS verification activities will come together to ! U Z0 H, V' ?8 Uconfirm BMDS capability.! E! p, c" |* Q# z* E; W MDA GLOSSARY, VER. 4.0 G & Q! U: P& y2 h2 O( Q0 b5 A121 $ C4 r, l' h9 E- L8 J! `+ Q8 @7 aGP Group.+ y- j" M, L0 P5 s& b GPALS Global Protection Against Limited Strikes.6 Y& M Z4 G. ?% P4 E# { GPC Global Protection Center. $ i4 k; e: W2 I5 [" ?( ?! qGPMD General Manager Program Management Directive. 6 _# c) p0 C" p, g# }7 k" dGPO Government Printing Office (US). 1 `. M7 t8 v$ R0 q! D6 Z% h5 SGPP General Purpose Processor. ; `& r! b8 b! Z+ p- P( E2 A/ I( [GPS (1) Global Positioning System. (2), Global Protection System.; b% T0 [6 Y5 `+ H' f3 o6 M7 c5 N5 n GPSIU GPS Interface Unit. ) A0 L# q6 d* q1 A# G: EGPU Guidance Processor Unit (US Army term). 1 N3 j/ {# S7 S' T9 y: D. c/ `1 S( EGraceful $ x3 u4 H2 m; s$ P" o0 ~7 vDegradation; J& }1 z9 O/ L* B6 f* D3 g A condition in which a system continues to operate, providing service in a . z9 \, i8 l5 }4 \* g. o! mdegraded mode rather than failing completely or catastrophically.8 k! I, ~, F" _) j GRASER Gamma-Ray Amplification by Stimulated Emission of Radiation. (See Gamma-7 J; P- X$ _" u) H8 c) t Ray Laser.) & t- p7 w( }' S" gGRC General Research Corporation. ^0 V5 X; H4 N; P9 ` Green Code Interface Software.4 [5 b: L7 H, Q* E* p0 R Ground-Based ) Q$ ]% u# J) ]4 WDefense( i' o. D7 D- Y# w The ground-based sensor and weapon systems of BMD.% E3 p% f; B: {) V Ground-Based6 C7 l( F& f7 C4 z d' X Interceptor (GBI) $ ~9 O6 Q5 x" \' y$ O9 v0 OA kinetic energy exoatmospheric interceptor with long flyout range to provide,9 l8 e5 Y& U3 F where possible, a multiple engagement capability for defense of the U.S. with a & n- c: }, g" prelatively small number of missile launch locations. It is designed to engage7 } _- n9 P# Q o post-boost vehicles and/or RVs in the midcourse phase of flight. 4 w6 {6 i( |4 R4 D(USSPACECOM) (Successor to Exoatmospheric Reentry Vehicle Interceptor* C$ I5 G2 C. U( A- b Subsystem (ERIS).) See EKV. ' Z2 a4 p8 V1 z( r& U, lGround-Based 5 T) W& \1 j7 }6 P' e9 R$ eInterceptor% P( Q2 p, T& g$ Y' q7 d Experiment4 ~3 e, K4 t! q/ G (GBI-X) - H+ C% W* F8 T5 a4 K% `Designed to infuse advanced technology and promote competitive environment 7 |& H7 c( ]0 G+ p3 W# V! ufor GBI.* I X; s# L: I Ground-Based) T9 [) ^! X9 D# G9 J Radar (GBR), R) D5 o7 m( D6 i# y A task-able, modular, multi-function, phased-array radar that provides 1 I! `1 d9 [2 L" s5 B& k4 `- R8 p# @surveillance, tracking and engagement planning data in post-boost, midcourse, 3 f. x/ D1 Q$ ~5 G$ \and terminal flight phases within its capabilities. It also provides target& K' B( J7 t/ x: Z+ v discrimination, in-flight target updates (IFTUs), and target object maps (TOMs) to 6 m+ O! {, A! yinterceptor vehicles. See THAAD. (USSPACECOM)1 |* z8 y) F1 G7 a8 K3 z0 `1 E" ? Ground-Based - K- j* j' N% X/ v I+ n9 g6 \0 H URadar Terminal2 g+ g5 b. e+ c, V& K (GBRT)/ S0 \ V2 R# N- Y1 { The sensor for the NMD system. An X-band, ground-based, phased array radar 2 U0 @9 L% Y+ icapable of detecting, tracking, and providing discrimination information to a 5 b! m, @) C& z" Bground-based interceptor.9 v: O4 O# S% T6 M. O Ground-based5 B% }: U" }) I& w Surveillance and& e) f8 a3 j; v Tracking System ! }% ?9 `# z& ]5 w(GSTS)' R, k/ R2 j- k A fast-response rocket-launched sensor, which can support the SDS midcourse' K; _( l( w; v6 E( t* ? s sensor suite by employing multiple Long Wavelength Infrared (LWIR) wavebands " V$ K: k# H' c/ Land a visible waveband sensor to provide tracking and discrimination of+ ?! @- |$ n2 s# m% V8 [ potentially lethal targets.( ?0 [3 B/ W u! ` p MDA GLOSSARY, VER. 4.0 G / d9 m3 W7 H" e) [/ Q- w5 [122 5 C. F( O& D0 v# FGround Entry ; h) T9 j/ b. X1 B7 }. y9 l$ yPoint (GEP) - R' J4 H9 A8 M+ oOBSOLETE. GEPs provide the communications interfaces between the SDS + s6 P0 R ^: ]( O+ j% ispace orbital/sub-orbital elements and the C2 E. See IFICS.7 e& @8 J. _( Z8 J Ground Mobile9 T6 d) U9 Z2 L8 e/ \ Regional 6 F/ h7 f' {6 {: b3 g& T- rOperations! X& y% L! J0 Z* I4 [' \+ o4 t Center( K- V! X! V5 V- w- ~7 N2 _ (GMROC). s4 J) [$ X4 d! j. [ F. f Transportable ground segment of the Regional Operations Center. 3 r7 N+ L3 G# e9 A TGround Zero The point on the surface of the earth at, or vertically below or above, the center8 s/ N8 M0 k/ S& {+ N9 s of a planned or actual nuclear detonation. ( n+ o# q! R% |$ {$ A* tGS Garrison Support (US Army term). 7 ~, L; b7 @# W( k! UGSA General Services Administration (US). 9 U3 X" n+ U9 i# N& ?$ BGSDC Ground Station Demonstration Lab.7 _' }6 o5 V, s9 ~ GSE (1) Ground Support Equipment. (2) Government Support Equipment. 7 P& S- J. P* r5 K) L6 o0 sGSFC Goddard Space Flight Center, Greenbelt, MD. + Q) u' P+ @* N; G9 L4 [GSII Government Services Information Infrastructure.1 M$ W1 g: x) ]4 i( J GSM Ground Station Module. / k- Y6 C8 [# b2 Q7 c/ qGSO Geo-stationary Orbit. T7 k3 E$ k: i* w7 \, C6 _GSR Ground Station Radar.' R7 t" y2 c Y GSTS OBSOLETE. A fast-response, rocket-launched, Long Wavelength Infrared. E: W5 Q, \6 U6 V9 n; \/ ~4 l. ^ (LWIR) and visible waveband sensor, which would have enhanced the * S( s+ Q9 r: N# E9 minformation available from the SDS’ midcourse sensor suite by providing tracking 8 w/ g. ?, B$ z8 J) {( {and discrimination data on potentially lethal targets. 1 J( ?: G l4 E, H: S+ J9 E, b! @GSTS (F) GSTS Farm. 3 \. O" q# I" U3 n2 T, V9 K6 uGTA Ground Test Accelerator. # f# O0 \& z. q$ y0 N: P; sGTACS Ground Theater Air Control System.& T% y5 c7 V- X9 a; g GTE GTE Corporation. w k8 q' J! L3 a; ?! d GTF Guided Test Flights. + V6 a- @3 |8 h, k& KGTM Global Track Manager. # M- r9 }3 K" w* v' M0 s B1 p fGTN General Technical Note. 9 A8 h5 i% X4 X& i! zGTR Gulf Test Range, Eglin AFB, FL.0 U: N6 z# M( ]+ W3 q- S/ Z5 a- u GTSF Guidance Test and Simulation Facility (PATRIOT), Huntsville, AL.2 ]& O$ ` P7 ^% ] GTV Guided Test Vehicle. 2 @) e& G1 ^/ |GUI Graphic User Interface. : F) g4 H! Z5 ~. D8 i6 n/ wMDA GLOSSARY, VER. 4.0 G; w7 b; |0 G6 {) P8 v 123 / X/ S& x, _. XGuidance (1) Direction, altitude control, and navigation (where appropriate) of sensors: O, w' Z0 V+ l" P7 } or interceptor vehicles. - u4 E" ^- D* V: _/ p% r(2) The entire process by which target intelligence information received by a9 `# n4 Y4 r, J l+ U guided missile is used to effect proper flight control to cause timely 1 ?* q- U) K8 s+ X- U; Gdirection changes for effective target interception. ; Y1 {, m4 S8 ~8 ]5 K: eGuidance " {8 S6 `3 z2 @. v- HEnhanced 7 a1 k4 {' H8 T; d" dMissile (GEM) ! U( p, b4 D, w4 IA companion program to PATRIOT PAC-2, which includes enhancements to the3 x0 ^8 S$ S5 {: I: u radar to increase intercept range and performance. 8 ^, z' ^' O2 }+ G) u0 |6 A4 ^% YGuidance 3 Y- j: n' z( {8 A) r/ QSystem (Missile) 7 }, s; {; R4 z" tA system, which evaluates flight information, correlates it with target data, # b3 H5 Y, G2 X0 ~8 hdetermines the desired flight path of the missile, and communicates the 1 P7 x8 _4 e) p# y% F& X* Bnecessary commands to the missile flight control system.+ K/ {3 i3 r" X! _ Guided Missile An unmanned vehicle moving above the surface of the earth, whose trajectory or 1 C, j% n. s" M" Dflight path is capable of being altered by an external or internal mechanism.% g+ [( N! t7 [* i, q/ |+ E0 ~ GVSC Generic VHSIC (Very High Speed Integrated Circuit) Spaceborne Computer.& i2 e/ O) P' N! E/ r GWAPS Gulf War Air Power Survey, 1994 [a DoD-sponsored survey].$ F Q9 ^) m+ R, A# |, d Gwd Giga watt-days.: U" k9 v; G; x' N7 \ GWEN Ground Wave Emergency Network.3 A9 H3 a' `) Y4 f& C; i GZ Ground Zero. ' ^/ u: O4 n! aMDA GLOSSARY, VER. 4.0 H7 W' W) G) \3 O' `/ w 124; `& Q4 F X+ w3 e H Hour. 7 b- o3 o; Q: x8 o0 lH&S Health and Status. " s2 v U6 t* a: u9 C+ }H/W Hardware.( x! _2 g, X6 x' i: b HA Higher Authority.5 D: Q! [1 B' M, C' A& o HABE High Altitude Balloon Experiment. 3 ^. {! s% Q" x o& K% Z5 f+ sHAC House Appropriations Committee (US).# z z1 { K6 E HADS High Altitude Defense System.; \0 `- S, E: t1 l/ O Q3 S7 J& {( U HALE High Altitude Long-Endurance. ' o' ] x, L! m+ bHALE UAV High Altitude Long Endurance Unmanned Aerial Vehicle. $ V0 X4 J7 A: V2 C, M, g5 ~2 Y) SHalf-Value2 u. f$ I: C) m7 X( u Thickness (HVT)! n0 r7 z: ^) i; @6 n8 c The thickness of a given material, which will absorb half the gamma radiation ' g% d" S8 T$ [( Y' y7 g, xincident upon it. This thickness is inversely proportional to its density and also ! E8 e% K# Z; o8 _) ~, sdepends on the energy of the gamma rays. W, W1 }4 l, _) ]0 F1 r HALO II High Altitude Observatory II- E/ R" S; D4 \$ f8 M8 J HAMS Hardness Assurance, Maintenance and Surveillance. 2 y$ F5 t+ K7 U! f0 V* X5 P( e n% _Handoff This occurs when information on positions, velocities and tracks are given by one: R- M5 r. j. L; S sensor or system to another and the first sensor or system continues to track the6 r+ m% u2 Y% P8 h+ V objects. $ J% W, v; F. A; XHandover This occurs when information is passed on to another sensor or system in which" Q6 a+ `8 E9 O, y' ~3 M6 Y& o/ B the first does not continue to track. ( i+ [/ Q _4 z7 THAOI High Altitude Optical Imaging.

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HAOIS High Altitude Optical Imaging System. . w% Z" T# l6 H8 E( NHAP High Altitude Probe.' c) Z, e+ Y: t/ P: b @' {2 W Hard Kill (HK) Destruction of a target in such a way as to produce unambiguous visible7 R) i6 x. M4 g. g$ s d6 U evidence of its neutralization.0 w: q3 K9 \& \9 t# e. y" w- a Hardening Design and manufacturing process and other measures, which may be employed7 _) e$ O0 G. c6 \% _ to render military assets less vulnerable. - j1 J: U5 t9 b' v- _HARDMAN Hardware/Military Manpower Integration (Navy ILS term).# e% V+ h6 u: v x1 w5 d% B Hardness A property of a target; measured by the power needed per unit area to destroy( m# @# t) P: D) I6 @, Y R4 Z# F the target. A hard target is more difficult to kill than a soft target. E$ i- c& [# Q. jHardware-in-the-/ @( X- |5 o+ G4 p6 l5 B Loop (HWIL); k5 T3 _ ~6 h: J Tests in which BM/C3 computer and communication test systems will be in& q2 S, X; h* K$ _% @( e communication with some of the hardware test facilities developed for other BMD 9 I- ?; ^! F1 q+ e5 \/ J+ T; Dtechnology programs. - ^9 d! G+ E' L6 N! F$ U. w" CHardware - K$ [+ M3 T, {) b5 _3 YSecurity0 T/ _( z1 D9 C3 f ^$ q Computer equipment features or devices used in an ADP system to preclude 7 ]" B" g/ i z% `3 q: [unauthorized access to data or system resources. 4 N: \; q; `6 l. yHARM High Speed Anti-Radiation Missile. 5 x& y% [9 k9 R1 A. s) ?MDA GLOSSARY, VER. 4.0 H . n4 p& Z# y8 [125# T" q+ l" f' r% u$ Z HASC House Armed Services Committee (US). 7 Y- {. t( x, ~+ {* V: sHASP Hardened Ada Signal Processor., h4 }/ x* R9 o6 H% ` S HATELM High-speed Anti-TEL Missile.0 b, G s- e% m* `! o HATMD High-Altitude Theater Missile Defense. (U.S. Army)4 U o3 m$ B6 w, z$ [4 D) R HAVE STARE Name assigned a proven sensor capability.0 I6 A& ]' p( U; a% d* W HAWK Homing All-the-Way Killer.( ~) m, @) c4 I3 z; i9 u HBCU/MI Historically Black Colleges and Universities/Minority Institutions./ v) W/ v- D: b HBHO Hard-body Hand-over [algorithms]. 2 ]6 u+ U/ [3 I G! Y! ^+ s& m3 tHCO High Consequence Option (Safety Engineering term).* g# y# T+ p8 T* d HCT Mercury Cadmium Telluride. 7 i' z8 P u3 K- SHDA Hybrid Detector Assembly. + T2 h: I8 f. C/ PHDBK Handbook. v7 r: d$ I2 N& I U HDR High Data Rate.0 d8 }% M0 Q+ Z' r `3 u* h HDX Half Duplex (TelComm/Computer term).+ C2 ^$ m- V/ {+ K! y HE (1) High Explosive. (2) High Energy.* e; f" Y! P# R! J6 x Health and Status; ]; z2 R* z2 t* @ (H&S) : f: Q7 D- I* V1 J% MHealth and Status pertains to a unit’s ability to assess the conditions of its, V6 E* l+ R2 P2 P subsystem functions. The term H&S is used for units in remote locations, such2 O% ~* S1 w$ A( x9 W as satellites, where ground controls must interface with BITE to determine 7 d. O+ @0 q4 V' O% ?operational status of the satellite and its equipment.& f& C8 n2 n8 ]9 j( e4 v; S x Heavy Replicas% @0 A: ]" X( X# m (HREPS)3 h$ \. l$ Z& ]9 J7 u' ?) z Decoys, which by virtue of shape, size, and mass, closely approximate an RV’s $ n# j5 z0 u, y* M1 i, Gsignature. HREPS have significant off- load penalty. 5 x, I( M/ b- k' W( wHEDI OBSOLETE. See High Endoatmospheric Defense Interceptor. , t `* R7 P$ p6 C& ?6 i rHEDR High Endoatmospheric Defense Radar./ Y9 ^/ Y7 v0 A8 K; M HEDS High Endoatmospheric Defense System.* Y+ ~* N7 _4 H" j8 d& Y/ r/ Y HEI High Endoatmospheric Interceptor.1 D" u+ A0 `/ y HEL High Energy Laser.) z$ q# Q- Q: |) Q HELKS High Energy Laser Kill System.( ?+ ?6 R8 D9 W$ J. `8 {0 s0 U( V HELLO High Energy Laser Light Opportunity.4 r. }( b ]. p- O HELSTF High Energy Laser Systems Test Facility. 8 K$ L5 Q+ J( g% R! hHELWS High Energy Laser Weapon System. 2 C' ~3 [5 s. \. uHEMP High Altitude Electromagnetic Pulse. : C+ E) A/ u; ?8 `* m4 ]; J2 B9 h/ ?MDA GLOSSARY, VER. 4.0 H: z% o8 K& k4 w( S4 ]/ F 126 7 S$ {3 D* t: O1 S" dHEMTT Heavy Expanded Mobility Tactical Truck (US Army prime mover).3 Z/ `3 U! J6 E. I- z% C# ] Hen House Soviet area defense radar used as a component of the Moscow ABM system# {5 `1 t! \5 _* f- o. L that provides VHF coverage of space to monitor orbiting satellites and early, p# G" t: T u! }2 a0 K warning of ICBMs launched from the U.S. y7 d/ @4 v2 G1 D6 B* t7 c4 E- \ HEO See High Earth Orbit. , g9 U* v. t" s0 Q6 Q3 ?: DHERA (1) An improved surrogate TBM test target. 1 [% B# S s; ?# p$ e- i7 c(2) Two-stage, ground launched solid propellant theater target vehicle. (MDA 1 \% n9 }* H6 h, ZLexicon)( B" j/ C9 ~0 U HERO Hazards of Electromagnetic Radiation to Ordnance (SM-2 Bk IVA). % h! k6 Q% C, @4 `. OHESP High Efficiency Solar Panel. 7 J9 l$ h" {" K, x5 z# bHEU Highly Enriched Uranium.% s$ i4 f! y4 b5 H. }, E HF (1) High Frequency. (2) Hydrogen fluoride.. Z; ]+ R+ |& Z% `& S: U# c HF/DF (1) High Frequency/Direction Finding.( ?$ ~8 a1 F& L0 C2 c (2) Hydrogen Fluoride/Deuterium Fluoride. (Chemicals used in IR chemical. u2 b- F" V: u) Z lasers).$ P! h/ K" L9 ]0 S6 P HFCNR High Frequency Combat Net Radio. 9 @4 |: ^: c7 t9 wHFE Human Factors Engineering. ' ^1 Y% G7 E) m7 R+ M' s: M% |HgCdTe Mercury Cadmium Telluride.. N- _7 L5 J9 D+ x2 u- V6 q HHB Headquarters and Headquarters Battery.$ L7 Y; c; F/ c5 k HIBEX High-Acceleration Boost Experiment. % K5 y+ P' ?, rHIBREL High Brightness Relay. 2 C; L. z/ n# }$ ]/ d, nHIC Human-in-Control. , v2 |2 I, s& pHICOM High Command (Navy term). 1 S+ u0 d4 ]9 I2 n' l/ d6 U* yHICTB Human-in-Control Test Bed.8 ~1 d* `( A; }$ y4 q" ` HIDACZ High Density Aerospace Control Zone. ( Z1 U7 `! G* z: U8 wHIDAR High Data Rate. ( `, O; X+ I" i2 `2 A7 |+ [" \High Earth Orbit ' A, X5 [# K0 X/ e(HEO) ) R: n7 S0 s! @# C, Y7 [An orbit about the earth at an altitude greater than 3,000 nautical miles (about & ^! v4 S! b. {( ~5,600 kilometers)., a( h% e* E, x High4 U/ {7 z. c" b0 ~2 z Endoatmosphere+ ~) g3 ^1 G- a" i) g' A% W* c j That portion of the earth’s atmosphere, generally above 40 km altitude.& J6 E3 b$ ~7 W' C High 2 I/ R. j; p# s' K3 s9 k8 zEndoatmospheric : D4 G, A- Q1 Z' @$ GDefense , P) y* F( |, I: i& hInterceptor (HEDI) & d4 x, M: n9 n& BOBSOLETE. Interceptor concept designed to engage RVs within the (upper or, S3 Y/ Z8 Y+ ~ high endo) atmosphere. (Predecessor to Endo-Exoatmospheric Interceptor/ p+ Z* I( Q: g2 r3 L (E2I).)- p [' G* E) J+ E6 g; r# { MDA GLOSSARY, VER. 4.0 H : b; j* |3 ?8 ]' g3 r. F127 ' y: J# E) Q% o Y0 e' ?% r9 rHigh Density3 \ x6 }! y3 g2 y7 C9 W3 T Aerospace 4 X7 u/ R( [3 XControl Zone + m( p& H/ @4 J! o+ P* T(HIDACZ) + e1 n" R* O$ \/ e3 x+ U( L* ZAirspace designated in an airspace control plan or airspace control order, in; @% U: ]3 y! O! t7 N, V4 B which there is a concentrated employment of various weapons and users. A# t4 T5 r& J5 R7 f) } HIDACZ has defined dimensions, that usually coincide with geographical 4 Q- j' B# N/ p# rfeatures or navigational aides. Access to a HIDACZ is normally controlled by the + }6 D% D, G* ^6 zmaneuver commander. The maneuver commander can also direct a more ) q$ _: r" j9 x" c# f; xrestrictive weapons status within the HIDACZ. $ h) j/ V* k/ c) u, yHigher Authority) Z7 q8 S" z8 p6 ]% j2 E5 w4 N Interface 2 e% u. X, H; i7 pPolicy, strategy, doctrine, readiness conditions, and rules of engagement from+ O V9 L, a, r% z( f, Z9 G3 l higher authorities for use by the defense system in conducting system : ?, W7 K3 ^7 A5 \0 g+ ~operations including specific orders specifying actions such as testing, defense * I* s8 W! E- t. H$ `4 \( y& `enabling, pre-delegation of authority, etc. Also the reporting of situation1 s; m- O+ l7 G5 D& _, ?1 m" c assessment and system readiness to higher authority.) Q# Y8 x7 X, ?0 L High Order- E r0 r. d1 H+ E5 t* x# C Language (HOL) ) b3 K% a6 g( L) c$ B; p4 ]A programming language that requires little knowledge of the computer on which B. j% b' [' h$ Y; F5 o( G8 f a program will run, can be translated into several different machine languages, 0 X, e) v r* C, x7 Qallows symbolic naming of operations and addresses, provides features4 @" ]; c" X! L; ] designed to facilitate expression of data structures and program logic, and& V* K6 o/ U/ _ usually results in several machine instructions for each program statement. 0 T* p2 ^: G' a6 R# w. Q3 h. tHIL Human In-the-Loop. / l' d7 f% L6 b3 ]$ `% XHIMAD High to Medium Altitude Air Defense. 4 @0 ]6 a" t) M1 xHIMEZ High Altitude Missile Engagement Zone.. X+ D% a1 }6 [8 w1 H% y4 t HIP Hot Isostatic Processing.! g* u& d! v" g# k0 P1 E2 h HIRAM High Resolution Infrared Auroral Measurements., A0 h+ a4 [, }0 L O" ?, s! F; U+ I7 C HISEM High Speed Environmental Multi-burst Model.) T0 C( }" U, }; } HIT (1) Heterojuncture Internal Photomissive. (2) Homing Interceptor Technology.3 j# j& E% u: i# j HK Hard Kill. - D( A m Y A7 c$ bHKV Hit to Kill Vehicle. ; r( J6 A8 Y+ L1 Y" OHLD Hardware Description Language. ) s; Y" ?0 K |5 R( N1 dHLLV Heavy Lift Launch Vehicle. q9 L1 M' ?1 _! [7 H# w# BHMC&M Hazardous Material Control and Management., L( w5 [) r( \ HMI Human Machine Interface. ' O3 H' C3 F( Y! z8 a* o* p6 XHMMWV High Mobility Mutli-purpose Whealed Vehicle (USA term) (pronounced Hum Vee). / E0 N7 a6 g2 ]+ R! SHMPC Hazardous Maintenance Procedure Code.2 [, m ^2 t3 w/ W4 I HMSC Hughes Missile System Corporation. ! T' t q/ x& Y& k4 B$ LHOB Height of Burst. $ t# v, O: z* S0 }9 gHOE OBSOLETE. Homing Overlay Experiment. (Predecessor program to ; c, N5 @; k8 s8 c$ N8 [( f1 @Exoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS).) ! p7 r, D( j0 s% J `9 vHOL High Order Language.0 V' \' H6 Z' Z2 w4 [: l MDA GLOSSARY, VER. 4.0 H0 n5 s" p9 x! x3 X l! [ 128 & n- ^# s% Y! n. z1 ^2 L4 s$ eHoming All-the- - d7 a& b) ]* S3 E1 w% g2 pWay Killer0 q: Y: H& _2 @2 W (HAWK) + j* y! _2 l$ H, g% j. d3 K- [8 a(1) Upgrades to the HAWK interceptor and radar system to provide the3 R; ^: Z+ g5 w. C& z Marine Corps with a mobile point theater ballistic missile defense# [+ G* i% [7 I8 d capability. ; P3 }$ d( O, G(2) A mobile air defense artillery, surface-to-air missile system that provides : ]& N) K& a6 k! c6 D" r( K+ H$ pnon-nuclear, low to medium altitude air defense coverage for ground5 z% Q; N1 e8 ^; [: a2 r# g forces. Designated as MIM-23.2 i# d$ }& ?( V0 W, W Homing Device A device, mounted on a missile, to aid its guidance to a target. The homing 9 y0 w: E% E I H: R/ k1 D tdevice uses sensors to detect the position of, or to help predict the future ( L. U' o+ a. A' }' P6 {position of a target, and then directs the missile to intercept it. The homing7 M& n* h6 K$ I. F. i* z" b device usually provides frequent target position updates during the flight of the 8 G, f. \' P3 K3 ^missile. ' w5 J$ E5 T1 I, K* |/ ~$ e9 `/ KHoming ) V3 D- X7 i. q" z0 tGuidance1 `- r" y V5 o& t A system by which a missile steers itself towards a target by means of a selfcontained mechanism which is activated by some distinguishing characteristics of% _* k6 ?: K+ L* P( j1 z the target, such as an infrared signature.! m7 P, l" s; M! h HOMS Homing Overlay Mission Simulation.5 d9 a$ l& M' P l1 [( f HOST Hardened Optical Sensor Testbed. ( ?3 c. M1 V2 @1 D3 @Host Installation A designated DoD facility that provides non peculiar SDS support of SDS : }4 \. b6 i* q% felements. - N9 h& F t' ~* A# kHostile& J% }1 q$ Z& ]& I8 Q+ M: V Environment & ?1 w7 n8 C! T! r) o+ jThose environments that result from a BMD system engagement of an enemy4 b' z, w1 F! c- n4 Q9 C G; x threat or collateral conditions resulting from deliberate hostilities. Hostile " k4 J( ^7 h* F5 O$ p# S lenvironment categories currently applicable to National Missile Defense are 6 \( u& z- _' Z0 \Nuclear, Battle Debris, and Electronic Warfare.& i- @6 ^: U1 q8 N Hostile Track The classification assigned to a track that, based upon established criteria, is / m- l% b4 | F. n3 Zdetermined to be an enemy threat. V! p0 n. H! A. D4 K1 o' S Host Interface The interface between a communications processor and a host computer.1 G {; R; z9 F5 p Host Nation . y3 O, G/ L p. W5 tSupport: ~5 G# q1 X5 r" s+ S Civil and/or military assistance rendered by a nation to foreign forces within its. x/ }, h3 b# A" O8 N$ \ territory during peacetime, crisis or emergencies, or war based on agreements; r( c* o- {2 S; \ concluded between nations.3 m7 J7 q/ ]4 r! e: R hp Horsepower. 6 \$ V$ H& u0 RHPA High Power Amplifier. ' U- F, }) X$ [" b" OHPC High Performance Computing., ^5 L2 b( }+ e- p: \ HPCC High Performance Computing and Communications.4 v. G7 j( x$ H6 I9 H3 F* E HPG Homopolar Generator. & e. S+ ]6 X& oHPI High Power Illuminator (Hawk).+ Z3 w2 V; G2 `! g/ n+ l) s7 I! H HPIR High Power Illuminator Radar. " H- \0 t- G( N* t o2 HHPL High Power Laser.6 o- k& _7 D) M" |* w HPM High Power Microwave.6 R6 D- Y$ O9 ]( S6 j& n HQ Headquarters. ! B& B6 @" s" JMDA GLOSSARY, VER. 4.0 H ; ]' A- P: T. j4 \8 ~, J129( s4 j. G% _' T ~1 P, Q' v/ Z, e0 Y HQMC Headquarters, Marine Corps." M- ~" e+ e0 Y( Z+ y9 l( O HRDS High Resolution Display System. " R, O2 L$ K7 k" j. w ]* iHREPS Heavy Replicas." B' _% a* l, u$ w HRR High Range Resolution. 7 f/ w7 p# e4 i* aHRSA HICTB Requirements, Support and Analysis." z5 C3 l V# F/ A8 z' f) | HSDB High Speed Data Bus (TelComm/Computer term).* [. b4 `) c D; Z0 A' E HSFB High Speed Fleet Broadcast (Navy term).+ n( [) U3 s, `, w0 Z( c/ w6 W/ X: A HSI Human Systems Integration.4 L+ V1 n" B, ]5 O& i HSV Huntsville, Alabama. ) O9 o$ v& p7 T8 jHTICIA High Technology Crime Investigation Association.5 i5 g' X! r3 \# `0 _ HTI Horizontal Technology Initiative.) W* a! g0 N# {# B5 b+ |& L HTK Hit-to-Kill.) p* p4 [, \0 W9 t( z1 ~# t HTMIAC High Temperature Materials Information Analysis Center. ' F4 D. b! a5 Z9 w$ z; T1 LHTML Hypertext Markup Language.) w* |* {) o3 T" m0 h7 `1 A HTPB Hydroxy-Terminated Poly Butadiene. 9 @% [& L: {4 o8 ?HTS (1) High Temperature Super-conducting. (2) Hawaii Tracking Station. * `6 Y1 e, _# G, L; E! B5 D6 Q8 lHTSA Host Tenant Support Agreement.- o! p3 G, r# F% X' K+ d8 i HTSS Hardened- sub-miniature Telemetry and Sensor System. 9 E9 Z+ c5 H2 m, K w) W) p, [2 UHTTP Hypertext Transfer Protocol. . l7 u* g+ N' ~6 l6 EHUD Heads Up Display.' J7 H8 D. C/ @3 W& M3 } Human Factors A body of scientific facts about human characteristics. The term covers all2 H L8 G# a7 L3 D. w biomedical and psychosocial considerations; it includes, but is not limited to, . ~ q, x5 m5 Z8 j' jprinciples and applications in the areas of human engineering, personnel8 u7 N3 D, P" u5 _( S+ C/ k selection, training, life support, job performance aids, and human performance $ y6 z( d; Q) r$ e$ T: l+ E8 J# bevaluation. $ \$ Q6 [, _) `' |Human Factors / ~" k# N. _' U/ e6 OEngineering9 F' b. M: O2 n1 j9 ~' F% G The design of man-made devices, systems, and environments to enhance their X0 L' s T" i3 @$ u( M& ]* |use by people. Also called human engineering, human factors, and ergonomics.

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