航空论坛_航空翻译_民航英语翻译_飞行翻译

 找回密码
 注册
搜索
楼主: 帅哥
打印 上一主题 下一主题

航空缩略语词典 [复制链接]

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.1 q- h! a& M) ^& r ELS Earth Limb Sensor. , ?0 t u' _2 |4 c" y) GELSEC Electronics Security. 8 S# ^# B: D dELSI Enhanced Longwave Spectrometer Imager. & B, ?" V7 B+ G5 VELV Expendable Launch Vehicle.4 U2 E& v6 B) m% e( i3 x3 U Emanations 3 {2 w: z+ w' g* N. ASecurity 6 K7 _$ x) w& \8 u(EMSEC)9 B. N; q9 V. { The protection that results from all measures designed to deny unauthorized ' r/ P; D! _7 |" |persons information of value that might be derived from intercept and analysis of * \$ B. R; ?1 Z3 i, hcompromising emanations. # e! A9 b1 N! ~7 ]! f% y) eEMC (1) Electromagnetic Compatibility. (2) Early Midcourse.8 E2 u1 I+ v) g* [6 v' D, D EMCON Emission Control) p2 p9 ~+ \7 r EMD Engineering and Manufacturing Development (previously referred to as FSD). ) p: h# J1 X. A5 R9 f" ?# HEMDCT Expanded Memory DCT.6 b0 B# ~5 ?, \, S' I8 ~ EME Electromagnetic Environment. A% G& T# n6 Y6 e6 `" v' m( g MDA GLOSSARY, VER. 4.0 E& W* A5 ^& c% |( U 930 \4 v! u% ?0 ~4 @4 p' N7 ~. P Emergency* Q7 ~ }+ }) Z( L6 X% _ Capability 4 i( s2 j9 Q0 x! z- Z5 r(replaces ; T Z' i& O, G- {! @( DContingency 4 |4 K* q, z1 z, l9 t, rCapability) 5 y$ L1 p: `; C0 ~3 I+ |BMDS elements or components that are still in development or testing that0 v; j9 ?9 B3 \. f# O provide limited ballistic missile defense capabilities. MDA, working with the2 M+ |& G. n4 S- n Services, will develop plans, which cover the potential use of prototypes and test 6 J4 a# `& c: t% l) Cassets for contingency deployment should the SECDEF determine that an 2 a# v" X' m1 N+ Gemerging BMD threat requires emergency fielding of a BMDS capability.' Q/ \( L+ K7 j/ }( d7 h: S* F EMF Electromagnetic Field. * T% l F6 ?- H$ REMG Electromagnetic Gun.$ D8 b/ _( _ F7 \# i( Q1 e8 b EMI Electromagnetic Interference. ) [) v3 O, ?' \- D' [EMIP See Exoatmospheric Midcourse Interceptor Program./ G4 N- N1 W( k0 L: U$ `! R9 j Emission Control' c* [: y( v: X( Y6 c5 a (EMCON)! \. _9 \, W# {6 l- A The selective and controlled use of electromagnetic, acoustic, or other emitters 0 ]) H( @0 d. `to optimize command and control capabilities while minimizing: a) detection by ! e# `- X+ V# X$ M: e; a8 Zenemy sensors, and b) mutual interference among friendly systems. EMCON + H$ z6 }0 J. [, [2 D) Ucan also be involved in military deception plans. Also called EMCON. - E9 ~$ j3 L8 r% lEML Electromagnetic Launcher. A device used to launch hypervelocity particles.3 a; j) c% ` R7 Q' B4 {8 ], k EMP Electromagnetic Pulse. " k: O9 V4 F* H7 t8 pEMPSKD Employment Scheduling (USN term).2 O, c4 g9 u+ ^. b EMR Electromagnetic Radiation.% M( B4 `& A# G% g# O9 m9 u: V- K EMRLD Excimer Moderate Power Raman-Shifted Laser Device.) U" s( \: E% A- [+ h1 _ EMSEC Emanations Security.- T: s$ W" H& B2 ]8 f EMSP Enhanced Modular Signal Processor.6 |8 ]3 H& ?; q; b9 b- E3 ?: u EMT Engineering Management Team.# L" p5 X1 C1 c) L3 E+ V EMV Electromagnetic Vulnerability. ) {. \& k( w( ? \ENA Engineering: Architecture and Analysis. 0 `# J3 b+ E4 CENCATT Engineer CATT (US Army term).8 z0 x# P. E2 x: U4 Y( U Enclave Isolated resource – an SDS asset that has lost connectivity with other SDS 6 {! z9 P* c1 y4 T) R+ e* ~: Dassets with which it normally has connectivity, but is still capable of coordinating 6 @5 Z3 K, w1 A" {4 X7 Q5 j9 Iwith SDS assets to conduct ballistic missile defense. Various combinations of7 L0 q' g1 B6 Y- \: E" @ connectivity losses are possible; for example, (1) an operations center has lost 3 k, y3 ^4 n; iconnectivity with Higher Authority, yet can still provide sufficient C2 and can still6 C% h1 p8 z( v' _$ t1 ?8 Q connect with sufficient weapons and sensors to conduct an engagement and (2). b6 E0 V& a. Q# h an operations center has loss of connectivity with another operations center with' Q k, o+ p7 K# m which it normally shares data, but can still conduct an engagement.* r% u& f6 ^/ ?5 g& K Endgame FOV The field of view of the interceptor’s sensor during its final maneuvers after target' p5 L4 {, ~) H' S6 z8 R acquisition to intercept the target. May be less than the acquisition FOV.8 n. W4 Y" C' G End Item The final production product when assembled, or completed, and ready for) R7 \! E2 r. m' J5 r2 P issue/deployment.5 ]9 H8 q+ {9 E+ y MDA GLOSSARY, VER. 4.0 E 2 N% j# i2 m! \$ e8 N8 g9 e94& G! }+ U! \4 ]6 Y Endoatmospheric Within the earth’s atmosphere; generally considered to be altitudes below 100# d1 t0 R# q0 |. z7 I- o3 s km. An endoatmospheric interceptor reaches its target within the atmosphere. b6 S& p# K; q" ]& V Endo- 0 O3 O m# V, }: J& X* p, uExoatmospheric 6 z* b- g/ m% D/ `" i1 ZInterceptor (E2 I), D& @& U p b W A ground-based interceptor capable of engaging RVs either endoatmospheric or, i# I. W5 A, b" M! F: v5 z m exoatmospheric. (Successor to High Endoatmospheric Defense Interceptor: q |5 a) J* [4 ~) @% G+ Q' V (HEDI).)3 V; z2 {+ g4 Q9 Q ENDOSIM Endoatmospheric Simulation. + S+ C9 T# t" H8 `Endurance The time an aircraft can continue flying, or a ground vehicle or ship can continue/ i Q/ G; |' ^ w; G5 I operating, under specified conditions, e.g. without refueling.& q$ D$ ~ D2 V/ k& k. V ENG Engineering. : b% c) J( Q+ GENGAG’T Engagement. * M: x# j3 F! c3 i: q" CEngage (1) In air defense, a fire control order used to direct or authorize units and/or- U7 D+ |' ~4 g& e ~2 b weapon systems to fire on a designated target. $ Q5 f! W. f3 F; c(2) In air intercept, a code meaning, “Attack designated contact.” 1 {/ N4 S1 u9 VEngagement (1) A period of hostilities beginning when the first ballistic missile target 1 z. g6 x1 f0 @5 I) v" X7 ]% _$ cundergoes fire from the first defensive weapon.& ^0 O5 U( x% l+ ~9 j; e (2) A period beginning whenever any hostile object is identified (designated) , j p+ o h- h: H) ?as hostile and ending after the last hostile object has been attacked. ' V9 u- ]/ I. n* B6 M6 R. X(3) In air defense, an attack with guns or air-to-air missiles by an interceptor K9 P) j- [" Vaircraft, or the launch of an air defense missile by air defense artillery and & o4 B' T+ z7 sthe missile’s subsequent travel to intercept. 9 g% w8 ]" d) w5 a6 S( ^7 d" MEngagement * O' ^( O8 }- h9 n6 s9 o CAuthorization& s B, ~; T9 _% B9 }, W The authorization given to USSPACECOM to use weapon and sensor systems 0 E# O5 ^! S4 i# Runder previously coordinated and authorized rules, procedures, and conditions.4 P3 m) B3 A$ b. P Engagement $ t/ K- X3 S) E9 N1 xControl! n R( V @& i& j9 i (1) That set of coordination, assessment, decision, and direction functions : [2 ~* f B Bnormally implemented automatically to execute the selected battle plan, ' P2 w9 y5 O6 K R8 l% L+ K/ S( smilitary strategy and tactics within partitioned battle spaces (i.e., a ' M( C2 e) }: c- m6 aspatial/functional subdivision of battle management). Includes the% \8 X- ?6 T! z* X" w6 u determination of: what specific objects to intercept in order to implement . k4 v2 W) d! q4 V% [' @" r5 Lthe selected military strategy, and which specific interceptors to assign to # K( V9 G( e, H0 R" peach attacker to implement the selected tactics within the rules of0 V) ^0 J3 ?! D( k# F engagement. : q8 u, q5 U( z(2) In air defense, that degree of control exercised over the operational+ O8 I! \& Q& Z; W. ?# m functions of an air defense unit that are related to detection, 0 N1 L3 o, i+ {/ }0 ?& kidentification, engagement, and destruction of hostile targets.

使用道具 举报

Rank: 9Rank: 9Rank: 9

42#
发表于 2008-12-25 20:05:49 |只看该作者
Engagement3 R8 Z% o9 t4 S) T0 u" X Planning 3 @" ~1 ~' e) F6 t0 k% q( MA set of rules and parameters to be used in developing weapon-target 1 S- m3 p! l5 Lassignments and for sensor resource management. (USSPACECOM)3 S L$ g% C# K9 L- u0 g# ^ Engagement % v; E4 J6 o: S3 qSurveillance ' b; n1 A; i% P/ r6 JThe surveillance required to support RV negation in the midcourse tier. * W# B; N- R" X9 m7 g+ j& {Engagement 0 k. u* {7 b5 S( Z/ n" q+ J: J' fTime / `' m* W4 }# l8 p6 {% ]The time that a weapon takes while engaging a given target. This includes not6 _- b% f# D- S" v only firing at the target but all other necessary weapon functions involved that0 u: o; W( c" q3 R! n9 L6 p are unique to that particular target.7 K# h% V2 v: w" R* } MDA GLOSSARY, VER. 4.0 E . O' c9 r6 ]% f, g9 B( X95 , E. A0 ]* g$ E3 d" c* cEngineering and4 E3 s3 ^. _8 m; v, d Manufacturing - o+ X6 E6 `9 g+ P! _6 ?5 X$ FDevelopment$ ~& \ H4 a2 \1 B# y' I (EMD) 2 z+ I _7 O9 l" l" ZThe third phase in the acquisition process, following Milestone II. The system3 b6 ]+ d# A S3 l% n, ~ and its supporting items are fully developed, engineered, designed, fabricated, 7 y3 [/ J8 l' m9 |+ X8 Xtested, and evaluated. The intended output is a pre-production system that ) ^4 G0 [1 c7 Kclosely approximates the final product; the documentation necessary to enter the1 [3 j* k$ Q3 Y8 R- ? production phase, and the test results demonstrating that the production product % S' l' ^% _0 m5 u5 U# dwill meet stated requirements. 6 @: ^; |4 ]9 D$ _Engineering( _$ U* g+ u. [; d' \, u' u Change Proposal ; A# s/ O( F8 L# s- @0 R0 H2 R(ECP) # K. A% M' u9 R5 J: cA proposal to the responsible authority recommending that a change to an: o/ e5 n9 P1 \* b9 M# ?7 k original item of equipment be considered, and the design or engineering change9 P/ F6 c: {5 x- L2 s/ S be incorporated into the article to modify, add to, delete, or supersede original ! F l) {" e* N) x! N) Vparts. - o+ q' ~5 D( b; m8 mEngineering 8 M1 u7 ]. k2 kDevelopment0 Y6 x5 @; u; q A funding category including those development programs being engineered for B! q1 s6 c* S+ W: y- U" Z; A" u+ z) M service use but which have not yet been approved for procurement or operation., S2 ?9 |& P+ e/ d1 q Money under budget activity 6.4.- B) w% I6 W+ k& D3 K% h' ` Engineering- o& Z$ A6 e. k* N2 O Development& Y% F% Y* R7 c: Z2 `' P Model1 L5 a$ j% L; w* D Enhanced Target " d: Y w, h+ y/ Y9 Z- [Delivery System 5 ]. y ~$ S6 ]' C( v1 q(ETDS) 6 i5 e0 o& G0 W! @# {3 tAn advanced prototype used during the Engineering and Manufacturing7 d0 S( F- s4 V# c; i Development phase (EMD) to resolve design deficiencies, demonstrate maturing6 N$ ?6 \: ?1 m! x& L- D performance, and develop proposed production specifications and drawings. 5 e# R, j9 r7 u/ u6 CTarget delivery system being developed for future GMD testing that will, l* l8 U" @5 b- ^ complement existing systems, provide flexible, modular configurations, and will 7 m N7 Z3 _4 |. Q% i: B) f3 W$ X6 _) Lbe launchable from land, air, or sea modes # L* ]2 I8 T! w' Z3 ~0 XENNK Endoatmospheric Non-Nuclear Kill. ! Q4 ?6 m* g; q" z% H, F4 |ENSCD Enemy Situation and Correlation Division (JFACC term).7 w4 Y) F$ v( K3 v7 R+ `. g. z$ Z Environmental 5 `3 U9 u( L: X: z+ P1 J- t. tAssessment (EA)( c, C- I3 v; @' X1 T A concise public document whose primary purpose is to provide sufficient6 F! A/ N7 d8 I1 T analysis of environmental effects of an action to determine whether to prepare% R; q d2 z _0 _( M an environmental impact statement or a finding of no significant impact. , s0 N4 j) k/ T* B2 Q/ HEnvironmental + n- z, r( ~6 o$ ` O. `Impact Statement2 \3 P! _2 J" X/ r& a) X: K _! { (EIS) 4 X) M) ]7 s3 u. K$ Q$ D) y5 x; ~A detailed written statement analyzing the environmental effects of a major . `: b. e2 }/ A- ]0 {, X* k; k; QFederal action. ! d, `, d+ ^% P* Q( \Environmental n6 b, ]! Y8 `& B, z( FSecurity* l4 F' T2 e$ g: N( M, t& W A specialized form of physical security that prevents technical penetration, e.g.,; N0 y0 C( e9 @% P k7 G penetration by waves of electron beams. - n/ P1 t& h; f$ XEnvironments The media, conditions, and/or physical objects in which a BMD asset is immersed % [; e, N! y# l' ?# s/ Hor surrounded. For BMD systems and elements, the comprehensive / \+ p# |# | j! d2 f' denvironments definition consists of natural, hostile, induced, and storage, : {0 w) R; g+ J; h9 O2 o2 ptransportation and handling categories. d# F1 q+ X4 ]% Q+ r! jEO (1) Electro-Optical.; q6 A! _- X, w! e: ~7 k (2) Engagement Operations.. Q0 [, C7 ~! U (3) End Office.6 u) r$ F( K; A# {' t, G (4) Eyes Only. " U3 T' J, _( C& m8 ~2 KEOA Early Operational Assessment.* z4 a% @8 |! S, H0 R5 O- X: B EOB (1) Enemy Order of Battle. 2 R2 {+ g, f9 G$ y7 g' d(2) Electronic Order of Battle. ! S3 D* p# S- T0 a# I6 z, ^EOC (1) See Element Operations Center. 6 \( U0 _1 `! U+ o3 u(2) Emergency Operations Center0 K' n# T9 q! H+ R8 b* q3 v& H MDA GLOSSARY, VER. 4.0 E $ t N- a- F5 I* P* v96) d4 `. ^$ C1 u& {* [- ?4 A EOCM Electro-Optic Countermeasure.: p9 |+ Z' W3 K EOCT Element Operations Center Test Bed. ' J6 t9 x3 d8 Q0 e: j+ d! zEOD Explosive Ordnance Detail; T1 [: P' b0 I; i( `; y+ Q EO/IR See Electro-Optics Infrared. - K4 c X$ p) |! s3 p8 F& m2 I: sEOM End of Message.: G6 i( }; \ V' D) Y1 _! `3 o3 b: X EOP Executive Office of the President # w8 V3 c% o) T3 e/ u+ DEORSAT ELINT Ocean Reconnaissance Satellite (US).( }) ]2 K3 w5 e6 ?. V EOS Earth Orbiting System (NASA term).6 t( i0 j6 H' _ EOSH Environmental Operational Safety and Health. 3 M& d. A/ Z+ B* wEP (1) Engagement Planning. (2) Evaluation Plan/ K. q; v1 e! V9 Z& w2 G# Z EP Cycle Engagement Planner Cycle (NMD BMC2 term). - r) n8 p. G4 {( g" g0 @! g WEPA Environmental Protection Agency. 6 y2 m0 T- E# V) E4 s' F% ZEPD Engineering Product and Development" w- {. ?% ^& |/ \6 u3 \8 j: M* _ Ephemeris/: k& A" E* l1 f! i, r Ephemerides 1 G& @+ G& H& v* r1 c(1) A table showing the positions of an object in space at regular intervals of x5 u. V2 z6 N+ E3 U! [ time. U- s" ~, p1 \+ d. e+ W- w6 I7 |(2) A publication giving the computed places of the celestial bodies for each ! E1 V1 y2 y0 \ j7 w$ L }day of the year or for other regular intervals.1 j# D. {; j- w6 s/ M EPITS Essential Program Information Technology and Systems.% S+ f% f+ V4 q/ Z D EPL Emitter Parameter Listing (USN term). 2 J; ~' |2 D2 ?4 Z* MEPLRS Enhanced Position Locator Reporting System. ( {: b) y- z1 O# d/ J+ @1 LEPO (1) OBSOLETE - ERINT Project Office (US Army term). (2) Element Program) _3 { o# h1 ? Office.! b$ e3 b2 h# V; y EPP Electric Power Plant (PATRIOT). f1 r* f/ l {1 V+ Q, C! g6 {EPROM Electrically Programmable Read-Only Memory. $ ^# F5 y {8 k) hEQEC EurQuantum Electronics Conference (See CLEO).5 V- o- J2 I$ i7 g Equipment9 |/ i7 S% H1 o2 b/ J+ M Operationally % e, w. p5 j: ^* j* E$ |: UReady * t$ \4 t. \+ i. K5 Y: t. \. hThe status of an item of equipment in the possession of an operating unit that # f4 E; \: a: ^$ s* s2 Pindicates it is capable of fulfilling its intended mission and in a system7 n' V7 H. m+ A5 a configuration that offers a high assurance of an effective, reliable, and safe9 W) F( p0 }" x, d performance. ' h/ ?* ~6 U0 b& W7 dER (1) Enhanced Radiation (“neutron bomb”). (2) Extended Range.( g% I8 c7 X3 p3 D; h$ { ERA Explosive Reactive Armor! o4 \( }' v3 T s, T# D. h ERADCOM OBSOLETE. Army Electronics Research and Development Command. (Now ' ^2 W$ [) e9 a9 I" D3 d% B0 nLaboratory Command (LABCOM), Adelphi, MD.) . a5 P, e$ F) Z1 O4 NMDA GLOSSARY, VER. 4.0 E2 i$ T: f* h0 E1 k1 Y 97 E2 L0 P) c8 n* GERCS Emergency Rocket Communications System (US). : x! [( Q" p, `* J/ ^7 h( C" eERD Element Requirements Document. 0 p7 z3 j2 c2 W* j, S& qERG Executive Review Group.; u& l! S; n# E2 V# \5 D* [$ N" ?- m6 e ERINT OBSOLETE. Extended Range Interceptor. Now referred to as PAC-3. + |$ P P, P$ s1 Y8 Y$ j! jERIS OBSOLETE. Exoatmospheric Reentry Vehicle Interceptor Subsystem., r; N" n$ s. Z% H% y; b' p (Predecessor to Ground-Based Interceptor (GBI).)( X) P: p2 L7 U$ F5 _ ERIS(F) OBSOLETE. ERIS Farm.# C2 h: u! F0 J$ d& \- d4 |; ` ERP Emitted Radiative Power. # A6 i! E U9 G% i9 {, B7 x- `ERR (1) Element Requirements Review. (2) Engineering Release Record. & c# J: A- i/ b gERS (1) Early Release of Submunitions. (2) Emergency Response System. % R* h: _+ s" t$ v' _0 O5 C) p1 sESA Electronically Scanned Array. ?2 ~8 ]5 p$ @5 k. f7 [ ESAD Electronic Safe and Arm Device. 3 s8 k0 `1 ^) V4 z4 f: i; c9 vESAR Extended Subsequent Application Review. % A$ J+ r% f9 }& `2 {ESC Electronic System Center (AFMC), Hanscom AFB, MA.2 ~. @6 |& f( b ESCN Existing Systems and Center Notebook., l/ A7 S- \& Y/ W6 X# N/ a ESD OBSOLETE. Electronic Systems Division. (Now Electronic Systems Center,0 K2 b9 s$ u& j Hanscom AFB, MA.)* |2 x& C# D- z! Y! L ESH Environmental, Safety and Health7 _* V& P. h4 ?' C! u7 f ESI External Systems Integration.( T7 s; p& B6 g' I ESI ICD External Systems Integration Interface Control Document. 8 B$ |. O6 M% i0 i2 bESM (1) Electronic Warfare Support Measures. (2) Electronic Support Measures. 4 w" X7 T1 S( ~4 {, x. }ESMC Eastern Space and Missile Center, Patrick AFB, FL.; P7 C. F. L( s" V# H% A ESNet Energy Sciences Network.) E. L: M9 a3 O- {3 [ ESPRIT European Strategic Program of Research in Information Technology. % ?4 I) K8 ~# o2 ZESQD Explosive Safety Quantity Distance.$ V. B& o, M" Z8 ^% w0 | ESSM Evolved (Enhanced) Sea Sparrow Missile. ! r$ H9 H& N0 q: T6 p/ gET&C Extended Tracking and Control.1 ~& F- c* @: w& ~$ q) u ETA Estimated Time of Arrival. 7 d$ l% l {& w8 K+ J9 b; QETC (1) Electro-Thermal Chemical. (2) Estimated Time-to-Completion. ?2 ]( v- {. O* PETD (1) Estimated Time of Departure. (2) Electronic Transfer Device.0 }8 y- l3 r7 s% p" @ MDA GLOSSARY, VER. 4.0 E 8 E8 h t- q7 A- R98, [2 d" u1 M# b; h j: s ETERTS End-to-End Real Time Simulator. ! p" Q; U& W2 n! METESD End-to-End Sensor Demonstration. 8 s7 K$ \* j" k) M0 u) ^ETI Estimated Time of Intercept. / b* X& n6 X6 t' }0 H- aETIC Estimated Time for Completion. . I6 @( F4 v1 d3 ?, G$ hETM Engineering Test Model % t% X5 t& G3 d9 y3 |ETR (1) Extended Test Range (Pacific Test Bed) (2) See Eastern Test Range. (3) * G2 M" K h6 B dEnvironmental Test Round. (4) Estimated Time to Repair. 3 k, b8 R* t) x3 y5 @- c" kETS (1) Experimental Test System. (2) Experimental Test Site. ! q& X. L$ J0 ^( V/ i7 R6 l4 iEU European Union [formerly European Community (ECI)] / U9 Q% |$ v% g' c1 f! c" y9 cEUCOM European Command. See USEUCOM.! A$ `) a7 @4 J, C$ X; v EURATOM European Atomic Energy Agency.$ e" l$ y/ F b C! ?' _" D EUREKA European Research and Coordinating Agency. Y$ {" h7 X0 y. y! ?EUT Early User Test.& E" [2 i, e- M5 m3 ^& ?' I EV Experimental Version- e7 b% t) T" g# Z. N( R) f( v EVA Extravehicular Activity.. T1 Q+ R' b1 p1 G3 C4 Z Evasive MRV A reentry vehicle, which maneuvers for the purpose of evading defensive 2 a) p( K; Q" }. H! c' a% e- D$ Iweapons.: t4 h" c' C/ [ Event Based ! Z; q2 k7 C2 m9 CContracting . L4 G( D! @3 ]+ p/ d8 J( eSupport “event driven acquisition strategy” by linking specific contractual events3 n( u4 `3 ~1 S$ w4 J to the “exit criteria” for the acquisition phase, or to intermediate development A e) v* V+ i' K events established for the acquisition strategy.7 B' {! l7 I! P1 y. i. B& _ Event Driven" d1 a0 a) j: m+ X Acquisition * [4 \% m2 R% K7 H1 M# MStrategy * o" P& }2 G* v9 v; SAn acquisition strategy that links program decisions to demonstrated $ G4 I% v$ I# u3 ]2 K& Oaccomplishments in development, testing, and production.* z7 i0 S O6 [5 ^, G$ [# U* i Event Validation A sensor element internal process that results in a determination by the operator) M8 o% L3 X: ?6 s" N6 \ that the sensor is healthy and the event reported is real.

使用道具 举报

Rank: 9Rank: 9Rank: 9

43#
发表于 2008-12-25 20:06:02 |只看该作者
Event " y' l6 @0 H; P5 M" @7 YVerification 0 K! F. ~# o; [8 A8 DThe process by which it is decided, from SDS external data, that the event 3 D, X3 n. t* I/ Wreported is real.0 f7 X1 `5 I, P MDA GLOSSARY, VER. 4.0 E" g+ G: @* c3 ]# |1 ~2 Y2 B 99 $ G5 [* R' E3 X% i6 i/ ?Evolutionary3 L2 Q% }4 X/ I3 V* m Acquisition 0 v$ W# Q, \/ O& i% H1 V. r2 _. {# a(1) An approach in which a core capability is fielded, and the system design has & Y% B. k. h! ?a modular structure and provisions for future upgrades and changes as: {: A* P4 \5 C# V# {0 C requirements are refined. An evolutionary acquisition strategy is well suited to 4 n" v! [# T1 n5 W& S5 ^8 uhigh technology and software intensive programs where requirements beyond a 8 S# ^% G3 p: w" u# o) |core capability can be generally, but not specifically, be defined.* o0 C+ x+ }; {) k$ P# S9 g% [ (2) An acquisition strategy that defines, develops, produces or acquires, and ' M4 P- i, X$ X9 t: R2 Nfields an initial hardware or software increment (or block) of operational capability. , Q/ C* @0 V1 x' \. Q5 tIt is based on technologies demonstrated in relevant environments, time-phased w6 B- Z7 q' g( D4 G# z requirements, and demonstrated manufacturing or software deployment . _. C8 a& J# D$ jcapabilities. These capabilities can be provided in a shorter period of time,1 \" M0 u/ ]4 ^1 d followed by subsequent increments of capability over time that accommodate " l. X" N- z7 i0 j A7 iimproved technology and allowing for full and adaptable systems over time. Each' T& m8 K; x+ q3 c, e: L* G$ G3 p increment will meet a militarily useful capability specified by the user (i.e., at least: ^; G3 [8 P' u! V the thresholds set by the user for that increment); however, the first increment; V4 r4 Y; A7 l" ^5 { ~# T: p, c may represent only 60% to 80% of the desired final capability. (MDA Lexicon)0 Y) J" b9 x& L0 v% ~9 W) ~6 |. I Evolutionary : C( F, o+ f9 m3 C2 X# U8 wRequirements * G3 |/ `2 S. e# e1 X+ ADefinition$ ?" W5 d) `' O/ k6 |4 \! C3 R Mission needs are first expressed in broad operational capability terms, and then . A) v# h8 u+ ^5 C ^) Iprogressively evolved to system specific performance requirements. 8 X7 v$ ]: e4 G7 n# E% I* nEVPA Experimental Version Performance Assessment.6 v3 J/ C3 I: `' u9 W4 x5 [1 X' n EVPA/TEVS Experimental Version Performance Assessment Test Environment System.! I; U* f4 D& q EVS Enhanced Verdin System. 7 h( Q2 y8 L eEW (1) Electronic Warfare. (2) Early Warning. ; Q- Z& S% V. \- }3 eEW/AA Early Warning and Attack Assessment. - A! [+ T5 g$ A8 |1 s) H( fEWCC Expanded Weapons Control Computer (PATRIOT).; l3 J- Z& V% R3 d9 N! U+ n- P. ` EWDA Energy and Water Development Appropriations (US). % h# Z) \: s0 g* rEWG Event Working Group. & D, p+ ~. m+ N. \; R, ?* xEWN Early Warning Net.; A2 o0 h1 i! S* Z: ?* A& Y5 h EWO Electronic Warfare Officer. : E, W) R: O8 BEWPE Electronic Warfare Pre-Processing Element. 2 L( F5 J3 H! D' K! a! LEWR Early Warning Radar. p; \. H9 |6 X6 \% e EWS Early Warning System. * B6 n0 _8 U1 V9 b# i' iEXCEDE Electron Accelerator Experiment. 7 U8 E' g( [; d: J; G8 d" oExcimer A contraction for “excited dimer”; a type of lasant. A dimer is a molecule 2 E) ~2 j: S& b1 e/ bconsisting of two atoms. Some dimers (e.g., xenon chloride and krypton fluoride)/ K a- Q, H- Q L5 g are molecules, which cannot exist under ordinary conditions of approximate( [0 |+ q+ {/ g: B/ ?9 d) g) u thermal equilibrium but must be created in an “excited” (e.g., energized) condition 2 p1 @6 T$ z3 E- m$ Xby special “pumping” processes in a laser.( J) Z- h2 W3 R$ @ Excimer Laser , E; z/ A- m9 G# v. l) K% R7 r1 _+ B* ^(EXL), q" I% Z# m( B4 K A laser in which emission is stimulated when a gas is shocked with electrical* e. D" @6 `7 ?3 T/ X energy and the excited medium emits light when returning to a ground state. - F# i" j3 O8 ?1 u1 @- u. ]5 {3 E7 ]MDA GLOSSARY, VER. 4.0 E* X: C0 a: ?3 \ 100- g: a- \; V" u0 h! @: G! E EXCOM Executive Committee. , q: X) I( C; N/ cExecutable \# t! ?) ^2 q8 I6 B' P, B$ y, }Program % e, u4 s9 ^% w: zA program is executable if the PM has adequate near-term approved funding.3 D0 X# T* G- a' M# C# j Y Executing Agent The individual within the executing element assigned responsibility for managing ; w: Z, N- E' c/ Z, _5 j0 `5 WMDA funded programs.7 s- U7 w1 x; c/ c+ _ Executing + I* o% o9 a! D: |Elements) p" J v" ?" L% X; [' S; C Agencies or organizations (DoD or non-DoD) that are managing BMD-related , g/ P2 a4 O4 ^5 a, Wprograms.( a2 o: K' v- l/ A- @2 t% z9 v Executing+ z) _& P7 x2 f$ U2 { Responsibility : t0 c. S) G$ _) z. t& rProgram Manager responsibility. 6 J8 t9 g. r) @! U# T5 ~7 TExercise A military maneuver or simulated wartime operation involving planning,! j1 w0 @, u* d/ D preparation, and execution. It is carried out for the purpose of training and5 y. K! m& w- v) `8 H. g6 l evaluation. It may be a combined, joint, or single-Service exercise, depending $ X# k% P0 B$ q" j; X3 W3 p* d; don participating organizations. See also Command Post Exercise. 2 |, @9 J% s% P0 ]& n; @# lExit Criteria Program specific accomplishments that must be satisfactorily demonstrated 3 K( r7 y& z! d. \# ?- R! hbefore an effort or program can progress further in the current acquisition phase' b. b3 H% u d; K or transition to the next acquisition phase. Exit criteria may include such factors; D; W' A8 S. W( a+ K$ j) h as critical test issues, the attainment of projected growth curves and baseline. ]' Q/ t8 U5 f* P& f parameters, and the results of risk reduction efforts deemed critical to the1 M3 }4 ?) j2 q decision to proceed further. Exit criteria supplement minimum required$ e7 ~7 H. L+ `4 J, b accomplishments and are specific to each acquisition phase.2 C* c" x7 F" h9 J9 | EXL Excimer Laser., z6 L" m" b% \. x5 [0 l6 r5 k" ]" C Exoatmospheric Outside the Earth’s atmosphere; generally considered to be altitudes above 100 , o/ l+ s5 O Y* w! ykm. " b+ _8 b; S. {, s' n: ]1 hExoatmospheric4 P9 Y$ N5 @: D# ~3 ^( Y! a Reentry Vehicle " z4 d4 m: ^& Y% ^: e! zInterceptor% e. f% _+ o/ `2 p; j0 ]6 y* ~ Subsystem - Z+ X7 O# I6 E2 Q4 ~5 }: k6 H1 `7 U(ERIS) $ o8 J6 |: p: T9 rOBSOLETE. Interceptor designed to provide functional test validation of GBI. M$ t/ p% }5 l( Z& ]+ N* p' c* B Exoatmospheric * _/ o/ ?8 Z+ ^$ ^0 R% ~5 o$ y( {- xTest Bed (XTB)+ G) J, K s2 m! R6 L4 g: ]/ k Flight qualified and range integrated vehicle to support other programs such as 3 J) k8 I3 v# w3 uGBI-X.9 L, c" r5 C5 @2 {* W Exo Decoy A decoy that matches RV signature exoatmospherically. Exo decoys can use 2 Y7 X5 z0 F) Y9 o2 B- a7 nradar and/or optical means to deceive sensors. , |* z, m; v4 f8 ^Expert Systems Software programs, which use artificial intelligence techniques to capture and , @% ^$ W$ i( R6 B' M* iapply the non-algorithmic knowledge and procedures of human experts.- A4 r8 Z# s' R) m5 {! F0 w Expired- J# M% k6 v. v6 N) y& T Appropriation . N+ W7 w& {3 w9 cAn appropriation that is no longer available for new obligation but is still available 8 v3 `9 B' d8 P. O1 ?for disbursement to liquidate existing obligations. Under current legislation no ' V& _" s% j, V7 A- V, Y+ adisbursement may be recorded or paid after a five-year expiration period. * ^, M7 ^* d+ a8 o; ]5 yMaintains all original accounting identity, e.g. FY, appropriation, PE, etc. - q( {+ R! B' M* HEXPLAN Exercise Plan. 7 I1 R, p! Z M9 d, uExplicit- X2 k' y# l7 L! y0 Z Coordination* x* p y/ K+ s9 l# n$ l! ~ A battle management technique which communicates results, decisions or9 i# ^) s' a/ S, i& H; q( ~, J command from one battle manager to another, usually from a higher command 1 B O6 o, O) hto a lower command.9 j# R& t) o" k: k, E9 g MDA GLOSSARY, VER. 4.0 E0 R8 D* ?- ?" `$ Y8 P; A5 v 101 5 |% N" q( J' [5 E# KExtended - `: x4 j8 f/ JPlanning Annex $ |1 D7 Q% u7 f: H) {5 y$ vA document providing program guidance for an additional 10 years beyond the ; s6 M, v: j( W2 HPOM. $ \& P: v9 R( ^8 O9 @6 ]. oMDA GLOSSARY, VER. 4.0 F P! M' _8 e0 I" X! g: x) g103 2 @$ p" z { o2 E- {( }F (1) Fluoride. (2) Fahrenheit.1 s" Y2 Q4 v, m F/O (1) Fiber Optic. (2) Follow-On. 9 g; p( J* C EFA (1) Field Artillery. (2) Feasibility Assessment. ! t p& Y, r& p9 aFA/RD Functional Analysis/Requirements Definition.& M O. d( x) W: b! e) b) P FAA Federal Aviation Administration. " E4 X/ v X2 }/ h4 OFAAD Forward Area Air Defense (US Army).& _% ^/ g# b; y. |2 U FAAD C2I Forward Area Air Defense Command, Control and Intelligence. 3 W- J" g) g5 m4 ]6 JFAADS Forward Area Air Defense System (JCS term). + S0 c* r1 d* y2 k. `) K& {FAAWC Fleet/Force Anti-Air Warfare Commander. ) s2 q3 o5 r4 q9 x+ d ~FAB Fly Along Probe. ! k# c+ K! K8 q6 p! I! W J3 b8 kFac Facility (MILCON term).: E" I ~; d% C' }( q, |% e FACP Forward Area Control Post (JFACC term).% ~6 ]3 T5 c! b8 y7 \# H1 E FACSPMF Federal Agency Computer Security Program Manager’s Forum./ O( O" W& S6 ?- k( L' H# W FAD (1) Force Activity Designator. (2) Feasible Test Date. 7 g2 V1 i- k/ a& B. ^, }; aFADEC Full-Authority Electronic Controls.1 L0 i D$ T0 Z/ ~) q FAFB Falcon AFB, CO.% u8 f, _5 f) O" I E! P FAFBR Falcon AFB Regulation / B# ?' h" {3 Y% f* ?Fairing Structure to protect the payload during ascent phase.0 F# g4 P+ E% U: u% L/ p0 Q FAIT Fabrication Assembly, Inspection/Integration, and Test.! X# `, J) b3 r6 ~6 I FALCON Fission-Activated Light Concept. q4 o# X7 @' X& G( m FAM Functional Area Management.( P! H! M, P. w9 V FAMIS Financial Accounting Management Information System. 2 E- e8 w: a: ]2 c& y1 ^0 `FAMP Facilities Acquisition Management Plan./ I, g( u: b- _ ~% h FAMSIM Family of Simulations (USA term). 6 }$ j6 |! r" A- DFAR See Federal Acquisition Regulation.! e7 l; a8 ]' M$ m; [: M Far Field The region far from an antenna compared to the dimensions of the antenna and2 G& ]0 u: F5 N8 ]. g& f. W6 Q Y the wavelength of the radiation.2 ]# s% ? {) | FAS (1) Fly Away Sensor (TCMP).% P3 @" B: m5 j3 M (2) Federation of American Scientists.: ^& j' s1 w! |4 h* G1 U FAST Facility Allocation Study Team.5 o# s- a H N+ ~/ D MDA GLOSSARY, VER. 4.0 F8 l4 G/ x' _( t 104/ _* v" F) ^- Z Fast-Burn+ _& x+ F0 v3 S9 u% C Booster (FBB)5 [. M: X+ o5 x3 K1 F9 R' _ A ballistic missile that burns out much more quickly than current versions, 2 Z+ O4 |5 ^9 f0 F8 Z- zpossibly before exiting the atmosphere entirely. Such rapid burnout complicates 4 U) {7 r& o1 r1 E3 s5 sa boost-phase defense. # S8 n L6 u1 i& L0 k& A% K/ ]+ x7 RFAT (1) First Article Testing. (2) Factory Acceptance Test. / e7 b, }( u& ~8 JFault Tolerance The ability of a processor to maintain mission effectiveness after some# N- h8 q# `) U+ z& | subsystems failed.8 g, y" G" u$ _( p+ V3 z& q) y4 ?+ q+ z Fax Facsimile. : V9 O! l8 g9 C4 I: |" @3 D XFBB Fast-Burn Booster., Y) p, u6 x+ {. f FBIS Foreign Broadcast Information Service (US). / k; H$ d% |! h1 HFBM Fleet Ballistic Missile. # Z$ H8 p. ]& z% `9 O. q, G- xFBMS Fleet Ballistic Missile System (USN term).( E3 {4 m& c' ^8 f. ]% w FBP Forward Based Probe., @+ }" v; M; g t0 Y FBR Forward-Based Radar (US Army term).# O# J% \- Q1 n0 E d FBS Forward-Based System.1 p2 w: c3 u3 C; E6 Q" L FBXR Forward-Based X-band Radar. J9 y' U& {+ EFC (1) Fire Control [of weapons]. 6 Q8 m4 U) e8 U6 _4 D2 y(2) Fund Code.& n. V9 g; ?& i8 e: h. y( u& j* f FCA Functional Configuration Audit.: S8 E5 D5 c$ Z; [" g( { FCC Federal Communications Commission. ' N" Q% K4 b* f; A2 E; L$ fFCCM Facilities Capital Cost of Money.& D5 k( |8 y) I7 ~) @( q7 d FCN Fully Connected Network. # s7 I( ^6 R0 A. b( r' KFCO Field Change Order. 7 ?0 h6 H K1 x h# w' |FCRC OBSOLETE. Federal Contract Research Center. * v4 B+ k% M1 W G% H. | X) ?FCS Fire Control Section.

使用道具 举报

Rank: 9Rank: 9Rank: 9

44#
发表于 2008-12-25 20:06:20 |只看该作者
FCT Foreign comparative testing.. b ^/ b7 b4 U4 F5 c7 W) o FD First Deployment. @& d4 ^* d. Z7 X, c% J7 k FDA Food and Drug Administration.1 N2 t( P4 w0 }. p9 c0 R* X* ] FDC Fire [of weapons] Direction Center. : `* v% z) t) @- _0 K- F7 bFDG Foreign Disclosure Guide.5 ^9 F" D8 c- Q) h FDM Function Description Manual. * X& g/ Q* b* L0 P9 A2 OFDO Fee Determining Official. * o5 z( I! y6 j7 Y7 iMDA GLOSSARY, VER. 4.0 F. C5 m9 N. y8 K8 q# ~, v1 T& B1 K. \ 105* k( ~3 D9 H L0 H FDP Flight Demonstration Program. % _2 S" `% ]' M4 H' kFDR Final/Formal Design Review.9 t' W! d! j5 { _% ^, J6 K. i FDRU Final Design Review Update (MDA PAC term).* T' v. g) [1 f2 v3 F3 X FDS (1) Flight Demonstration System. (2) Fault Detection System. * x! h) f7 } K. |- n! G9 oFDSV Flight Demonstration Space Vehicle. , i% f, s% y; {& k: a2 VFDT&E See Force Development Test and Experimentation (US Army).) q# T) G# @4 ?# D FDX Full Duplex (Telecomm/Computer term). ( g5 c% E( m* d6 k! qFEA Functional Economic Analysis. ! p7 h0 I' O' K3 \) g; TFeasibility Study A study of the applicability or desirability of any management or procedural 3 ?) l J" C* j* x5 C# xsystem from the standpoint of advantages versus disadvantages in any given * A7 d% V$ P8 I- T1 Dcase. * U( u& M0 x+ @. Z6 TFEBA Forward Edge of the Battle Area. 5 X3 c" m' M- W7 R" D! |/ g5 e6 oFECA Front-End Cost Analysis' \ W) u5 V. S2 k% `0 f) ~8 R8 S6 v FED Federal.7 _ o0 f% v- G0 j3 g* `3 t FEDAC Federal Computer Acquisition Center.: d2 h, r* g, N( s Federal' Z* P: R' `- A) |9 v Acquisition 2 W3 @( B% v( |2 T$ ZRegulation : f! Q) O M. b! d( S! y$ K) FThe primary regulation for use by federal executive agencies for acquisition of0 c2 ^# n! T1 G) j' d4 D, D supplies and services with appropriated funds. It directs the defense program. [' B) v: N! i9 Q manager in many ways, including contract award procedures, acquisition 1 r) S: f7 d: a9 |" Yplanning, warranties, and establishing guidelines for competition. The Military ' ^$ o9 C$ u5 x& d, ]! m! zDepartments and DoD issue supplements to the FAR. The DoD supplement is8 s# Q/ n8 g: l4 h% |* U called DFARS (Defense FAR Supplement). ( c0 m5 F o% ^0 X ~9 @FEDSIM Federal System Integration and Management.9 k+ ~" T8 [' z- C) x FEL Free Electron Laser. 3 _# V1 U( R9 u5 _& WFEMA Federal Emergency Management Agency.1 |3 k1 p; ^' h/ y7 [ Fenced Funding An identified aggregation of resources reviewed, approved, and managed as a# W8 e# m: V' l( j7 v distinct entity. The proposed program must be implemented within specified 1 Y& S. [- a. L. t* wresources. Examples of fences areas are: Intelligence and Security, Support to 1 w- T( r5 k, m! j5 ROther Nations. 2 u6 r) F2 M4 ]' K2 ^8 i; k1 iFER Financial Execution Review. 2 T* o/ a7 d) o7 @* pFES Facility Engineering Surveillance Plan. " G/ Q" W1 y$ Y( JFET Field Effect Transistor.2 l: U+ ^0 I; h. J5 d0 g { FEU Flight Evaluation Unit.; m, E7 W( |2 { FEWS Follow-on Early Warning System. # L3 Z4 _% X( ?8 x" u2 KFF Fire Finder Radar (US Army.4 O# {) Q' g' J) ]& v8 Q' t* P MDA GLOSSARY, VER. 4.0 F: B8 P8 [' d% B 1063 G# t5 H( ^! i( W/ S9 P FFBD Functional Flow Block Diagram.3 e0 D# v. I7 H FFCD Full, Final and Complete Disclosure (Treaty negotiation term).1 {' A% B6 P* L1 O: \ FFD Fraction Failure Detected. - W% n, t( p F* [FFH Fast Frequency Hopping.: S/ S7 p/ f/ D; `+ D FFP Firm Fixed Price. ' ]5 Q) \1 {3 l9 D _# J3 DFFRDC Federally Funded Research and Development Center. 4 D& ]7 y6 M9 M2 XFGC Functional Group Code (Navy ILS term).# y6 Q6 d, X [$ ?- \4 G: W2 e FGEP Fixed Ground Entry Point. + S# p; M/ K& ~) i9 ]FH Flight Hours.8 g3 \( O V# \, P FI Fault Isolation. % V2 J* b+ l- l& f$ ?6 lFI&A Fault Isolation and Analysis. 2 j1 y& }5 u1 [+ [9 QFIDO Fighter Duty Officer (JFACC term). 4 h- {# [' ]5 IField of View . _ U: j1 Y5 e- ?1 }9 N$ o(FOV) Q4 i. f- [$ M) dThe angular measure of the volume of space within which the system can5 ]9 m6 @: [# s! V- u$ V$ W' F respond to the presence of a target. 9 D4 }8 F3 _5 J1 q& @" w* fFighting Mirror ! C# C0 T2 H- J7 i/ ^(FMIR) T0 f7 x7 b% _# v' m( p1 ?1 ]Part of the GBL System. The low orbit mirror, which receives laser energy and . }4 g( a. J9 _5 x, _ p! freflects it to the target. / U% n+ `! L; [1 ~' s5 oFigure of Merit 4 z1 z r+ @4 i* Y" R. e- h( P(FOM) * x$ A* _: Z$ S" @7 \The numerical value assigned to a measure of effectiveness, parameters, or% E& W* f+ ?2 J/ t other figure, as a result of an analysis, synthesis, or estimating technique. ]) J; r4 A" `) U6 {1 Q$ g FIP Federal Information Processing. : O$ f8 h7 c' J& q* gFIPS Federal Information Processing Standard. 6 I" P4 z6 `8 e5 n C5 b7 jFire Control The control of all operations in connection with the application of fire on a target.8 P5 v" o% F; E9 e1 } Fire Control - P* \0 D" m9 K% r! @: W& qSystem. n- L h$ i( c+ ?1 A8 t$ x A group of interrelated fire control equipment and/or instruments designed for 2 }! `! q/ p* Q) }' xuse with a weapon or group of weapons.7 Y+ }) ?$ b Z t- F. G+ h- J Fire Support' F9 _9 M. S+ t1 d+ h. Y Coordinating! s- b1 V: ?4 h. x' B% [ Measure $ m7 y8 [- i, LA measure employed by land or amphibious commanders to facilitate the rapid $ G2 A; k. T8 M" \engagement of targets and simultaneously safeguard friendly forces. @& s/ ~+ N+ C& w% p6 ?# g; J Fire Support% d( o8 m1 S' \" ], g* S% H7 J Coordinating Line " D, k( y. u9 p w(FSCL) + j5 ~& B0 {0 | {9 `A line established by the appropriate ground commander to ensure the7 d+ G4 v7 R' {. w) g% L1 z coordination of fire not under the commander’s control but may affect current' l; E* v2 @3 R! N1 I tactical operations. The fire support coordination line is used to coordinate fires4 U5 ~" Q8 O& `7 u of air, ground, or sea weapons systems using any type of ammunition against- f. ?; ?6 x" J9 o4 W8 N2 e6 ? surface targets. The fire support coordination line should follow well-defined' m% U0 l+ n( e7 G terrain features. The establishment of the FSCL must be coordinated with the $ D- d# b+ I/ K/ @2 m9 t+ @appropriate tactical air commander and other supporting elements of the FSCL 6 N3 m4 k$ \7 L" H* B& i4 u" A6 zwithout prior coordination with the ground force commander provided the attack/ C+ a3 t A( G will not product adverse effects on or to the rear of the line. Attacks against8 X+ Q% U) D8 Y+ Z1 E! E- m' N p surface targets behind this line must be coordinated with the appropriate ground3 F" b. ?+ b5 ]: x9 V force commander.3 l/ x* H( t+ T, O MDA GLOSSARY, VER. 4.0 F ) H, Z7 z8 J4 ~2 L% O; D k2 `% y% P1071 L' R T |$ c9 \5 w& ? Firing Doctrine The ratio and manner of assigning numbers of interceptors against given0 E* v2 K; q9 P* R6 } attackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are0 R& ?5 e' A+ N. g examples of different firing doctrine. The priority of targets being defended and+ J0 c; L0 s* ~4 A the number of interceptors available relative to the number of attackers drive 0 N, G- a! k; ?) I( \' _doctrine. - o2 {0 P2 U* AFiring Rate The number of missiles fired per site per minute. ' G1 i U5 k9 Q+ dFIRMR Federal Information Resources Management Regulation. ( j, \1 @: d1 C) }7 b( A; pFIRST Forum of Incident Response and Security Teams. ; z$ k+ n% M! KFirst Article First article includes pre-production models, initial production samples, test - l% C" ]3 T+ j2 B4 N9 j9 H! r# @% asamples, first lots, pilot models, and pilot lots. Approval involves testing and 8 q8 X6 ~" l* E- W2 z$ pevaluating the first article for conformance with specified contract requirements ; p8 ^' N- p- Ubefore or in the initial stage of production under a contract.* D, S* H$ d7 m4 I* n First Strike The first offensive action of a war (generally associated with nuclear operations).0 T1 d1 t- X; P First Unit & p2 R. | e' oEquipped Date 6 R! Y/ V/ u+ CThe scheduled date an end item and its support elements are issued to the 7 a; d# P3 r8 q! L, winitial operational capability unit and training in the new equipment training plan- F% k) V7 v6 [% Y0 \' m9 d/ x has been accomplished.* r+ l7 X: _2 E) C; C8 \! T) H FIS Facility Installation Standard. ' m0 f; w8 `$ u. i/ l* ^6 vFiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which- r9 N5 e \$ h" Q+ a% O provides the fiscal constraints that must be observed by the DoD Components in " O& ?7 y4 a5 I. w5 ?the formulation of force structures and the FYDP, and by the OSD in reviewing4 }3 G0 t- b. c5 @ proposed programs. 2 q; ^! b" {3 Y3 {3 MFISSP Federal Information System Support Program. ( e( `6 L0 u! N( u; \7 o; yFIWC Fleet Information Warfare Center (USN term).( p% T K/ L& r/ U9 v FIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern # o' L7 R- G3 ^* ?Extension). 6 y- J% K' U9 wFixed Costs Costs that do not vary with the volume of business, such as property taxes, ( s3 C% H: Y) y, Binsurance, depreciation, security, and minimum water and utility fees.6 e7 n7 D$ F0 Q$ T Fixed Ground6 b" l6 @4 T* G: A9 m3 n' G. N Entry Point & I, Y% r7 h& K9 H(FGEP) * o" s( C) ?& D% l% U2 s: CThe subset of GEPs, which are not transportable. GEPs provide the) j; i+ g( a2 |2 M: f; i0 ^ communications interfaces between the SDS space orbital/sub-orbital elements " z8 S' x5 n" ~8 p" d# {and the C2E. ) c8 f: J) n; Y8 W, X* L# }Fixed Ground# C! s" j F* y7 s Station1 ~. ^, U8 l( H+ ]" L All hardware, software, and facilities located at a fixed ground site necessary to % F" Y' }+ |3 V' J# yreceive, process, support, and analyze mission status and data, and disseminate0 D0 ]3 I/ a, ?8 p; k W, |2 P operational messages.6 C4 {) p6 A& e% |; H8 H- B FLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor: M4 N: \8 ?+ A' q4 o; | program to Extended Range Interceptor (ERINT).). T0 O5 t& ~, G8 m- W FLC Federal Laboratory Consortium.1 D" t6 ~. ?9 ` Z3 f MDA GLOSSARY, VER. 4.0 F % M \( n9 C& r4 [$ } r' S108 / j' | \, b" |/ ^! VFleet Satellite4 `0 f6 E+ {2 H/ j Communications' S0 q% O; H0 \) v Q System # l2 |% i7 z# t2 x(FLTSATCOM) " i8 ] E7 I, ~ I% e* sOperating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost & d7 I; @$ T' }, {terminals with simple antennas for use on highly mobile platforms. It has a& z7 ~4 B9 ]; F relatively small capacity because of its much lower operating frequency. It K$ C C) x$ p5 f+ U1 H' sprovides a satellite communication system for high-priority communication% H& v9 }; z6 C0 y requirements for the Navy and Air Force that encompasses almost the entire/ o( }( n" t5 v6 ~# v. q world. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF) {2 x! s3 d7 |4 s8 J and SHF bands. The Navy has exclusive use of 10 channels for communication / e; J4 p& V y5 ^4 H6 {; M2 b9 `, qwith its land, sea, and air forces. The Air Force uses 12 others as part of its / [! d5 B$ R& D1 NAFSATCOM system for command and control of nuclear capable forces. The$ [' K+ M! l% t7 ? system has one 500 KHz channel allotted to the national command authorities. 5 o$ _4 D1 Q; q* u0 CFlexible 3 q% e: K) g( t! A/ c6 nResponse, D6 b6 w. S% b) u( ?* ` The capability of military forces for effective reaction to any enemy threat or8 H& w9 K3 J0 o# N4 p- h attack with actions appropriate and adaptable to the circumstances existing.; ?2 ~0 i: Z) h+ u$ X) e% @0 X* w FLHER Funds and Labor Hours Expenditure Report. # I6 O( Z! t/ ^ @Flight + v5 \% y7 l4 ^$ F zDemonstration 2 d/ B& n, P# g- fSystem (FDS)2 K6 f4 e8 R1 o/ A H9 Z& p Part of the SBIRS Low Program Definition and Risk Reduction (PDRR) program 8 @) f" [, S: L7 g7 A5 s X0 ~phase. The FDS will consist of two satellites and a ground system being built by 3 p) p9 W$ \5 ]( B& z+ PTRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test - i% \* G8 E' N6 jprogram to demonstrate operations and performance of a SBIRS Low concept, 1 f3 C* ^7 z6 q4 P, ycollect target and phenomenology data to support the objective system design, " _5 b$ [8 y1 |# A+ Qand validate cost estimating models. 2 V* P$ h \2 h- _+ T8 f: T! jFlight Path The line connecting the successive positions occupied, or to be occupied, by an 6 w; a/ Z9 A& S2 Gaircraft, missile, or space vehicle as it moves through air or space. (It is more6 o% z( u$ Y& K" P9 h) H0 B6 K2 j$ B. ]' B1 r commonly referred to as trajectory for space vehicles, especially ICBMs.)- J6 m2 }2 z& D9 k Flight Readiness 7 `" }- N) j! u, HFiring - A( F6 l( N0 Z% I, p* @A missile system test of short duration conducted with the propulsion system% s5 m8 H( N& x2 F) l- X+ P operating while the missile is secured to the launcher. Such a test is performed( C. ^' T0 Q( V: f3 x0 K to determine the readiness of the missile system and launch facilities prior to7 r7 t( b* J5 o4 R2 @ flight test. * o& z5 m1 y/ c mFlight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching. ( y9 x' G' e, R# k) Q: }' }1 ^Flight tests are planned to achieve specific test objectives and gain operational 5 ]4 B' {% j* M- u' {+ Finformation. " u; O1 [! c1 N0 Q$ c$ ?9 FFlight Test& l7 W b0 M. Y- x Vehicle (FTV) / L2 U& L4 I' PPrototype of airborne or spaceborne hardware used to validate a technology& T4 `( K* \, u concept.

使用道具 举报

Rank: 9Rank: 9Rank: 9

45#
发表于 2008-12-25 20:06:36 |只看该作者
FLIR Forward Looking Infrared Radar.8 X( J0 u. X8 P; @; H( k1 b FLOT Forward Line of Own Troops. , t! @+ |: `( ^0 K& BFLT Flight.0 O2 Y5 ^- }4 Z7 m8 L FLTSATCOM Fleet Satellite Communications System.7 E1 \, [2 }! I# e/ Q8 T; R Fluence (or/ _7 @8 Z: u7 V. G/ o' ` Integrated Flux)/ Y( v/ p0 R3 D2 u5 t The product (or integral) of particle (neutron or photon) flux and time, expressed' u! w' H& L8 S, p; o2 V" e8 z in units of particles per square centimeter. The absorbed dose of radiation (in0 }6 B9 g& H3 x) i0 |+ B rads) is related to the fluence. (It should be specified whether this is incident or- Y" O" W7 u$ m3 W absorbed fluence). ! g! H+ Y4 k7 a) k0 B* _# pMDA GLOSSARY, VER. 4.0 F) Q- |( p9 D. t7 M/ S 109 % L O* f/ g" d yFlyaway Cost The total cost related to the production of a usable end item of military hardware.2 u) \+ u7 L5 B7 F* F Flyaway cost includes the cost of procuring the basic unit (airframe, hull, chassis,+ @, S+ ~7 u# m; S( R- E, u% s etc.), a percentage of basic unit cost for changes allowance, propulsion 0 C9 S; |) e) w6 A8 b+ {* hequipment, electronics, armament, and other installed government-furnished1 `1 E" @3 h4 R7 m& D equipment, and nonrecurring production costs. Flyaway cost equates to . S0 v* }$ y9 E, z, C; TRollaway and Sailaway cost.4 z4 P4 J' K/ n! ^4 O9 r: k: \ FM (1) Flare Multiunit. , \+ f) h# I2 g7 b. j4 {' t(2) Frequency Modulation. ! a+ M4 m& Y! g(3) Functional Manger. % m1 a! K! _% g3 d% s) P(4) Force Module(s). f* T3 K% x% ` (5) Field Manual. 9 g; r) v/ u+ a7 xFMA Foreign Military Acquisition.: z/ e2 P. j1 f, M FMB Financial Management Board. % d. k" x9 M) X8 ~; n; s5 tFMC Flexible Manufacturing Cell." W' R( N' W2 z9 Q8 q FMEA Failure Modes Effects Analysis (ILS term).; }9 K5 s' k; g. P; B1 v3 q6 U FMECA Failure Modes Effects and Criticality Analysis (ILS term).% X% S# S" h4 Z. p FMIR Fighting Mirror. 9 z2 y' v' a. y0 TFMP Foreign Materiel Program.3 B$ }: F6 m- z {' C. d7 k FMS (1) Flight Mission Simulator (PATRIOT), Huntsville AL.# y$ b8 M# P+ {# w/ f (2) Foreign Military Sales. ~' C4 t7 x7 o: y+ u6 k6 K: h FMTV Family of Medium Tactical Vehicles (USA term). : d) H& k6 }9 _% L# a3 rFNC Federal Network Council 9 s5 h- X( a( Z8 x" M H, l# P% a5 fFO Force Operations (PATRIOT). ' d" t, Y6 D6 b l, rFO Link Fiber Optic Link. % ]) A; n9 B) _9 SFOA Future Offensive Aircraft (UK RAF term). 8 P) c4 `# i$ ~2 L! iFOB Forward Operations Base.' f7 G, l P) l& F0 ` FOBS Fractional-Orbital Bombardment System. , h$ R. m) n( _FOC Full Operational Capability.2 Q: {' @! e9 k Focal Plane The plane, perpendicular to the optical axis of the lens, in which images of points 2 M/ J1 @0 J" S( n- o! oin the object field of the lens are focused. 1 k3 ^' v* \9 C3 SFocal Plane& m# n5 X5 {/ x; j# H$ n g Array (FPA), C1 B8 o* @7 [$ ] An FPA is a matrix of photon sensitive detectors which, when combined with low; X, H/ ], g9 H; ~& U noise preamplifiers, provides image data for the signal frequencies of interest.9 G4 e7 a' }5 m- T+ V# P/ b FOFA Follow-On Force Attack.1 W m* s0 b0 n9 `8 x& p" u FOG Fiber-Optic Gyroscope.4 z) {) r; [8 X FOIA Freedom of Information Act (US).( s" a2 o$ o4 h MDA GLOSSARY, VER. 4.0 F ' q- X) q( _7 w/ I8 B3 ]1 c110- c4 m9 q4 O) o- Z FOL Forward Operating Location. & j F6 l6 c7 W! uFOLAN Fiber Optic Local Area Network.# q4 q7 w5 T& g& k8 Y+ t- A Folded Optics Any optical system containing reflecting components for the purpose of reducing9 Z( f% X/ @$ k: ] ^' J the physical length of the system or for the purpose of changing the path of the5 }/ o9 [4 H5 y+ S optical axis. ) H6 t, g+ d+ C0 ^) W3 `Follow-On' L* V5 W2 Q: g6 S: _ L Operational Test 4 j3 {6 o8 n' v: Xand Evaluation - }* J4 I- w4 b& @(FOT&E) ; U. Z, x8 O f' ?# G- DThat test and evaluation that is necessary during and after the production period 2 H$ @9 O J6 ~$ jto refine the estimates made during operational test and evaluation, to evaluate . s& `7 D) E3 m, c6 b, @changes, and to reevaluate the system to ensure that it continues to meet : b4 C+ V6 M- a( ~/ x& O# n" C. Goperational needs and retains its effectiveness in a new environment or against / d+ ?; ~( s+ l9 Ya new threat.4 P* x8 S' V4 n& Q" L# l9 b FOM Figure of Merit.' G$ Y D9 {' K! T3 ?/ V FON Fiber Optic Network. , q( k" S! A( \8 F' U) _Footprint (1) An estimated area of possible reentry or the solid angle of a detector or % s8 C0 q7 {/ o+ t) z4 T( G! ?; ilinear area of a detector at a certain location. p# w9 N8 i v* G9 w3 X% s(2) Geographic area in which a focused satellite downlink can be received. 6 ]' ~0 S. c) s0 l" ^9 k" A/ X* a+ UFOR Field of Regard. . f( i; U3 l1 D* F" KForce Closure The point in time when a supported commander determines that sufficient 4 }8 w: j8 B3 k! gpersonnel and equipment are in the assigned area of operations to carry out' p' v) M) u+ F5 U9 f8 J, E assigned tasks.' r+ O+ [. b5 K* } Force Development Test and . T7 q# y, M/ d) I8 K2 `5 c, {Experimentation & k- x8 Q2 ?6 n. Z+ V/ UTests employing representative users to examine definition of materiel + F' Z4 `8 f- `, C" frequirements or support/assess development of doctrine, training, organization, 8 y3 ^+ I; O. Y8 @- J: G2 M" h8 [( n Vand logistics for system acquisition. (U.S. Army). 1 U1 r3 L+ n) [Force Direction The operational management of the forces. ' k% ?7 ^- t1 |Force Integration/ x5 e3 `) S/ a6 u2 g Staff Officer. b! b* ^1 H: i7 I2 h; ^ Army individual assigned to ODCSOPS to serve as HQDA user representative for * X/ c9 V+ S# z6 w/ Ia specific system. Provides continuous coordination necessary for integration of . I6 i3 F$ Q2 T1 k* Sa new system into the Army force structure." P# b% F* Q! o# @' A Force ; O. q0 Y% l* J4 Q. c5 aManagement 7 c3 e W" r+ [) K0 S, G, n3 sThe assessment of the effectiveness of the defense forces throughout an 5 A6 s8 r& I) fengagement and adjustment of tactics and the system configuration as' Q: C4 W; Z" p1 ^ necessary to effectively allocate resources to satisfy mission objectives. 9 f3 g! a! f/ ^( J& U9 d$ {Force Reliability The percentage of the missile force that will successfully detonate within 3.5 ( e+ S4 p) X2 x0 P9 K0 Q% a. C8 _CEPs of the target.! O+ h9 }: r$ r$ Z FORDTIS Foreign Disclosure Technical Information System. " e: z0 h" E. K3 V; P% {Foreign ! R1 Z+ S$ s1 ?7 P' J/ @Government: \, H; h/ u$ h' z Information 7 N6 B& ?& X1 O: N) Y3 K a" X7 X1 tInformation that is (1) provided to the United States by a foreign government or + n: Y9 k9 P2 Y( S0 o: }governments, an internal organization of governments, or any element thereof * ~1 n" A; M: t9 Jwith the expectation, expressed or implied, that the information, the source of2 l, R6 O& X% W! `: _ the information, or both, are to be held in confidence; (2) produced by the United 1 u5 b8 R4 c6 sStates pursuant to or as a result of a joint arrangement with a foreign" f. N8 P7 v9 X; n; r& c government or governments or international organization of governments ) B2 c2 K) x9 @" Z: K5 Trequiring that the information, the arrangement, or both, are to be held in4 d% ^ F) ~7 }" ^* V, K0 k | confidence. - T! m4 j. K) B4 a) j: Y, X: E0 c1 m" [MDA GLOSSARY, VER. 4.0 F1 Y0 s6 l2 r4 G$ ~ 1113 |5 a# }- h- Q4 j& s- w Foreign Military P# \% s4 W9 O, y Sales (FMS) ) e8 [! B- L2 h' S. CThat portion of U.S. security assistance authorized by the Foreign Assistance Act 1 d7 K) w) S8 Oof 1961, as amended, and the Arms Export Control Act, as amended. The* k) | o5 D7 o9 a+ U/ b5 c recipient provides reimbursement for defense articles and services transferred7 N& |5 A* T) Z! c8 |( C from the U.S. Includes case sales from stocks (inventories, services, training) by 2 ]* W U$ ?8 Q: V2 ^7 Jthe DoD defense services. w4 o3 _; @# ~; }: pForeign Security 4 q: ?( t/ s4 B7 M0 D, j8 e% h7 l1 kPolicy Model( a" e# U# p }3 I4 X `4 y* n9 Y/ Y A mathematically precise statement of a security policy. To be adequately 2 _! _1 j9 n0 l& ]8 E# xprecise, such a model must represent the initial state of a system, the way in j1 ^2 D; g: C0 r* H% p# a: v which the system progresses from one state to another, and a definition of a * C% C- ]3 [( Y. S“secure” state of the system. p. d" b; a# C# J: K0 e. JForm, Fit, and 2 o9 O& J* w2 r# k- ?1 eFunction Data- H! s" a. @* M' m/ h7 ^5 W1 v4 \+ v Technical data pertaining to items, components or processes for the purpose of/ i% H$ M y' ?, [% |) m5 P: m" l identifying source, size, configuration, mating and attachment characteristics,3 g) g- Q* y) y% h* U1 p9 Q functional characteristics and performance requirements. 0 h7 |2 c2 W; `5 r$ v$ ?; gFormal" Y' i9 s: R& ^: `) f1 k Qualification " X/ {' \: H$ J$ h( }3 ~, RReview8 |) k9 ~% `( t6 m" Q/ L A systems level configuration audit conducted after system testing is completed ' G# j8 n" I$ Y# h+ } D4 Wto ensure that performance requirements have been met.1 t* x1 r$ Q) ]2 D: Q: | Formerly0 M5 J1 \$ q9 \ h" N Restricted Data 6 ?/ S b6 `' x! G& z6 O$ x$ ~+ u/ XInformation removed from the RESTRICTED DATA category upon joint * w+ R. [! z+ hdetermination by DoE (or antecedent agencies) and DoD that such information) x7 z$ {) X8 a) E, c2 g relates primarily to the military utilization of atomic weapons and that such Z% G& ^9 N3 t. Linformation can be adequately safeguarded as classified defense information. 9 Z3 t, j) S$ @0 l# e. k; AFORSCOM U.S. Army Forces Command, Ft. McPherson, GA.* \5 {5 P: Q9 A& |: ^: J FORTRAN Formula Translation Language.

使用道具 举报

Rank: 9Rank: 9Rank: 9

46#
发表于 2008-12-25 20:06:48 |只看该作者
Forward Edge of . [# `" T' f9 o1 t1 \5 Nthe Battle Area H9 H, _. \- @! F2 T, P(FEBA) , [% l9 v- Z: Y- |The foremost limits of a series of areas in which ground combat units are 8 @0 B J6 _9 Odeployed, excluding the areas in which the covering or screening forces are R6 m5 `- X2 V* V" U/ hoperating, designated to coordinate fire support, the positioning of forces, or the0 t P; k1 |+ s, g maneuver of units.9 l% Z) X; _" p. t Forward Funding Carry-over of RDT&E funding into second year of appropriations availability.% X r m) _# z" I0 K) O Requires permission from high authority.5 }9 F+ n' c, D! j$ V2 z FOS Family of Systems (TMD).- D- Z1 ^+ {- Q8 t. V. W& h FOSS Fiber-Optic Sensor System." u; v1 v. W1 W FOT Follow-On Technologies. ! K j% {- L- N1 |' Z; T/ v1 pFOT&E Follow-On Test & Evaluation. ' D1 K9 X' |4 V7 GFOTC Force Over-the-horizon Track Coordinator (USN term).- u, M* w, H( a% |, d3 } H FOUO For Official Use Only. 8 j& d) G5 _ Y: {- K) AFourth , ]5 _2 L( o0 b3 P3 rGeneration3 h& H1 |# S4 W7 s; p; s0 @2 | Language 9 l; Q) V" E4 k: @A programming environment that produces both screen and report utilities for 0 T) p. S7 P/ H. j* euse by lower-level programming environments. . Q- b9 q& |. j& _1 pFOV Field of View.& u. M4 G" l* P' ~ p( J: {' y FOV Radar [Full] Field of View Radar: @5 F1 L/ P; g3 E9 P- M FP Focal Plane.4 K1 F: A5 b4 \( g) u+ n MDA GLOSSARY, VER. 4.0 F % {& [5 N3 f) U# O G" b112& T" ?+ t! q0 l1 G; C FPA Focal Plane Array. 4 p; ^; B5 P$ H- B9 m4 b5 ~FPC Facilities Protection Committee., a* D7 r9 I$ n7 P, J FPI Fixed Price Incentive. 6 Z3 W- R1 K! P# c0 L1 M; ZFPS Fixed Radar. L- T8 V$ ?7 @FPTOC Force Projection Tactical Operations Center (USA term).; i0 M) d6 I: N$ L& L FQR Formal Qualification Review.+ ~) x" L! u0 V) r FQT Formal Qualification Testing. 6 u' k7 v0 @3 G7 A. cFR (1) Federal Register. (2) France.5 r- Q% l( P/ P8 _3 r- G FRACAS Forward Reaction Altitude Control System. 1 g) N' k. K8 V0 X* F& E1 IFRACS Forward Reaction Altitude Control System.3 \; _% A' m5 S0 Q' V6 d2 H7 m. n Fragmentation - ]7 H8 o! r! N. \) xWarhead " @' X" M' m t6 ^" p0 NA warhead, which releases small solid objects to damage or destroy its targets. 3 B- [! u9 O7 q- [1 @$ wFRAS Free Rocket Anti-Submarine. . b4 L: ^6 O/ a: K3 Y3 z8 tFRC Fire Control Radar 2 i) D6 y1 _, k4 pFRD Facilities Requirements Document.& ?/ w E) ` M5 t, ]/ a W Free Electron6 y9 r& M; O+ g! w7 ? Laser (FEL) - [9 @% v: g: YA type of laser, which generates radiation by the interaction of an electron beam: u$ m% O* R' m, M9 A* C5 V' t with a static magnetic or electric field. Loosely speaking, free-electron laser 8 h; b% N. ]$ ^; {, |technology resembles and evolved from that used by particle accelerators (“atom( r7 X9 i: [" [5 e. r smashers”). Lasers, which are not free electron lasers, are bound electron4 n4 m* m, `5 D( B lasers. + {% U4 w. q: y! z3 S3 L* @( e8 ~Free Rocket A rocket not subject to guidance or control in flight. # P% ?! k( a* N9 T$ lFrequency 0 U# p1 D" c0 d Z! ?- hManagement + L7 a2 ?3 I. v$ G# k0 Y8 U4 z% \The act of allocating frequencies, or bandwidths to a telecommunications9 k5 i0 @4 ]* k system, necessary to minimize the potential interference between % v. F& q Y# l; U! Qtransmitting/receiving devices. Governing agencies and international agreement. a/ o$ O( H+ ?) N6 I4 G* C controls authorized use of a particular frequency, frequencies, or bands. ' i' V L2 Y8 BFRG Federal Republic of Germany.# y: y3 e! F- f6 i5 r FRN Force Requirement Number. 9 {. n+ z! F, e' e$ ]$ nFROD Functionally Related Observable Differences., |0 q' p% G) ^. k8 S' K0 W FROG Free Rocket Over Ground. . d9 _4 g" A, m, v" T* bFRN Force Requirement Number. / p, F& a3 C, M: n6 B8 Q: ~FRP Full-Rate Production. - _6 d3 j/ M% `. B' m, u, I/ YFRS Federal Reserve System.1 d9 v( b! f5 g% a FS&E Facility Siting and Environment (MILCON term). % p; g, z- V4 bMDA GLOSSARY, VER. 4.0 F, \: L9 ~8 N) F u 113 . x: M w! B; H6 i C9 oFS3 Future Strategic Strategy Study.$ x$ S r/ Y+ L% D* F( F FSAF Future Surface-to-Air [Missile] Family. H2 {, H+ S; q! m FSC (1) Fire Solution Computer. (2) Fire Support Coordination., } p0 d0 w: ^, u FSCATT Fire Support CATT [for Weapons] (US Army term). 8 z( a8 ]) @. w5 ?. Q2 p0 L& h0 sFSCL Fire Support Coordination Line. * Y% [+ d: j: ]+ u$ L4 C: P. TFSD OBSOLETE. Full Scale Development Phase. See EMD. " P$ n7 d" d) F E' h1 NFSE Fire Support Element. 1 y5 f E: Y" E7 mFSM Firmware Support Manual. 9 X# M- K) k# U A6 j7 x) M/ w; h# }7 lFSP Facility Security Plan. . I1 ^) x) Z0 |FSS Fixed Satellite Service.* b. K" O: M3 `3 `/ D" A9 u# P FSST Forward Space Support in-Theater.. i7 L( @6 S$ t2 c5 S FST Flight System Testbed. ; H- i3 R9 r0 v0 r" `- cFSU Former Soviet Union.. C" i g2 ?/ X% \4 K FSU Republics Former Soviet Union Republics. ' h3 q' q, v9 z+ g/ GFT Flight Test. % ~; A- x* X9 G4 i3 }: ]4 x$ zFt Foot 5 T+ T, [$ O- ]' u2 H* W; sFTC Federal Trade Commission. 0 X$ r6 D* z4 n" M% X; nFTD OBSOLETE. Foreign Technology Division (USAF), Wright-Patterson AFB, OH. 8 e. q; U8 L8 W+ S- uSee NAIC.5 q+ _* ]4 ^' [( E, R7 M5 [ FTI Fixed Target Indicator 9 r6 Q5 Y! V3 \6 n5 JFTLS Formal Top-Level Specification. + u- s5 j8 F6 OFTP File Transfer Protocol (ADP/Internet term). : \" ^( ^6 I) R$ DFTR Flight Test Round. 2 s, d2 [4 i" I1 O- ?- X4 ^4 U" NFTS (1) Flight Test Summary (2) Federal Telephone Service " Y* E) C6 [) c" WFTS 2000 Federal Telecommunications System 2000. * x! n* W" I) _5 @* hFTV (1) Functional Technology Validation. (2) Flight Test Vehicle.! W' H% e9 |& y. g FTX Field Training Exercise.. d& [- h1 i8 Y# e3 z6 @ FU Fire Unit (PATRIOT).% g, ^- o, M$ y( M FUE First Unit Equipped.. F N% s0 j; x8 b1 `7 K MDA GLOSSARY, VER. 4.0 F ( y3 F4 S- B% Y2 ]8 v b" N9 `1144 i% s/ M+ B: W1 ~! V Full Mission 2 `0 h$ g6 R9 `1 ? L( aCapable( t# t0 t& D( H4 T) U m Material condition of an aircraft or training device indicting that it can perform all8 Q y9 X5 C' H0 g of its missions. Also called FMC. s' {; c! g* r" m3 d, B5 B3 P- | Full Operational D7 p5 ^- q/ o, D5 D$ M* C- cCapability (FOC) $ r% `; B9 y* O+ \4 zThe full attainment of the capability to employ effectively a weapon, item of/ ~, v6 }* i' a! ?" \# l equipment, or system of approved specific characteristics, which is manned and) Z, t, a( e* C% h0 [% }9 b& a operated by a trained, equipped, and supported military unit or force.* ^* T' u6 D# {! ?/ {8 [: \ Full Rate9 ~3 R- j( d- k& i `- s% I; }% L Production5 s' ^% U; z& R. e( K7 C- ` Production of economic quantities following stabilization of the system design V! y6 L& X: I5 c0 {and prove-out of the production process. : q/ {6 D5 G7 O# i% ?8 v1 K7 AFully Configured3 R T" Z" ^5 P/ [9 D( A End Item% }, X+ a8 z' m The final combination of end products, component parts, and/or materials, which ! m. h) x* P5 N& w; O' \is fully ready for its intended operational use. Normally all production units are & K" L; b" b' @ C: pfully configured. Research and development units may be considered fully) }. Z. H7 F# b4 w9 W g( D( t; g3 t configured if they are or are planned to become operationally equivalent to the1 n& f4 z0 g: ~5 O( J1 w production units.

使用道具 举报

Rank: 9Rank: 9Rank: 9

47#
发表于 2008-12-25 20:07:01 |只看该作者
Fully Connected" i, H0 c7 |# `9 I# P Network (FCN); f& o. z( Q3 \& q" { A network in which each node is directly connected with every other node.1 W X' F9 x( ^& [# Q Functional + p. m% n' s, k9 B: D" IAnalysis 8 \9 A9 ^) I% P) aAn approach to the solution of a problem, in which the problem is broken down 5 R4 O$ b, O' }9 R E6 xinto its component function, such as intelligence, firepower, or mobility. Each 9 h- z1 n I% s4 B5 u( h' `, M% V$ rrelevant function is then further analyzed and broken down into smaller. Y$ R3 d) k/ a5 h$ |% U, W functional components until a level of molecularity suitable for solution of the$ Y8 s) M" d5 O% t! m1 g4 @& c+ M problem is attained.: V8 B' z) l* s) X; x5 C3 M9 x2 l2 t Functional + M( {& o3 B* }; y2 L2 bBaseline% U+ F( r3 e, u4 E+ b (1) Established after the system requirements analysis/design activity has/ R; a$ r" ~( r completed the definition of the system functions and associated data,# g8 `! ~+ H: r) \( Y! d- N interface characteristics, functional characteristics for key configuration# m7 U8 D, p6 u items, and tests required to demonstrate achievement of each specified+ A, ] q7 |- ?0 ?- K) g" s+ V characteristic. This Government normally controls the baseline. ( {+ G J6 H/ J. u$ c/ d7 b4 M(2) In configuration management, the initial approved technical # w% [/ e- R$ N3 [3 r3 v, Z5 J8 vdocumentation for a configuration item.) b. L. i* T9 ^( y+ ?8 o0 r: X( p (3) Documentation describing a system’s functional characteristics and the+ Z' m( O ^9 R9 Y" w' w verification required to demonstrate the achievement of requirements.- J& V/ A7 N3 m% B i Functional . u; j+ Z W7 WConfiguration V5 o/ g/ N1 R) E Audit (FCA)( w5 b+ t$ z2 M& v' y, n2 R% K The formal examination of functional characteristics test data for configuration 4 \& B6 F5 p3 Q6 mitem, prior to acceptance, to verify that the item has achieved the performance2 @* M2 |3 z2 L( b7 _ specified in its functional or allocated configuration identification.' j! c! B) O) [) h! T0 a* c& { Functional , X9 R1 |' {: |7 h$ [ C- Z7 c% V7 [4 yEconomic* Q' j! z& |" `" K% C5 c Analysis (FEA)) O* Z! i8 m; c7 J4 `8 T A structured proposal that serves as the principal part of a decision package for , X9 `) x$ S2 S7 {enterprise leadership. It includes an analysis of functional process needs or $ c$ n; W6 |& [ a$ rproblems; proposed solutions, assumptions, and constraints; alternatives; lifecycle costs; benefits and/or cost analysis; and investment risk analysis. It is# }% G! Y' Y( ~ consistent with, and amplifies, existing DoD economic analysis policy in DoD3 _+ f( T7 q; |/ [1 I Instruction 7041.3. 5 |0 ^% ]9 X, G3 F5 pFunctional Kill The destruction of a target by disabling vital components in a way not) T! e+ R L6 m immediately detectable, but which nevertheless prevents the target from # h. o9 j1 v0 I$ Z1 pfunctioning properly. An example is the destruction of electronics in a guidance 0 H/ A4 z* h/ z& jsystem by a neutral particle beam. Also referred to as “soft kill.”! p x% @* ?3 Y0 S! b9 ?+ a# l Functional8 T" t9 s4 k$ O9 d/ _9 S0 W Support ( j5 r1 u; i$ ?9 lSystematized methodologies and procedures, or a common set of standards, ! s. i' d1 l( happlied to materiel acquisition programs. ! _+ a# a, y! A: F, N7 [; wFunctional : M; p6 a$ h( t0 t3 q4 i9 B. @Technology 5 C" ^* Q" H) H+ qValidation (FTV): p' d6 {7 o5 D& F9 \; z$ [3 ^8 M Program with the intent of proving or disproving a technology is useful for a given' \; |' U5 z4 ~ application.3 Y r/ B- y6 O4 D+ N8 b MDA GLOSSARY, VER. 4.0 F8 `( E7 i! b; \ 115 1 \' }7 y+ N9 o# S7 JFunctional; W+ Y) {! C- n7 G9 a Testing+ R7 Y) }6 ]2 r/ x: e/ y The portion of testing in which the advertised features of a system are tested for: w, h8 m' v1 I, ~, D# a5 x1 d" m/ F correct operation.6 r5 k3 x$ J8 X* _6 S Funding Profile Program funding, usually displayed in columnar spreadsheet format by years, : n4 \" O( L: fstarting with previous year through current year and out-years.# h. N$ G, _/ h: f. c' K8 F Future Years / i u1 g4 I. w1 R1 eDefense Program0 |/ M& v# c. |% q! }* a (FYDP) 8 H! L% x" Z3 t2 wThe official DoD document that summarizes forces and resources associated with " ?4 q f9 f+ ?1 z/ j" \, |programs approved by the Secretary of Defense. Its three parts are the0 D) j$ Z4 e; @- [+ k/ g. c organizations affected, appropriations accounts and the 11 major force programs 5 s; G8 M+ w- i! A. J3 [/ \" W! u(strategic forces, airlift, R&D, etc.). Under the biennial PPBS cycle, the FYDP is 7 A, T& y3 Z* R) }4 fupdated in even years in April (POM); October (budget); and then in January / g8 e) t0 ^3 A, P(President’s budget) of odd years. The primary data element in the FYDP is the # a- j7 i4 ~; T, ~. _: q2 kProgram Element (P.E.). Formerly known as the Five Years Defense Program. 3 L8 M, b* i6 n1 QFWCA Fixed Wing Combat Aircraft. 3 V' k; Y/ N4 ?" v9 X0 h) @$ cFwd Forward.4 v. H4 o7 k; \9 F5 Q0 g- T1 C- a' _ FXBR Forward-based X-Band Radar. 0 L p1 h* _" ]; TFY Fiscal Year. ) p; B7 f2 q0 t! y; e8 }5 W& |$ XFYDP Future Years Defense Program. 3 X3 f& f* s5 UMDA GLOSSARY, VER. 4.0 G" a$ S5 Y- J& V( m 1166 R1 K1 F9 Y- \2 K G Giga (one thousand million).$ w. ?/ R4 E2 [0 C8 P! D, I g Gram.: f6 l5 S/ M9 c. F5 ^8 ?- F G&A General and Administrative costs. 4 y' L$ E2 n- M! \G&C Guidance and Control. ) J* ^1 \. I& t$ X3 k" B. VG&O Goals and Objectives. / _; |& q' E) G! Y5 `G/A Ground-to-Air0 F) ~9 q) V+ H G/G Ground-to-Ground. 0 f$ d* B% U B. JGaAs Gallium Arsenide. 6 i7 ], ]+ z% I, z, R/ f' DGalosh The Soviet Anti-Ballistic Missile system built to defend Moscow from missile- M- Q2 i' ^0 Q) z7 Z2 J. w attack. 9 {: e8 b) S( k5 UGamma-Ray Electromagnetic radiation resulting from nuclear transitions. Although incorrect,. y7 T# x! C6 `; a high-energy radiation, particularly “bremsstrahlung,” is sometimes referred to as% }4 q" |# e% H; r3 k1 ?( A gamma radiation.( q. F* @0 Y- j( l Gamma-Ray Q& \7 ^ Z- a: u! G6 KLaser 7 Q4 e+ }1 O" F! v, CA laser which generates a beam of gamma rays; also called a “graser.” A ! i$ e& e* s. v1 ?# |) Bgamma-ray laser, if developed, would be a type of x-ray laser; although it would, n4 O& I7 Q; o; _$ Z | employ nuclear reactions, it need not (but might) employ nuclear fission or fusion& }; X1 Q% Z; r0 f. A reactions or explosions. 3 S6 i- X, q6 K, tGAMS GPS (Global Positioning System)-Aided Munitions.7 s+ U9 Z: G. G7 M6 Q9 Y GaNMPA Gallium Nitride Microwave Power Amplifiers. (A demonstration program to develop8 V/ G$ b- y9 n/ k* r/ ?8 i( [+ { GaN based transistors and integrated circuits for power amplifiers in systems; s" D. f% G5 Y such as Ground Based Radar. Goal is to reduce total weight and size by a M5 Q! {6 T( @# T! z( O factor of 10). . f6 d0 _6 S# `% `5 y# TGAO General Accounting Office.) s3 ?' q$ \3 m; S4 N' f& h GARDIAN General Area Defense Integrated Anti-missile Laser System.9 H$ G; z: n! e& ` GAT Government Acceptance Testing.5 m6 \, J" o1 l3 ~ GAT CALL Guidance, Apportionment, and Targeting Call (JFACC term).8 P/ F1 K: p% [; n+ {% R& [ GATE Graphic Analysis Tool Environment. j" ?* k2 v9 ?# t- K8 J {, _Gateway An element that contained a node on the SDS backbone network as well as on 9 Y. @, @& V I8 m- h. j4 h2 lsome other network(s) and would have performed protocol and format 8 _0 e9 K0 @/ |8 d# g* [conversions necessary to accept messages from one network and retransmit: ^3 G- q1 v8 o! d+ h them on the other.% J3 N6 v5 o7 N( H! D GATS GPS (Global Positioning System)-Aided Targeting System. 4 I6 |" V+ a, ?4 h& Y& BGB (1) Ground-Based. (2) Gigabyte. 5 {, k" n+ D7 v3 D+ F% h- U' TGBD Global Burst Detector.9 m- Q/ O' J. P8 K Y GBDL Ground-Based Data Link. + Z8 ]9 e7 N6 e( K- T5 aMDA GLOSSARY, VER. 4.0 G 7 X8 ~; l1 t3 S& \4 l- W) ~" R! Y1175 w; e! s3 k4 X. Q- ]2 G2 H8 [ GBEV Ground Based Experimental Version.3 {4 N2 _7 I) `" `' O( P GBFEL Ground-Based Free Electron Laser. ; _4 {( i" e7 B3 }) ZGBHE Ground-Based Hypervelocity Gun Experiment. ! F; [ ]+ G3 v- @; qGBHRG Ground-Based Hypervelocity Rail Gun.+ x* C7 f. m! G GBI OBSOLETE. See Ground-Based Interceptor.! f" v1 a* w+ A/ V/ l GBI-P Ground-Based Interceptor – Prototype. 7 n: A) y& y0 ^GBI-X Ground-Based Interceptor Experiment.# t) Q8 D7 n& \1 m9 N; C, ? GBKV Ground-Based Kinetic Kill Vehicle. ! T: v+ y* M+ M# r k @( R- \" ?GBL Ground-Based Laser. % B! r; @0 C! n; PGBLD Ground-Based Launcher Demonstration. * f9 E/ G% I! ?! d3 n, H. ?3 V1 iGBLRS Ground-Based Laser Repeater Station. 0 n& H& n7 R) n2 @4 b) NGBM Global Battle Managers. ; y4 G- l. W/ \3 y! x1 N0 R; sGBMD Global Ballistic Missile Defense. 8 }2 ]2 @; G% P) `" Z/ CGBMI Ground-Based Midcourse Interceptor.2 o8 |4 [: W, t' A1 g GBOS Ground-Based Optical System. 4 M6 i5 k- b5 j0 i! Q* y) CGBPST Ground-Based Passive Signal Tracking.. e$ u, m6 R8 x7 F GBR See Ground-Based Radar.; J$ ^4 |) K/ a( L v7 X! t GBR-M Ground-Based Radar-Midcourse. 1 o* H2 j0 U) \" P: u6 n6 B1 ^6 Q; DGBR-O Ground-Based Radar-Objective.0 B6 A3 C& r: `1 P. }1 L GBR-P Ground-Based Radar-Prototype. . d' ]# K: ~5 q( z4 R7 {GBRT Ground-Based Radar Terminal., r0 K6 {" a# P+ @/ I GBR-X The experimental version of the GBR. % Z+ k( g1 I3 zGBRF Ground-Based Radio Frequency.

使用道具 举报

Rank: 9Rank: 9Rank: 9

48#
发表于 2008-12-25 20:07:14 |只看该作者
GBRI Ground-Based Rocket Interceptor. y1 C2 L4 I/ W" n. q$ G. w GBRT Ground-Based Radar Terminal. 8 S3 b0 p; Q( A- S+ D, M4 HGBS Ground-Based Sensor. & j) j9 _7 }0 ]& Y: r- c' MGCA (1) Guidance, Control, and Avionics. (2) Guidance, Control, and Airframe.9 R* p+ X# p( G, S1 g0 k" B7 O GCC Ground Component Commander (JFACC term). 7 t0 x4 i+ j% w0 S" s8 W' \1 yGCCS Global Command and Control System. ; S8 r2 ?) p2 d9 }% B1 MMDA GLOSSARY, VER. 4.0 G' x& ]9 x: s7 |, U0 ] 118 5 e, V J& q$ u4 M( }GCI Ground Control Intercept.5 i" I R) w. F% X, ^/ f$ R7 O GCN Ground Communications Network. 6 V; e7 g2 u" _0 P- i2 e& o2 kGCS Ground Control Station. 2 e+ b9 \) h$ T0 `; GGD General Dynamics.1 ]4 q' c0 w4 D: Y, ]9 F& Q GDL Gas Dynamic Laser. 6 j/ C* U& y3 {GEDI Ground-Based Electromagnetically-Launched Defensive Impactors. 6 A0 c3 v8 o) }$ KGEM Guidance Enhancement Missile (PATRIOT).- t0 D6 e2 r& R1 U' H4 e6 U General Manager . B( x1 R& o" S$ _Program7 [+ P* Z% h5 @4 i Management, H! c& o4 S: V9 m. n Directive (GPMD)0 U5 w& O' v) d$ a. e0 i OBSOLETE. The primary document used by the GM to direct the Service BMD, L1 z$ [6 Y$ g3 N1 v PEO on the specific actions necessary to fulfill BMD program requirements. 9 q( m: r# K' x* [8 FGeneral + O* A) b0 w& DSpecifications & I9 l! m7 V7 x/ q- \7 z IA general specification covers requirements common to two or more types,/ c* ]5 U7 @0 r& T" n# m& M8 P* ~ classes, grades, or styles of products, services or materials; this avoids the ; M" }/ ?# @. U8 Prepetition of common requirements in detail specifications. It also permits+ x1 G* i4 q; p [2 E$ z changes to common requirements to be readily affected. General specifications' k7 \# x3 I, w may also be used to cover common requirements for weapons systems and 7 [* }8 f) z5 |1 S5 W- x2 Osubsystems. + V: K" ?, Z: N# t1 NGeneric Rest of & B( r: G( S8 Q" O, `World Target& L1 M1 g. J$ E% n (GROW); |+ ?. `/ B6 E/ U3 {# d6 J5 J6 W Strategic target being developed for GMD program.% z% Y \! A2 a GEO Geo-synchronous Earth Orbit. . J( K) |, m e$ t7 |GEODSS Ground-based Electro-Optical Deep Space Surveillance System.- ^$ d& N% B1 N0 f# D2 ~3 m Geo-stationary % |/ q& ]* P. g2 A* lOrbit (GSO)- W6 d3 k+ f/ m+ G9 R" ~: |6 h) Y An orbit 35,784 km above the equator. A satellite placed in such an orbit2 B: E; j, B* M, I revolves around the earth once per day, maintaining the same position relative |4 n4 J+ C0 [( j7 A' Rto the surface of the earth. It appears to be stationary, and is useful as a $ i- t1 O, f) {4 U. o4 }( Jcommunications relay or as a surveillance post. / I( l) v" B. A bGEP OBSOLETE. Ground Entry Point. IFICS.* P3 U# u; ^ S3 Z- h$ p* S3 j GES Ground Engineering System. 3 [1 r' D; l% q. n, L( V1 Z0 n4 LGFE Government Furnished Equipment. See Government Furnished Property.( P2 p0 @; I5 Q/ @, T* x) A GFI Government Furnished Information. * N) B, B6 k7 I7 @GFM Government Furnished Material.; H J0 I) E) @" V. t7 ~ GFM/P Government Furnished Material and Property. See Government Furnished . S+ j7 }# R! n( r) M0 W+ o' bProperty. " g3 j: C* j5 SGFP Government Furnished Property.5 D. D/ X9 K8 O t ^& v GFS Government Furnished Software. See Government Furnished Property. ( C8 V9 d& Q$ \, q' ?8 B' L. hMDA GLOSSARY, VER. 4.0 G ; F) [& @# Y) m119 " |% u5 ~) c) S1 xGhosting This condition occurs when two or more targets reside close to the same plane5 v6 H) `' A" k$ \" F: ~. S& f also containing two sensors viewing the targets so they are within experimental - E, I) Z% i1 X1 G: z; @determination of having the same hinge angle F. Thus, ghosting depends on # \. ?& G" r8 g, h* v4 oLOS error and positions.7 H7 t% D+ z3 H3 V$ v. M5 S8 U GHz Giga Hertz (1 x 10(9) Hz). 4 Z0 R/ T5 C& w" t6 B1 k! [3 \4 UGIDEP Government/Industry Data Exchange Program. ! P' }3 i1 l N& Z- [/ s- K: a" MGIF Generic Interface. ! ]8 r4 s/ p+ X4 K; n- KGII Global Information Infrastructure. 2 y! Q+ Y0 x3 qGIP Ground Impact Point.- U, Y9 m) k8 q. ?9 |& m GIS Geographic Information System.( M3 }2 _+ [' |, Y2 Z6 f GITIS Government Integrated Technical Information System. ) Z5 `& B) I7 M; [ z# m; RGLCM Ground-Launched Cruise Missile., c3 f! n% S3 D$ n: P3 q" K GLP Ground Launched Probe. See Brilliant Eyes Probe.) u% o( Z x" _( o( ]- x3 a8 y8 l Global ' k0 l+ ?- F- _! k, M0 WEnvironment . ^2 s" l) M. U9 |The ISTC Global Environment is responsible for the creation, propagation, and : k8 o" m* w; }4 dmaintenance of test scenario common knowledge, how subsets of this; d. o6 y# L4 E information will be determined, and how common knowledge will be disseminated0 t" y7 J- n1 u3 L9 L to the various element representations (nodes). The Global Environment + g3 E6 v; d/ f' Y' _performs functions which are common to the scenario such as timing, health, / x2 S; E4 t2 ]8 V) X/ fstatus, state vectors of objects, and effects models.( w7 V5 `; k; h Global 2 P2 G" R8 h# q; _' S- j9 X7 rPositioning 3 l: j0 B, a/ {5 x# H2 x0 ^' r% iSystem (GPS) ' I; g2 Q$ D4 f3 e9 Z4 s# aThe NAVSTAR Global Positioning System is a space-based radio navigation y* \1 j/ B" B5 M- ^$ E! c! L' m network providing precise positioning and navigation needs of all the military $ o) v: a" @5 S: }services. In the fully operational configuration, there will be 18 satellites in six 6 ^) y% i0 G! ~) x; ~" v- Borbital planes with an orbit period of 12 hours at 10,900 nautical miles altitude.' q' N' x! Z8 X% t Each satellite transmits three L-band, pseudo-random noise-coded signals, one 4 {% L0 J; h( R9 ^8 y+ FS-band, and one ultra high frequency for spacecraft-to-spacecraft data relay. 9 |, V5 O; T' l* hGlobal Protection . ]+ S: \6 f3 \7 b OAgainst Limited: [: v( o% u5 ^! h9 a- P Strikes (GPALS) # O6 `2 `( `+ h8 p# S' o0 wOBSOLETE. GPALS was an architecture denoting an anti-missile system / I2 U$ Z" u, V; i" t- @5 @# Zdesigned to provide protection against limited ballistic missile strikes, be they) R4 P! ]) Y2 H) [' E deliberate, accidental or unauthorized—whatever their source. GPALS was! B: p4 L% S, F5 l+ l1 B" R* k) z9 `8 _9 Y composed of three interrelated segments: (1) theater ballistic missile defenses, " }/ F/ X2 Z& z7 yand associated space-based sensors, to protect U.S. forces deployed abroad, % K# a3 l3 f& N2 p! L+ P" \& m$ Vand our friends and allies; (2) ground-based defenses, with space sensors, to4 u/ |& `, r# T2 e protect the entire United States against long-range ballistic missiles; and (3) 9 Q, C! M& f4 n: M5 iinterceptors based in space – Brilliant Pebbles – capable of providing " K* }' g E1 e$ u5 H$ D6 X# ]continuous, global coverage by intercepting enemy ballistic missiles with ranges- J6 j* Z' u4 a4 C" R greater than several hundred miles. : _ o1 G" ~5 Y/ v9 r6 FGlobal Protection , B" Z9 m9 ?( hAgainst Limited3 e- }' H2 c* I R Strikes (GPALS)( j% o, Q j& a' W0 D Program ! M, L- R7 j, Y% hOBSOLETE. The GPALS Program consisted of six Major Defense Acquisition7 u$ R y0 T( ]& \) Q! J: o Programs: GPALS System/BMC 3 X9 K$ }) c+ w , National Missile Defense (NMD), Global Missile- H0 g- ~ Z8 m5 X# R Defense (GMD), Upper Tier Theater Missile Defense (UTTMD), Corps SAM, and % \6 U' _" ~$ M9 \+ U+ `( B7 x0 vPATRIOT. Army PEO GPALS was re-designated PEO Missile Defenses in 1992. & p/ i' J/ ?# I0 X1 tGLOBIXS Global Information Exchange System. 5 K$ W$ q1 O: Y2 f/ D: [* F1 B* nGLONASS Global Navigational Satellite System. , Y" U7 c& T5 Z" U6 I2 V. }MDA GLOSSARY, VER. 4.0 G$ j- \3 X' Z& k) ~ L 120 8 }+ k7 |, Z2 FGLOW Gross Lift-Off Weight. 2 w2 \) O0 l! k1 t1 g1 @3 RGLP Ground Launched Probe. See Brilliant Eyes Probe.' ~- k- Q8 o4 A/ F' ~/ v GLS Ground-Launched Sensor.' Q( n; y/ P3 D/ U: q' y- s) Z GM (1) Guided missile. (2) General Manager. & G: G6 ^" K+ N. O8 OGMACC Ground Mobile Alternate Command Center.* P# y3 j M/ I0 }$ N& n* H6 ? GMAOC Ground Mobile Alternate Operations Center.9 t$ B) {/ a6 g% L+ P) \ GMCC Ground Mobile Command Center. 8 ]( R k* |1 G! HGMCP Ground Mobile Command Post./ L. L, C( b: i7 U2 v: X8 F; F! L8 y( Z GMD (1) Ground-based Midcourse Defense (formally National Missile Defense) (2)# ~1 |( y& s- W% v5 _- V9 ] Global Missile Defense (OBSOLETE).& l0 }6 _8 }; c) H GMT Greenwich Mean Time.2 L: }, R# R2 P4 l; B$ K. t( W GMTT&C Ground Mobile Tracking, Telemetry, and Control. ! _; \8 y/ [3 ^( a% P' W6 ]GN&C Guidance, Navigation, and Control.# e* T" [( M7 G6 ~4 M" H1 ` GNC&P Guidance, Navigation, Control and Propulsion. ]5 ?, L `2 c8 ? GND Ground. - K# B1 [ _$ G! F, J+ M* kGOCO Government Owned, Contractor Operated." l3 _! g! P% g# G GOES Geo-stationary Operational Environmental Satellite.2 u( t8 e9 I/ G i( K/ y GOI Government of Israel. 6 D& R, A, \9 a5 ^! i0 ?* Y* g; B, IGOJ Government of Japan.

使用道具 举报

Rank: 9Rank: 9Rank: 9

49#
发表于 2008-12-25 20:07:26 |只看该作者
GOSG General Officer Steering Group. " Q$ M1 y2 T% u; m$ rGOSIP Government Open Systems Interconnect Profile (CALS term). 8 q, N- g8 N, ~+ H) n7 ~GOSP Government Open System Protocol (CALS term). , [' A" g7 P: u; ]& yGOTS Government Off-the-Shelf. 0 g% N" R% w& pGov’t Government.3 ~6 r/ ~" W8 L/ L Government) t. P8 y1 a+ X u Furnished 3 _8 X9 {5 A4 A/ q3 x- A7 zProperty 5 W: M) |$ m, Y+ z' EProperty in the possession of, or directly acquired by, the Government and; U( ^$ o. E5 l" O$ k& M subsequently made available to the contractor. (See FAR 45.101.): ~( I" u% U9 j Government" r" Q8 E4 Y' M: J1 i" } Verification + q V y8 d8 y2 i3 iManagement + Y% |/ w2 o n) t$ gPlan (GVMP)+ ^- v9 B% F% G& c3 r8 e A management document that provides the overall framework for BMDS. z; e, A7 Y5 b$ H9 b1 ? verification. It includes processes for implementation, organizational' N, O% r h# l _9 J3 S+ F7 w% U) z relationships, and stakeholder responsibilities. It covers the full scope of BMDS / [4 L" v+ \4 c) p4 g* iverification and identifies how all BMDS verification activities will come together to% [# `. x4 _; m! m confirm BMDS capability. w3 L/ L; m) X8 pMDA GLOSSARY, VER. 4.0 G, W7 Y6 p% f( L' T( A8 ` 121 $ L- M' V' u: G7 Y9 gGP Group.; z$ u8 @( I& M% w3 C GPALS Global Protection Against Limited Strikes. 0 u E8 C; r* J; [8 CGPC Global Protection Center.5 p. d) |* Z8 @$ t" g8 | GPMD General Manager Program Management Directive. ' v1 A6 Q. [) {' j+ O* ^4 | XGPO Government Printing Office (US). + y% P" ^% l5 UGPP General Purpose Processor. ; ^: ~6 \- D# iGPS (1) Global Positioning System. (2), Global Protection System.- G9 m8 ?! U6 ^ GPSIU GPS Interface Unit. . m: q: @1 `/ S" d" y( GGPU Guidance Processor Unit (US Army term). # ~: l& t5 s/ v9 g$ [* H$ XGraceful$ c$ C4 l& q8 k Degradation7 F) A: K. ~# F" G# i A condition in which a system continues to operate, providing service in a 8 L. r, q: s4 W! Ndegraded mode rather than failing completely or catastrophically.5 `, D8 v7 l% J1 N" p GRASER Gamma-Ray Amplification by Stimulated Emission of Radiation. (See Gamma- - i- v0 o4 D* ~( a( p$ URay Laser.) 1 R1 y7 E: X+ X! g6 j0 B5 j1 _! TGRC General Research Corporation. 9 B4 V6 g: r- q9 mGreen Code Interface Software. 7 E( p- U1 B/ C2 i8 [Ground-Based; T6 i$ @) L8 k8 c Defense / C/ \+ z; m& L5 v9 O; [, kThe ground-based sensor and weapon systems of BMD. ) [5 r+ P& S3 o& N: G* k. ^Ground-Based7 A: h" C3 F2 C j# e Interceptor (GBI)1 ?6 e0 D; ~2 f1 W5 A A kinetic energy exoatmospheric interceptor with long flyout range to provide, 9 ]! E+ O. }: N' q( B/ e0 [& V0 ywhere possible, a multiple engagement capability for defense of the U.S. with a * P4 N ]: Y) c+ V$ `( [/ z. \% j9 trelatively small number of missile launch locations. It is designed to engage7 F# ?3 ~. y) U" l6 Y$ V; ~ post-boost vehicles and/or RVs in the midcourse phase of flight./ T+ H; L+ f: F6 | (USSPACECOM) (Successor to Exoatmospheric Reentry Vehicle Interceptor0 J$ w: E+ Z( ^+ L, A Subsystem (ERIS).) See EKV.7 q7 B# \* N# W, m Ground-Based, z) i$ B. W( i! ]. I Interceptor, x( y' W# y/ d' {; T Experiment - h8 p+ E1 {: [( t(GBI-X)2 c3 O `6 l# b' F Designed to infuse advanced technology and promote competitive environment ; O8 s, ]/ S- Pfor GBI.! P) D6 h a- g6 I1 b Ground-Based2 ]" o! s1 o$ r9 Z* W" _ G! { Radar (GBR) ( |; B- y. w [A task-able, modular, multi-function, phased-array radar that provides! `: w% `& b( g! ^7 ^( N4 H8 t; T surveillance, tracking and engagement planning data in post-boost, midcourse, 8 {& F! v+ H+ r4 O6 C: L8 V) Y5 d2 Iand terminal flight phases within its capabilities. It also provides target 5 w" Y' Q- k7 G7 Cdiscrimination, in-flight target updates (IFTUs), and target object maps (TOMs) to3 _8 M4 |8 r! @: j+ x9 ^) D interceptor vehicles. See THAAD. (USSPACECOM) 1 z/ R6 j: \" L3 O1 X PGround-Based/ \) Y0 C0 _/ N Radar Terminal" ~1 X7 q$ K8 ~& B; c (GBRT)! w7 H+ k# S O0 ~) g& T The sensor for the NMD system. An X-band, ground-based, phased array radar 9 n5 G- R# p! ?" p3 l* @capable of detecting, tracking, and providing discrimination information to a0 b. v- A$ l+ L1 K. c* l ground-based interceptor.1 z* H! i' }4 a% O* {: { Ground-based ; C+ }5 X' ~, f2 CSurveillance and + E9 B7 D7 L' u% ^! o) ~Tracking System 3 O3 s% [/ Q5 L2 s \1 H, L% U2 [(GSTS) 4 E$ g1 \& m5 r- }4 E1 ~5 K* GA fast-response rocket-launched sensor, which can support the SDS midcourse# A/ Y, ]1 [7 a Z sensor suite by employing multiple Long Wavelength Infrared (LWIR) wavebands . L/ |. z+ v! h9 z5 _, x. Y# Vand a visible waveband sensor to provide tracking and discrimination of' W `4 i! C' D- c* V! x6 O( _6 d, i& f' h potentially lethal targets.' l, |+ `9 K' c MDA GLOSSARY, VER. 4.0 G / ^2 ~! ?9 c0 K, \. A122! S1 @* O# F$ W Ground Entry ( W$ w& E" t. LPoint (GEP)# h# a2 o$ _' {# g& ^6 ^* v& G OBSOLETE. GEPs provide the communications interfaces between the SDS1 U* F) P6 L/ [4 f" c5 | space orbital/sub-orbital elements and the C2 E. See IFICS. ) t9 n, D( l# T; j4 _; LGround Mobile 1 R& A: G/ n, ?, ?Regional# r, A* ?1 @& s C7 f Operations + A" \6 o7 S, W1 B" ECenter% m0 u0 }% e' ~% }/ ?( ]9 r1 b. `; N (GMROC) ( g1 l! [2 D6 F3 ~% _Transportable ground segment of the Regional Operations Center.4 e( T! F% P9 n/ J Ground Zero The point on the surface of the earth at, or vertically below or above, the center) @: x8 L2 K, u/ o1 r of a planned or actual nuclear detonation. , E# b# n# N# xGS Garrison Support (US Army term)., X8 J# ~% x, p! x& Q' p3 @ GSA General Services Administration (US). * o- h* n+ s% K( SGSDC Ground Station Demonstration Lab. 0 q9 d: D1 C! \2 t0 \GSE (1) Ground Support Equipment. (2) Government Support Equipment.* _, A; t$ B& R4 R% ^ GSFC Goddard Space Flight Center, Greenbelt, MD. `) t0 E# Y/ C( g: F GSII Government Services Information Infrastructure. $ S- y3 y) I' Q* u% N. |0 QGSM Ground Station Module. 0 @- Q3 p4 P" h v ^: `GSO Geo-stationary Orbit. h/ }* B6 _/ K/ sGSR Ground Station Radar.% o% S8 i- T( D) N. Y% u& @4 s GSTS OBSOLETE. A fast-response, rocket-launched, Long Wavelength Infrared% J( J7 z. y; O$ E" x7 t+ k+ W (LWIR) and visible waveband sensor, which would have enhanced the 3 b* h7 ^- L! ~; F2 G& `+ winformation available from the SDS’ midcourse sensor suite by providing tracking6 G0 G/ z) C; D5 j7 ?: r$ Y- E; M and discrimination data on potentially lethal targets., U- ~7 m! _) F: j0 ?' p GSTS (F) GSTS Farm. : B$ n2 G9 r$ v$ d; O0 H8 NGTA Ground Test Accelerator.8 `5 s% b+ w# u* A; Y5 `9 b n" m7 J GTACS Ground Theater Air Control System. & ^! D/ H& y5 U. M+ q* mGTE GTE Corporation. . G! b8 A; c; _) |( cGTF Guided Test Flights. " B. ~# K7 k+ r0 t: t6 E7 N P2 {GTM Global Track Manager.- j$ Y6 C1 d7 v C/ v GTN General Technical Note. + U* O+ t+ X4 q6 CGTR Gulf Test Range, Eglin AFB, FL.: e+ y1 O1 l# P3 y6 N& A5 J GTSF Guidance Test and Simulation Facility (PATRIOT), Huntsville, AL.. I5 S! w' F; w. a2 o" q GTV Guided Test Vehicle.8 \) H/ @: X# T+ T9 p GUI Graphic User Interface.1 l5 y0 P. ~, ~- k MDA GLOSSARY, VER. 4.0 G . q" I) C+ ?: V+ b4 b# i123 8 `2 X& S1 H4 u* N' z; F$ XGuidance (1) Direction, altitude control, and navigation (where appropriate) of sensors ) I5 G+ R& U4 s% ] y$ Z% ~or interceptor vehicles. ! Y& T( [, y) ^, s/ b+ V$ ](2) The entire process by which target intelligence information received by a 7 A7 R7 c! x/ d1 h* ^5 m! l: xguided missile is used to effect proper flight control to cause timely9 c7 L$ g4 U% ]0 N# m4 ? direction changes for effective target interception. 5 p; ] Q. e8 t/ U$ VGuidance & \! ?5 \+ }. |4 f5 K$ z& f; Z1 U! D0 BEnhanced ; r, ?4 P% a% a1 L$ r; v& _( {Missile (GEM) . h, y, f& P$ t! g; s$ ]A companion program to PATRIOT PAC-2, which includes enhancements to the/ s# S5 L U1 w$ e8 Z& `9 U" h radar to increase intercept range and performance.- [: V4 _) D0 d& i* s$ a# Z* }2 i Guidance : [2 J( v6 W+ Y; Y6 v4 q* l& fSystem (Missile) , @, m) Q. O0 h% Q$ tA system, which evaluates flight information, correlates it with target data, / d! f6 J7 N1 tdetermines the desired flight path of the missile, and communicates the * V9 ^% i* B; S4 F; {necessary commands to the missile flight control system.& P9 K; ?: \7 S/ ]$ o Guided Missile An unmanned vehicle moving above the surface of the earth, whose trajectory or 3 f9 ^6 ~0 Z8 h* U' P" Vflight path is capable of being altered by an external or internal mechanism. 2 m9 F1 n' i! k/ z0 M2 {GVSC Generic VHSIC (Very High Speed Integrated Circuit) Spaceborne Computer.1 y; A `8 x" \( b GWAPS Gulf War Air Power Survey, 1994 [a DoD-sponsored survey]. ; Z7 p- M+ q' @7 f9 N* uGwd Giga watt-days.% T4 F3 @' k* R0 s GWEN Ground Wave Emergency Network.) ]% w+ g+ N2 p6 l GZ Ground Zero., {1 v: S4 t- s V! f MDA GLOSSARY, VER. 4.0 H ) `& D2 Y9 i, m, k9 N/ @$ O9 C124 3 P, ^7 {2 v% Z8 j2 OH Hour. ! W# H7 r! k" H8 r1 M1 ]H&S Health and Status.7 D& B, }5 F) l7 v" f( n H/W Hardware./ L) V+ s1 l6 \. t2 ~! t+ T. T HA Higher Authority.4 z2 ^6 R& j1 B! B7 G: @ HABE High Altitude Balloon Experiment.- K% f4 n+ R+ c3 u HAC House Appropriations Committee (US).% I) h7 T2 L3 t0 [ HADS High Altitude Defense System. + Z3 c s7 p. l5 F6 f9 ~HALE High Altitude Long-Endurance. 2 u1 y. Q' q# P. W& NHALE UAV High Altitude Long Endurance Unmanned Aerial Vehicle. 9 c( ^& F( p7 }1 q; y; F# w% ~Half-Value. y9 G- i. s, s& W Thickness (HVT)( M; G( @. c' n) c The thickness of a given material, which will absorb half the gamma radiation 8 [% |' d. y* _% X- b- G! qincident upon it. This thickness is inversely proportional to its density and also * v. B2 H9 |# _depends on the energy of the gamma rays. 4 E: K9 {+ O# H$ VHALO II High Altitude Observatory II 5 j0 A2 [0 V N0 n0 MHAMS Hardness Assurance, Maintenance and Surveillance.+ F7 j" O$ S2 n# _% w Handoff This occurs when information on positions, velocities and tracks are given by one % d% g3 ~. z+ N: S3 i; v0 B9 Xsensor or system to another and the first sensor or system continues to track the D6 n4 Z' o8 f5 R6 `2 [ o; r objects. 5 l/ P9 | |. h, R5 T* SHandover This occurs when information is passed on to another sensor or system in which 5 `7 p' N7 P, C2 n% |; Gthe first does not continue to track./ w, w6 Y6 k S$ {$ } T* } HAOI High Altitude Optical Imaging.

使用道具 举报

Rank: 9Rank: 9Rank: 9

50#
发表于 2008-12-25 20:07:43 |只看该作者
HAOIS High Altitude Optical Imaging System.8 T; Z5 n% Q" s4 L3 C" \ HAP High Altitude Probe. 5 t! c4 s+ [. A( I. JHard Kill (HK) Destruction of a target in such a way as to produce unambiguous visible \, R& O( T$ devidence of its neutralization.# x+ G2 J1 }, X1 a, K$ U3 { Hardening Design and manufacturing process and other measures, which may be employed# ~7 X# O& U" ?/ v$ c' W$ o to render military assets less vulnerable. 8 Z/ |5 C/ Q' ?# v2 g; [* EHARDMAN Hardware/Military Manpower Integration (Navy ILS term). + g. i. \1 g& i0 g$ f, RHardness A property of a target; measured by the power needed per unit area to destroy 0 L `) O8 U& athe target. A hard target is more difficult to kill than a soft target.0 J( g/ ^2 e' B6 t' d I Hardware-in-the- 9 s4 Z K! s; E% VLoop (HWIL)4 r5 s% H' Z# T0 } ^ Tests in which BM/C3 computer and communication test systems will be in( k2 f/ |: O1 b. u communication with some of the hardware test facilities developed for other BMD$ X( z! \, k* X% }9 Y technology programs.; D8 ]9 S$ s8 l; F; g* q. [$ @) \: E Hardware * n9 I, L' C/ C# X/ T) QSecurity 7 A" N: P( V2 a/ _, ]2 hComputer equipment features or devices used in an ADP system to preclude 0 H) Y8 c' B t: V; T* Kunauthorized access to data or system resources.7 Q3 w5 Z8 Q: y9 G HARM High Speed Anti-Radiation Missile.7 o' I! P) x _1 X0 e _: X2 E MDA GLOSSARY, VER. 4.0 H / \; w. b7 b# Y2 M" E125: s9 {& N" s, ^0 F; S HASC House Armed Services Committee (US).8 a/ T. F0 o% ~4 ?8 f HASP Hardened Ada Signal Processor./ l" l- Q6 M& d- O" P0 \ HATELM High-speed Anti-TEL Missile. 7 @; F/ \" x5 H9 U# X1 i0 ^+ BHATMD High-Altitude Theater Missile Defense. (U.S. Army) ! x( M ~$ s. T- @HAVE STARE Name assigned a proven sensor capability.& `7 i |- j; R( g# |; ~ HAWK Homing All-the-Way Killer. # _. H! P- K, F( aHBCU/MI Historically Black Colleges and Universities/Minority Institutions.. v+ d; b$ Z: N; s6 E3 @ HBHO Hard-body Hand-over [algorithms]. 6 g. X+ s& J: D. \7 _' |HCO High Consequence Option (Safety Engineering term).: H$ b; b( B" ? E, h$ s HCT Mercury Cadmium Telluride. `8 \' o8 s2 @HDA Hybrid Detector Assembly. # J9 ?/ ~+ m. S, z( o$ t4 n* wHDBK Handbook. ' H: {1 Q2 c8 PHDR High Data Rate. % K+ n* f# ~4 u" y. C5 cHDX Half Duplex (TelComm/Computer term). 8 v ?: Y* h, q# kHE (1) High Explosive. (2) High Energy.! _! v. n% T$ K# N Health and Status, g" |% w) }- w8 m (H&S)2 v* F6 C' G r- W- Q9 t* m8 Y Health and Status pertains to a unit’s ability to assess the conditions of its % s( ^6 I% l! ?" C* ^& `7 Usubsystem functions. The term H&S is used for units in remote locations, such + [% ?; @4 j# }2 eas satellites, where ground controls must interface with BITE to determine6 S( ?* [5 l: F5 X6 x% m9 O, u operational status of the satellite and its equipment. + f1 n& P( j" Q5 BHeavy Replicas - F8 ^: @2 Y3 Z" E(HREPS)- c# ~, {1 {& X. g1 O; u. y Decoys, which by virtue of shape, size, and mass, closely approximate an RV’s1 ~, k/ W4 `& i4 B3 ^6 O signature. HREPS have significant off- load penalty. 0 R' g3 I2 g @# F" ~- o& CHEDI OBSOLETE. See High Endoatmospheric Defense Interceptor.6 ]! _6 _+ W4 W8 t HEDR High Endoatmospheric Defense Radar.0 [: \) r/ `9 ?8 J HEDS High Endoatmospheric Defense System. * E2 {: g" ^3 T( NHEI High Endoatmospheric Interceptor. $ }* o$ @2 F$ R0 P1 Y+ p' p: j% VHEL High Energy Laser. 1 @2 C" u9 Y" z1 l8 I. oHELKS High Energy Laser Kill System.$ V d6 {4 a. {6 l( S HELLO High Energy Laser Light Opportunity.8 J) i% x7 p T5 ]% F0 v HELSTF High Energy Laser Systems Test Facility.* [' b3 f; }7 C+ {1 x/ T HELWS High Energy Laser Weapon System.# Q; i. Y) ^# G/ d HEMP High Altitude Electromagnetic Pulse. : C4 o9 R- y4 g; [* m4 W0 iMDA GLOSSARY, VER. 4.0 H & K! j6 s% k' n126' @) i) _ S; ]" s2 G HEMTT Heavy Expanded Mobility Tactical Truck (US Army prime mover). , `1 L3 a9 \: AHen House Soviet area defense radar used as a component of the Moscow ABM system1 g3 L0 V H0 G$ ?: b that provides VHF coverage of space to monitor orbiting satellites and early . |2 p0 t$ o% n: Twarning of ICBMs launched from the U.S.# X% h9 V9 [8 b2 p: V, x HEO See High Earth Orbit. % C- X @: N( r! s, uHERA (1) An improved surrogate TBM test target./ e& e ]) f$ c. U (2) Two-stage, ground launched solid propellant theater target vehicle. (MDA$ R& G( ^. n K Lexicon)! Y+ N3 e$ x7 y+ l0 Q( I& B HERO Hazards of Electromagnetic Radiation to Ordnance (SM-2 Bk IVA). ! k4 r3 C" O! }3 W% e/ F! yHESP High Efficiency Solar Panel. 3 M" S. o4 ^$ l2 LHEU Highly Enriched Uranium.# J; o8 Y9 p- ], d! A$ ] HF (1) High Frequency. (2) Hydrogen fluoride. " p9 }/ v& W# y. bHF/DF (1) High Frequency/Direction Finding. + D7 r* T- V5 ` K3 I0 _+ {. @(2) Hydrogen Fluoride/Deuterium Fluoride. (Chemicals used in IR chemical, E" e5 j" T0 a4 H lasers). ( [* y7 ~! [ J% S9 JHFCNR High Frequency Combat Net Radio. 1 Y' U5 Y* t; ^/ z/ S4 M. wHFE Human Factors Engineering. 9 D* x5 M& O) C5 s5 F* V- F1 CHgCdTe Mercury Cadmium Telluride. 2 x& h! o- o( s0 w9 g" THHB Headquarters and Headquarters Battery. 6 `4 X2 u$ G3 P) Y, a+ aHIBEX High-Acceleration Boost Experiment.% n. z9 k: w3 r) Z5 ^! k v HIBREL High Brightness Relay. $ A1 T2 ?9 p6 J7 ~) w6 a1 IHIC Human-in-Control. / j( N- V, ]8 n9 R2 p5 RHICOM High Command (Navy term). * _: c b; X9 J' Y$ v- z8 eHICTB Human-in-Control Test Bed.5 ~8 i S5 R" t9 t# n% P" w6 z! o9 n HIDACZ High Density Aerospace Control Zone. . d- `4 |$ l3 y& |HIDAR High Data Rate.$ O6 D5 f( t# g, K$ J& c High Earth Orbit 9 ]& `$ t% h- U4 L, N8 \(HEO)) n: G# k; o- ^1 E$ r/ [ An orbit about the earth at an altitude greater than 3,000 nautical miles (about 0 e7 d' ]4 ^# T6 E5,600 kilometers). ; W! J4 e5 `+ ~( m. y) E8 q, PHigh . u# \4 a5 \& EEndoatmosphere9 o; j* m3 x9 M% F7 \5 H That portion of the earth’s atmosphere, generally above 40 km altitude. 9 O! s1 h% D5 X/ v2 j, eHigh ; ? b6 }7 a4 c5 B- |* qEndoatmospheric : J$ x! E/ i$ m3 i5 ~2 G! vDefense 5 E, n; I9 L' r5 u: p: @1 }" DInterceptor (HEDI)6 W* ~; Z# r1 Q8 n OBSOLETE. Interceptor concept designed to engage RVs within the (upper or3 U) ]0 q3 z X: Y/ k high endo) atmosphere. (Predecessor to Endo-Exoatmospheric Interceptor* o$ S/ d- R0 c (E2I).) 7 v0 z7 {/ L' W' JMDA GLOSSARY, VER. 4.0 H4 B2 n" h7 W6 o% E$ N7 }% ~7 U9 P 127 # Y+ y0 Z2 t5 x' [ [2 O! Y! Z5 rHigh Density # J% \# V. f6 P: KAerospace$ ^- L& o/ ] X& f Control Zone C* p% W0 k$ } y7 K' H3 L0 r(HIDACZ) 9 ^2 _ t% b0 B1 ` z' v* y8 ]Airspace designated in an airspace control plan or airspace control order, in 4 A, \7 ]8 F* i$ x2 K9 V' wwhich there is a concentrated employment of various weapons and users. A 7 y4 }& }( r* T( \3 FHIDACZ has defined dimensions, that usually coincide with geographical$ T; W( F, `4 x/ F4 _ features or navigational aides. Access to a HIDACZ is normally controlled by the $ ?' ?' P) Y! i6 omaneuver commander. The maneuver commander can also direct a more - ^% G5 H U; K$ Y5 H) F; Erestrictive weapons status within the HIDACZ. . W; J) r- v' yHigher Authority & x6 X# q( g8 l, l o' wInterface& W9 P0 i+ @: @8 w5 J1 B. z+ V Policy, strategy, doctrine, readiness conditions, and rules of engagement from 6 d0 d: R X1 e0 qhigher authorities for use by the defense system in conducting system7 U0 X3 c, Q9 e( ] operations including specific orders specifying actions such as testing, defense 9 N1 L7 t. a/ ^9 R' c* ienabling, pre-delegation of authority, etc. Also the reporting of situation) @- p! s2 [1 S$ Z/ A! j+ a! }5 i assessment and system readiness to higher authority. ! r; D$ e V/ kHigh Order0 _6 k" C7 t; i. J# U Language (HOL) + D b8 ?; d# B3 Y6 ^: a' pA programming language that requires little knowledge of the computer on which0 J( M# B/ l: f. u3 J% V a program will run, can be translated into several different machine languages,* X& d' [ F; | allows symbolic naming of operations and addresses, provides features , @' U. a3 X2 ?% i' Ydesigned to facilitate expression of data structures and program logic, and : ?8 A5 ~( \2 q) P# ] r1 fusually results in several machine instructions for each program statement.1 F% g- {$ j/ r) C HIL Human In-the-Loop. ! W3 r* Y$ T2 R+ p; i! x$ ~HIMAD High to Medium Altitude Air Defense.0 a3 I) T7 X4 B" h% D0 g7 k8 G& v/ M HIMEZ High Altitude Missile Engagement Zone. & ]0 ~& u- p3 [! DHIP Hot Isostatic Processing.! o5 _5 \0 H, b2 P" a ? HIRAM High Resolution Infrared Auroral Measurements. $ m4 B5 l( |2 i5 b- o' i! yHISEM High Speed Environmental Multi-burst Model.8 ~' q n# t- Q3 ?/ l9 V HIT (1) Heterojuncture Internal Photomissive. (2) Homing Interceptor Technology. % ], z1 x( p+ c" S- L5 f) I) A6 eHK Hard Kill. : h. Y. m- d- G* s# bHKV Hit to Kill Vehicle.8 ^; G& U0 p' v) Z HLD Hardware Description Language. , x) D4 C& F ~) n7 p5 r# C' nHLLV Heavy Lift Launch Vehicle.% D! b H1 b# `% X HMC&M Hazardous Material Control and Management.8 G9 @9 K& L: X2 p HMI Human Machine Interface. V# u5 t. |) f7 ?3 w. H. j& a HMMWV High Mobility Mutli-purpose Whealed Vehicle (USA term) (pronounced Hum Vee). 7 ^5 Y5 k! G E4 h* Z6 ?HMPC Hazardous Maintenance Procedure Code. ( B* X- y1 ~! J$ N4 j/ H; y1 }HMSC Hughes Missile System Corporation. 7 s' L+ O, Q! g) b" jHOB Height of Burst. - q# R' }/ Z/ D0 @HOE OBSOLETE. Homing Overlay Experiment. (Predecessor program to' p! h: B; \5 S2 c Exoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS).) 9 j; l% R l1 o4 P: a# k0 GHOL High Order Language. 2 F3 q% O3 T. A& lMDA GLOSSARY, VER. 4.0 H) X0 P% Y$ |* S6 w7 b 128 9 B( W2 V( X# y }8 P4 O. f. ZHoming All-the-9 o: B& S7 w" n( N& W7 e* C, q Way Killer ' F/ |8 C; _8 V* o(HAWK) & x( n* S9 B! {/ K8 |9 @8 R3 {(1) Upgrades to the HAWK interceptor and radar system to provide the ( P* } A" E) j# U6 ^( cMarine Corps with a mobile point theater ballistic missile defense 3 H: C3 L+ v# ?, tcapability. / k- \6 A& }1 D, f(2) A mobile air defense artillery, surface-to-air missile system that provides % ?: S$ h% B4 Z# r6 [; nnon-nuclear, low to medium altitude air defense coverage for ground 1 `; I$ a8 m$ f5 u$ c" F2 Tforces. Designated as MIM-23. 4 o% {, I: o8 a) SHoming Device A device, mounted on a missile, to aid its guidance to a target. The homing ' Z# ^0 w; t: j. J7 A' f- `! Udevice uses sensors to detect the position of, or to help predict the future 9 w/ J) I2 r" k; Vposition of a target, and then directs the missile to intercept it. The homing 4 u: m# t# T* x# q8 \4 Jdevice usually provides frequent target position updates during the flight of the" U* e( _5 Z0 \ missile. f3 u3 X. v/ Y* h3 h0 y Homing % q( R: \, {' R$ q. p* lGuidance' P4 Q( a/ l' ?9 p! U. q1 K 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# _0 ]4 M1 C7 N4 E the target, such as an infrared signature. 4 e; _7 b/ k2 C; W! y9 aHOMS Homing Overlay Mission Simulation. 6 g& m* ? @ Q+ ?" G9 K. A& P2 GHOST Hardened Optical Sensor Testbed. 5 d w3 F! R: @2 _! [Host Installation A designated DoD facility that provides non peculiar SDS support of SDS# R% L/ _% a, H4 r ? elements.* O$ J( {7 @) m& s$ v. P Hostile 8 ] ]9 o) U0 g* B. v! H7 f' E& Q5 }Environment 6 H2 g+ M' ~0 S; zThose environments that result from a BMD system engagement of an enemy . o2 C# g) h$ N, b ~threat or collateral conditions resulting from deliberate hostilities. Hostile 2 q& f' K) C: E( V5 k. b5 Q! Oenvironment categories currently applicable to National Missile Defense are 7 Y. }1 u0 V; T7 h; @+ y& D1 l$ }& P) nNuclear, Battle Debris, and Electronic Warfare. 3 s: \& `3 |6 r, r6 {Hostile Track The classification assigned to a track that, based upon established criteria, is* j7 c" K, h) _% k/ p- l0 ]. {0 { determined to be an enemy threat. ( m( u# O# W5 W9 D, f0 sHost Interface The interface between a communications processor and a host computer. . O$ R( n" l4 a$ f! n$ ? w" u) nHost Nation( ]+ M' @( @# Q$ b; w( F Support ; i" O8 a! ~% B. ?2 e5 VCivil and/or military assistance rendered by a nation to foreign forces within its k1 E ~. h3 x- A# {territory during peacetime, crisis or emergencies, or war based on agreements% g8 b6 R/ T. _0 K; F concluded between nations.1 Y% x8 j1 ^/ U! H$ P6 t3 [* D" @ hp Horsepower.- x4 }: b4 v# A" k% d: @, p HPA High Power Amplifier.6 h- s; W: z1 q, [- y HPC High Performance Computing. a) d$ m2 N( @ HPCC High Performance Computing and Communications./ y* G7 P& }7 G" N* u HPG Homopolar Generator. : l4 Y4 r, a6 K: @7 LHPI High Power Illuminator (Hawk). 4 N/ X8 I* Q( _& m2 ^: cHPIR High Power Illuminator Radar. 1 L) s+ |9 a" Y7 X) iHPL High Power Laser.$ i( Y7 r0 h; c' Z1 f9 o5 V' h+ a HPM High Power Microwave. # C# A- P- }; J) J* a$ S; B& AHQ Headquarters.: C+ r$ x; U/ n3 y7 C: S MDA GLOSSARY, VER. 4.0 H6 ~! D( U7 H2 g 129 4 N9 L% X. |* Y: \HQMC Headquarters, Marine Corps. 2 Q! J. u6 q! h) K. v7 OHRDS High Resolution Display System. " \; i. d8 x$ B3 tHREPS Heavy Replicas.8 K7 }- e. i4 w. }: e% r HRR High Range Resolution." R; q0 p& u7 c+ H6 ` d HRSA HICTB Requirements, Support and Analysis. 2 n1 K2 n- a' S: e5 A$ ]6 v1 Q; iHSDB High Speed Data Bus (TelComm/Computer term). 4 b1 Z0 @; e/ X6 l- jHSFB High Speed Fleet Broadcast (Navy term).' G! y5 R# U& s% @) c4 l( [ HSI Human Systems Integration. : \1 K- u: I" Z( c: L7 BHSV Huntsville, Alabama. % s3 |& V9 z8 o, oHTICIA High Technology Crime Investigation Association.+ ?* m N$ @0 ^6 U9 y+ A HTI Horizontal Technology Initiative.. s% Q7 E! d% Y7 C, O HTK Hit-to-Kill. # ?2 |0 p* E, U' OHTMIAC High Temperature Materials Information Analysis Center. % x! B9 }9 q, _HTML Hypertext Markup Language.9 Y# k2 x6 Y' T8 N4 K1 j/ t( S HTPB Hydroxy-Terminated Poly Butadiene.3 @0 B2 D& |6 h2 |( C6 \: J# f HTS (1) High Temperature Super-conducting. (2) Hawaii Tracking Station." k* A. `8 V9 d( o( w% C# F HTSA Host Tenant Support Agreement.- e2 ]) q$ g' A HTSS Hardened- sub-miniature Telemetry and Sensor System. F u" ~" V) T5 zHTTP Hypertext Transfer Protocol. a' ?# Y( ^/ a* e6 G; s# _HUD Heads Up Display.: n: z+ h0 A/ a) ]" r Human Factors A body of scientific facts about human characteristics. The term covers all6 l4 @0 |+ F* W8 K biomedical and psychosocial considerations; it includes, but is not limited to, 3 Q' h! @: L) O! T* |5 [# Qprinciples and applications in the areas of human engineering, personnel + H% Y0 _: l3 J. ^# ~1 zselection, training, life support, job performance aids, and human performance ! q* Z2 q) B* c" q' |evaluation.- q& W# _7 |: \- x9 [ Human Factors ; _+ C) R, O% gEngineering( y5 L2 q3 W T$ h/ B, N( f0 `, v The design of man-made devices, systems, and environments to enhance their2 N- I4 h4 K2 p" N* G' _2 K% Z) h use by people. Also called human engineering, human factors, and ergonomics.

使用道具 举报

您需要登录后才可以回帖 登录 | 注册


Archiver|航空论坛 ( 渝ICP备10008336号 )

GMT+8, 2024-6-5 02:13 , Processed in 0.046800 second(s), 9 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部