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 |显示全部楼层
ELPRS Enhanced Position Location Reporting System.0 @- g) V* B' r+ z, Z" R3 g ELS Earth Limb Sensor. o; Q+ l" U& O6 E3 q5 ` ELSEC Electronics Security. # W' _ w B2 g2 H4 ?8 u hELSI Enhanced Longwave Spectrometer Imager. 6 f+ Y; N) }# s6 t" X/ v" QELV Expendable Launch Vehicle.& I* f4 [! [' s4 `( e/ e Emanations 8 y X% p$ o: X7 |+ WSecurity }" t+ S$ f# V7 u6 ^(EMSEC) 7 l9 E& E3 V p/ e2 {0 E: _The protection that results from all measures designed to deny unauthorized$ M% t6 U# o/ W) o+ j persons information of value that might be derived from intercept and analysis of, q6 ]! R+ l! o. b" U0 t compromising emanations. # J) c1 O3 m' W" D7 j0 WEMC (1) Electromagnetic Compatibility. (2) Early Midcourse. 5 p; u, ]0 R G8 [0 y% \EMCON Emission Control ) d- q- P' y0 B r; L/ QEMD Engineering and Manufacturing Development (previously referred to as FSD).; U" Q, p6 r9 @$ b. X0 _1 Q" \ EMDCT Expanded Memory DCT.# Q) B6 K% @) o. o) d1 Y3 ^1 \ EME Electromagnetic Environment. ' v2 s5 A6 X. _. h0 R ?( n& o% h6 |2 eMDA GLOSSARY, VER. 4.0 E+ c. I0 O) q' K9 d$ d+ Y% i 93: N6 l. R' s2 @ Emergency 3 c- y, {0 X* a% z% r3 ?Capability 3 c2 `& l/ ]% Q& Y1 F8 z(replaces / e+ y' `# O. d" d s) K D4 xContingency ' B0 b" f8 O& y, _0 h4 }Capability)+ n9 S: w; a3 K" z BMDS elements or components that are still in development or testing that- u( M( D$ z9 N U provide limited ballistic missile defense capabilities. MDA, working with the' V8 U+ R4 o* R$ h# D2 K Services, will develop plans, which cover the potential use of prototypes and test& m. K, O# J* L+ r% t4 W assets for contingency deployment should the SECDEF determine that an + w! H( X% c: U& o( z demerging BMD threat requires emergency fielding of a BMDS capability. ! z! |8 X4 R+ U6 g2 t X }6 OEMF Electromagnetic Field. # A- M! R1 W; I- k8 o7 mEMG Electromagnetic Gun.3 l4 d- t( H3 u: ~! p, q& D' A EMI Electromagnetic Interference.! X. r/ y6 v$ J' Q) I. G2 k$ {2 K EMIP See Exoatmospheric Midcourse Interceptor Program. $ _5 g2 u4 K0 |3 q @7 r5 _Emission Control `2 S5 m5 c7 g) N L; }(EMCON)6 ]7 e. F( e, m0 i' n& s) v The selective and controlled use of electromagnetic, acoustic, or other emitters 9 Q0 l3 M; A2 @8 Hto optimize command and control capabilities while minimizing: a) detection by & T1 k( y0 A+ T& R8 Q: Qenemy sensors, and b) mutual interference among friendly systems. EMCON 9 T1 M2 p; @& l9 e, P a" P3 Kcan also be involved in military deception plans. Also called EMCON. , m2 Q4 J, a$ P, nEML Electromagnetic Launcher. A device used to launch hypervelocity particles. ! [4 X3 Y5 b5 Q; ~* d" h: O, @) yEMP Electromagnetic Pulse.7 n$ O7 X/ x- M: ~; Z EMPSKD Employment Scheduling (USN term). 9 R) g& R, n2 GEMR Electromagnetic Radiation.+ |/ p- H( _9 J4 F1 ^/ k EMRLD Excimer Moderate Power Raman-Shifted Laser Device. 7 Q& V' n; y0 y3 c5 LEMSEC Emanations Security.9 v4 \. u, Z- F+ Z EMSP Enhanced Modular Signal Processor. / b+ B' e i& a4 V* n9 LEMT Engineering Management Team. ( y" t* a4 @8 N! Y4 z, DEMV Electromagnetic Vulnerability.; X6 L( i7 i6 z ENA Engineering: Architecture and Analysis.+ N+ J. `5 m, L8 l9 a& Y/ R: }/ y3 y ENCATT Engineer CATT (US Army term).5 C5 T% }2 {& L0 [ Enclave Isolated resource – an SDS asset that has lost connectivity with other SDS# _; l, T e. F) q+ G! ]6 @3 e assets with which it normally has connectivity, but is still capable of coordinating ' a% `7 B8 U$ R0 iwith SDS assets to conduct ballistic missile defense. Various combinations of9 ?% ?! L. V* { connectivity losses are possible; for example, (1) an operations center has lost ; W: N& x0 q9 T6 w4 |connectivity with Higher Authority, yet can still provide sufficient C2 and can still ! q4 h: F* u0 `; Wconnect with sufficient weapons and sensors to conduct an engagement and (2) 5 U$ s! H& A2 T3 C, J3 nan operations center has loss of connectivity with another operations center with0 u+ n, _# I: V. I# q0 p. M which it normally shares data, but can still conduct an engagement.1 x( U* S. i; B; ?+ \0 K0 |# I Endgame FOV The field of view of the interceptor’s sensor during its final maneuvers after target1 j9 ]% q$ D2 J" A+ m acquisition to intercept the target. May be less than the acquisition FOV.; k7 z4 {* D/ A: v. o5 ^* | End Item The final production product when assembled, or completed, and ready for2 O% x% i8 p8 T" T, C1 v issue/deployment.6 M5 f8 J' L# s5 g0 G MDA GLOSSARY, VER. 4.0 E ! }& s0 S" t! [$ h5 z94 ( i$ P7 C0 _; {6 c, y3 x( {, sEndoatmospheric Within the earth’s atmosphere; generally considered to be altitudes below 100, d8 ?0 l0 _2 n6 ?' r8 C0 n km. An endoatmospheric interceptor reaches its target within the atmosphere. $ m& y+ N/ e' f% z: PEndo-) }+ c6 C* z5 S Exoatmospheric 0 R u' G6 v- t# Q. }: EInterceptor (E2 I) 3 W5 W. X+ V0 r- P; v. F$ ^A ground-based interceptor capable of engaging RVs either endoatmospheric or ) T" C( y8 l# Q: p7 }. dexoatmospheric. (Successor to High Endoatmospheric Defense Interceptor5 o1 f5 ?$ @& J4 |' M }0 b2 l (HEDI).) 9 z0 i9 F8 t$ ?- |5 [ENDOSIM Endoatmospheric Simulation.+ b# S [! e, c4 i% D: E+ D Endurance The time an aircraft can continue flying, or a ground vehicle or ship can continue * c7 f) k5 @ H1 W4 X" A" ]+ Xoperating, under specified conditions, e.g. without refueling.& ~/ j5 B' \9 H- E" V" t9 Z ENG Engineering.! o1 M ~. B) `6 @: ^! a4 | ENGAG’T Engagement.4 ?+ H' ^- {$ o" c* m$ ~ Engage (1) In air defense, a fire control order used to direct or authorize units and/or ! f! T2 w9 r7 S6 lweapon systems to fire on a designated target. 0 Y2 O% y* f# V' }$ Y+ H% ?) A(2) In air intercept, a code meaning, “Attack designated contact.”" V- M1 L6 L0 s- r1 a B Engagement (1) A period of hostilities beginning when the first ballistic missile target4 j' }9 J. z! k. {8 }8 s undergoes fire from the first defensive weapon. / B) e8 N4 q3 Q% Q2 C(2) A period beginning whenever any hostile object is identified (designated)9 p, N2 }# F0 n9 H. W6 P1 A as hostile and ending after the last hostile object has been attacked. : a, Z0 R2 ^9 @8 G$ W(3) In air defense, an attack with guns or air-to-air missiles by an interceptor , O4 O6 N; f& h# e$ k" g5 jaircraft, or the launch of an air defense missile by air defense artillery and : t1 w/ y* [+ I. S( pthe missile’s subsequent travel to intercept. 5 \8 y9 P( E! w0 F5 vEngagement% o) \3 f9 l8 G2 ^( Y) J- m- I* n Authorization 1 I! a, Y7 X0 g+ cThe authorization given to USSPACECOM to use weapon and sensor systems 8 ~& b. `4 G' X; Q: P) b% ^0 d( Punder previously coordinated and authorized rules, procedures, and conditions. : V- C: {- w& H/ d, c5 qEngagement' `. _& w1 d4 @$ r Control$ q) @: \: O6 M3 I (1) That set of coordination, assessment, decision, and direction functions! d4 m5 L% O# `5 @ normally implemented automatically to execute the selected battle plan,, m& p U/ ] l/ X9 e/ Z+ G% F& [ military strategy and tactics within partitioned battle spaces (i.e., a5 y6 ^; s7 i4 z5 h5 A+ x spatial/functional subdivision of battle management). Includes the ) ^ @3 X( Q3 u$ Odetermination of: what specific objects to intercept in order to implement / X5 R3 i$ E6 b2 U6 S% e+ bthe selected military strategy, and which specific interceptors to assign to . f! G" [; Z! L% |: N t3 {each attacker to implement the selected tactics within the rules of 3 W* k' Y; d2 p/ V; I2 Eengagement. . m1 G E2 I+ H(2) In air defense, that degree of control exercised over the operational) k8 \ n" ` q" Y# E functions of an air defense unit that are related to detection,5 b) H; R9 C8 e identification, 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 |显示全部楼层
Engagement " T' e% l: x5 F$ y& |# wPlanning ! U: X, d/ B# uA set of rules and parameters to be used in developing weapon-target5 P8 V: V |1 {* N; w4 T assignments and for sensor resource management. (USSPACECOM) ; J4 K/ U; X" A! a: N3 A+ ?Engagement , f, |" z( I' d9 `- s( aSurveillance% N& E- A! g3 Z) d The surveillance required to support RV negation in the midcourse tier.' N2 `) t. h; [ Engagement + w5 C3 @! I# W! n! P3 wTime' x3 |/ o# n! O! V' [; l* Y- r5 X The time that a weapon takes while engaging a given target. This includes not9 q1 S" X' ]) L( X3 K. ~4 j only firing at the target but all other necessary weapon functions involved that * Y& ?' k- V" V% k$ R6 G9 Y' |are unique to that particular target. 1 j1 _0 u( I! e: a+ T& [; c3 nMDA GLOSSARY, VER. 4.0 E + |3 }6 O' W. ~" e* X) T! T* e95 1 f6 d/ R, o# V; p3 a8 X/ fEngineering and : ^, U$ }& ?+ B$ yManufacturing Q+ l4 z3 {2 X; r' RDevelopment4 k' M3 S2 \0 f) S* v- Z5 t+ n (EMD) 7 g) Q; J/ e( c" fThe third phase in the acquisition process, following Milestone II. The system 9 [" }% \$ K. G# p$ pand its supporting items are fully developed, engineered, designed, fabricated,& Q$ K7 Z" ^$ J+ g" |. w8 v# G: l5 z tested, and evaluated. The intended output is a pre-production system that ; h( W: K& k1 e) z7 J4 K, Pclosely approximates the final product; the documentation necessary to enter the" k# f% A2 y. B production phase, and the test results demonstrating that the production product H/ J. S2 Q4 W Z. [% Z* Vwill meet stated requirements. $ l' I5 N* ?3 c2 EEngineering3 q( w ?& n0 [* o Change Proposal * I0 n# z4 P X0 }& R1 w- u: x(ECP) 1 \: ]. B5 ?; g8 _4 C4 rA proposal to the responsible authority recommending that a change to an 3 x# ? l9 ^8 R0 q1 ]original item of equipment be considered, and the design or engineering change 3 R5 X2 z0 M, Y5 f. j( }# `" O0 @be incorporated into the article to modify, add to, delete, or supersede original! }% O/ W. h5 v; K- y; x: M+ r a* Q) T parts. / ?# S, c8 [4 G) d/ NEngineering , x) [; }* r; j. D h$ U6 V* IDevelopment( o$ c) S' m4 ` A funding category including those development programs being engineered for* `( z# l c) F( u) s) M service use but which have not yet been approved for procurement or operation.- o3 d- l; j4 p8 ~/ Q% P, k/ j' A5 V Money under budget activity 6.4.% ^9 A& W6 L9 ^1 D5 E0 A Engineering 0 P3 n7 N2 c* H4 @, s2 yDevelopment# O; f% w5 F, n* s! a! v3 ~2 _ Model 4 M' Y/ A/ U0 rEnhanced Target 7 T, ?* `" B' `# j8 c0 g5 g# `Delivery System % X/ T1 i; a3 D8 X" T! _3 i8 E(ETDS) : u+ N0 x: x, A" IAn advanced prototype used during the Engineering and Manufacturing , `$ Y, m0 M+ | R9 V, q( a- |3 lDevelopment phase (EMD) to resolve design deficiencies, demonstrate maturing7 M' T l, A5 b: H0 c% R' D. Q% t performance, and develop proposed production specifications and drawings.: |5 Z B. @6 K, G" c Target delivery system being developed for future GMD testing that will7 | m( b7 |" K) W$ g+ w8 X complement existing systems, provide flexible, modular configurations, and will . a: u$ V& @* Bbe launchable from land, air, or sea modes0 k- f7 J# i( j7 { R6 }0 i ENNK Endoatmospheric Non-Nuclear Kill.+ D! n7 |/ D$ S- L: F5 } ENSCD Enemy Situation and Correlation Division (JFACC term).! ?( e3 [ m1 e3 p3 j; w6 o8 q Environmental " d& \4 O2 f0 HAssessment (EA) : T- g2 L8 i0 L" s% rA concise public document whose primary purpose is to provide sufficient& }& J# Q- N9 W* x analysis of environmental effects of an action to determine whether to prepare( L1 l- E: J7 @ an environmental impact statement or a finding of no significant impact. 3 U& Y9 ]* `+ N7 eEnvironmental & E* U! A! ~5 F8 y7 i; K1 tImpact Statement/ V6 |, H! d3 [4 n (EIS) : n' q! X7 f, }5 s' ?) pA detailed written statement analyzing the environmental effects of a major9 [+ B; |. ^# z8 a% m Federal action. / }% }4 k( n' X8 y! E& c4 z3 {* [Environmental 3 `9 P: ?; @8 C5 _9 Z+ kSecurity% F0 I, J7 @) S1 b: E, U) g) W A specialized form of physical security that prevents technical penetration, e.g., I& R, }5 e9 u) B% s* Openetration by waves of electron beams.# Z# ] m; z) C Environments The media, conditions, and/or physical objects in which a BMD asset is immersed " _' @0 S7 e" H( F# Vor surrounded. For BMD systems and elements, the comprehensive & M' x' m* } e& @environments definition consists of natural, hostile, induced, and storage, 7 ^( G S. n3 i; M1 {0 Dtransportation and handling categories.! w) Z" l: t, V; q7 X3 M; L EO (1) Electro-Optical. u) v# s( x3 V \. i (2) Engagement Operations. 6 G* n" z; @1 c/ ~" M5 l(3) End Office.# x, `% d/ `; I1 u; `6 V! O (4) Eyes Only.& q, j0 [! U7 S EOA Early Operational Assessment. & N- V# }* @- M7 a8 w3 E8 P: fEOB (1) Enemy Order of Battle. / n# ?9 x7 y, E(2) Electronic Order of Battle. 5 Y$ Z! R' M9 ^8 \EOC (1) See Element Operations Center. - K$ s1 t6 x! i( k# h7 K7 Z(2) Emergency Operations Center8 Y r$ j1 S/ ?. M3 E) i& x MDA GLOSSARY, VER. 4.0 E 3 ]3 j' v. U* s; m. X96 " x0 |4 c I) |/ c& I; IEOCM Electro-Optic Countermeasure.( X9 e" Q6 @! y6 z9 s, w: A EOCT Element Operations Center Test Bed. 8 t7 b9 P% [5 j. FEOD Explosive Ordnance Detail & y% [1 |# Y$ c& x) e9 NEO/IR See Electro-Optics Infrared.0 \$ t6 q( p2 ^+ ^' ]7 Z EOM End of Message.4 ~: D8 r0 {- p. o, A EOP Executive Office of the President- X4 r. y# N4 O- C: d% }; ^ EORSAT ELINT Ocean Reconnaissance Satellite (US). % n# L5 C0 r k6 ?EOS Earth Orbiting System (NASA term). , T3 i! `) s- r- \2 U1 w6 D. k: g9 GEOSH Environmental Operational Safety and Health.- j9 U4 K( Y7 [ EP (1) Engagement Planning. (2) Evaluation Plan$ R- U+ F) L9 v( }& s) R EP Cycle Engagement Planner Cycle (NMD BMC2 term). + V$ h8 s( t$ X1 _, D4 {' CEPA Environmental Protection Agency. 0 i8 {( \% ]$ T* _) e- a0 O5 REPD Engineering Product and Development 1 K( c# N* @4 I' f: {1 vEphemeris/ 0 w- N4 M6 F' J4 f: `. |& x9 UEphemerides3 q% ` N3 _6 Z: b (1) A table showing the positions of an object in space at regular intervals of# A# J" L4 C& `2 f9 k* d3 H, W5 _ time.+ \0 c, L" ?1 ^) s (2) A publication giving the computed places of the celestial bodies for each& r+ H! ^1 X8 F6 I day of the year or for other regular intervals.8 Y* P, s2 |: W7 E; k8 D% V& X EPITS Essential Program Information Technology and Systems. # i% L: R0 \" h, bEPL Emitter Parameter Listing (USN term). $ j+ `6 ~& U& o- p( C: kEPLRS Enhanced Position Locator Reporting System. . ~9 r& u) f( H0 s2 oEPO (1) OBSOLETE - ERINT Project Office (US Army term). (2) Element Program + ?6 X$ f9 ?7 e$ |. v1 [Office.0 g: m) ~( S' j1 x& a EPP Electric Power Plant (PATRIOT)./ n( z5 n- s! A; Z: v: s5 b EPROM Electrically Programmable Read-Only Memory. & }: n# E6 O$ Y( M1 W4 ^% K9 pEQEC EurQuantum Electronics Conference (See CLEO).* m0 ]" s5 l6 H$ z+ L/ a; E Equipment I% s9 ~& E- y3 o7 o Operationally : }# J. k: @5 jReady ( i3 A2 f& X7 g% [The status of an item of equipment in the possession of an operating unit that4 h( W8 B# ~/ p indicates it is capable of fulfilling its intended mission and in a system $ j0 _( C9 W( d, z/ c) K/ T# i$ ~: Wconfiguration that offers a high assurance of an effective, reliable, and safe ) e. }, Q! l W( _1 Cperformance. 6 f' N& f: r$ [0 lER (1) Enhanced Radiation (“neutron bomb”). (2) Extended Range. 7 [, Y$ _* F" y) @( ?ERA Explosive Reactive Armor- n, h' A* t3 d: v1 o' e$ {/ q ERADCOM OBSOLETE. Army Electronics Research and Development Command. (Now + Q8 ]! Z/ g2 g8 M0 Z% H3 L0 D' |Laboratory Command (LABCOM), Adelphi, MD.)5 d) w: S# `# q6 M8 m MDA GLOSSARY, VER. 4.0 E , f" ]. T5 v5 ?) G, q: U# h! a97 $ ^ J/ w+ W! NERCS Emergency Rocket Communications System (US). , e: N- T) h& a6 p& O( f+ e( |ERD Element Requirements Document. 1 w2 `$ \9 N1 \+ z3 wERG Executive Review Group.1 e% @( Q0 _+ M1 S* P( t( d; c ERINT OBSOLETE. Extended Range Interceptor. Now referred to as PAC-3.9 J* V) G# e' K5 |" @: s$ c1 g! d ERIS OBSOLETE. Exoatmospheric Reentry Vehicle Interceptor Subsystem. , U1 A9 B0 T' H6 I1 `(Predecessor to Ground-Based Interceptor (GBI).)( B. `# m8 h& f9 T$ s ERIS(F) OBSOLETE. ERIS Farm. & [: @; T1 Q L& DERP Emitted Radiative Power.* T3 W% u+ c7 d- Z. w Y3 h) c ERR (1) Element Requirements Review. (2) Engineering Release Record. + }( Z/ U0 ?5 T1 D9 ]2 b' QERS (1) Early Release of Submunitions. (2) Emergency Response System. * O( U' u8 ~" O4 F$ AESA Electronically Scanned Array. . Q. J2 F5 x7 Z; t1 p" e' TESAD Electronic Safe and Arm Device.! P5 G6 ^3 r! V ESAR Extended Subsequent Application Review.% m( ~$ ^. c0 { w9 B ESC Electronic System Center (AFMC), Hanscom AFB, MA. 7 a- E. Y0 z6 @4 O$ BESCN Existing Systems and Center Notebook. + q, _6 [6 F) G* @ESD OBSOLETE. Electronic Systems Division. (Now Electronic Systems Center,) o. ~) y1 a! B1 d1 h' a Hanscom AFB, MA.) ) h# Z+ u& e6 YESH Environmental, Safety and Health- y4 P- m; x/ n4 p ESI External Systems Integration.7 m4 t, h$ C7 d$ I ESI ICD External Systems Integration Interface Control Document.$ h: r3 x B8 p- H& B4 {7 O ESM (1) Electronic Warfare Support Measures. (2) Electronic Support Measures.7 m7 g& g1 _3 Y6 w! h% ?& W5 R# _ ESMC Eastern Space and Missile Center, Patrick AFB, FL. & @; g) k+ U& d* I" }9 [/ {% ~. ]ESNet Energy Sciences Network. , E) M/ M- X7 {2 s7 xESPRIT European Strategic Program of Research in Information Technology." H' Q1 @3 w/ x& b ]' [ ESQD Explosive Safety Quantity Distance.* g8 g$ T- P3 z" F& ^# L! D2 i5 d ESSM Evolved (Enhanced) Sea Sparrow Missile. " ]7 }! b. h: BET&C Extended Tracking and Control.) L" q; M- A% ], r% d ETA Estimated Time of Arrival.: `4 @' @) E- z1 ?( o9 x) C ETC (1) Electro-Thermal Chemical. (2) Estimated Time-to-Completion.+ p3 V$ z' ?* r) E ETD (1) Estimated Time of Departure. (2) Electronic Transfer Device.% b X& |. |3 t0 o MDA GLOSSARY, VER. 4.0 E- q2 F' V7 ]& h* q+ K8 e( T 98# I* V I/ e2 r# p* E/ | ETERTS End-to-End Real Time Simulator.' ]4 n% E2 l; L0 | ETESD End-to-End Sensor Demonstration. ) B8 g5 U" Z3 E3 \0 I/ [ETI Estimated Time of Intercept. 5 f- t' o! ]! d; P qETIC Estimated Time for Completion. & x' I0 E$ v9 e& I7 p0 L! S. sETM Engineering Test Model $ i# S3 @: N) q0 g7 k6 _ETR (1) Extended Test Range (Pacific Test Bed) (2) See Eastern Test Range. (3)/ P) q# G$ {, n2 W# n7 K9 n$ P Environmental Test Round. (4) Estimated Time to Repair.6 q* c- E9 G# t) T ETS (1) Experimental Test System. (2) Experimental Test Site. ' q' b) t* X+ e- DEU European Union [formerly European Community (ECI)] $ Q% d4 s9 S4 q8 K* q9 t' a, sEUCOM European Command. See USEUCOM. 0 @; g$ q) {0 f* ^! j4 F! AEURATOM European Atomic Energy Agency.: v. h* ^' C' ^ EUREKA European Research and Coordinating Agency.; b. {1 Y2 o$ G3 u EUT Early User Test. E# ], G. d$ }# c) n4 Q& l8 T! a/ OEV Experimental Version! O/ I- H& T# }3 _; R9 D5 a7 L" U% `2 T EVA Extravehicular Activity. 4 Y8 p2 ?& T9 G7 I8 v$ [Evasive MRV A reentry vehicle, which maneuvers for the purpose of evading defensive+ h; p- S- Z+ \! ` R w/ [/ L weapons. $ _1 |' @( X1 Z4 g( a% rEvent Based+ Y1 e7 Z- M9 r: P' W" s Contracting9 \3 |( [4 ^) ~2 s7 [# G Support “event driven acquisition strategy” by linking specific contractual events7 L K1 K; Y6 Z+ ? to the “exit criteria” for the acquisition phase, or to intermediate development' j) x( h9 K6 ^1 I7 H: G events established for the acquisition strategy. / q. ]1 e0 j& C. _" ~Event Driven) ~% ]5 Z$ ~% u2 o- q7 q* { Acquisition/ w/ \. g4 c3 A! y2 Y% d* W Strategy n7 @ Q9 A$ [An acquisition strategy that links program decisions to demonstrated. u% {! b/ K6 O7 M% k accomplishments in development, testing, and production.9 e6 O9 t* s: [2 \ Event Validation A sensor element internal process that results in a determination by the operator3 P0 e' [, G) J/ u8 G# [( { 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 |显示全部楼层
Event % a1 s7 }& v; Y Y' [& N, ^9 pVerification L- V, G. z. S- mThe process by which it is decided, from SDS external data, that the event6 S! x; R) ]9 J# j8 i) D reported is real.: j r6 J7 _4 j# @: y MDA GLOSSARY, VER. 4.0 E* z! q% A, U3 J. `4 B+ D 991 H! w* g( p2 z Evolutionary* L! P5 u* Z: C4 Z Acquisition& p9 o- t" }& X5 l, @6 Z T (1) An approach in which a core capability is fielded, and the system design has ! H+ I5 ~# T! _& na modular structure and provisions for future upgrades and changes as 6 E: o8 B, F) }1 O' Brequirements are refined. An evolutionary acquisition strategy is well suited to 9 t% A4 V5 F ?high technology and software intensive programs where requirements beyond a) z! Y4 L2 q! b' f) K core capability can be generally, but not specifically, be defined. 3 C7 i( X# h% J; T(2) An acquisition strategy that defines, develops, produces or acquires, and2 H2 K( {/ F3 A) H fields an initial hardware or software increment (or block) of operational capability. 8 c) g( r8 j' i p; N$ B- _# P7 n% eIt is based on technologies demonstrated in relevant environments, time-phased. }! F+ E7 ]& G1 J* d requirements, and demonstrated manufacturing or software deployment s* l% x7 x. Z3 u0 n5 b capabilities. These capabilities can be provided in a shorter period of time,. Z0 N( s) e3 m1 b followed by subsequent increments of capability over time that accommodate; d& @' s8 s, b+ X! q" t, |& d improved technology and allowing for full and adaptable systems over time. Each" D$ X% T+ U+ p increment will meet a militarily useful capability specified by the user (i.e., at least+ B5 @# h' c, b the thresholds set by the user for that increment); however, the first increment* |8 G; E" O. a. m9 S" |# ~ may represent only 60% to 80% of the desired final capability. (MDA Lexicon) 2 E- a% U0 w, P% cEvolutionary$ q4 G0 m9 a* x# M Requirements" l' h0 A r) s3 @$ \ Definition4 l- @, T% _% m& n' J Mission needs are first expressed in broad operational capability terms, and then ( F% q: U5 h& Wprogressively evolved to system specific performance requirements. % U5 C9 G& r: p. [: k; pEVPA Experimental Version Performance Assessment. # e- N6 _9 j1 n" bEVPA/TEVS Experimental Version Performance Assessment Test Environment System.2 a6 G- C! M+ L% n. l* K EVS Enhanced Verdin System.9 E3 W" g% R0 X; w EW (1) Electronic Warfare. (2) Early Warning. 0 N* Q Y7 \' M9 y, g6 K0 \EW/AA Early Warning and Attack Assessment. 9 {2 a6 g+ O) e, `. L9 FEWCC Expanded Weapons Control Computer (PATRIOT).4 ^6 O$ A. C/ w p, V3 J- F EWDA Energy and Water Development Appropriations (US).9 T3 n* I* \! Y EWG Event Working Group.& U/ C, d& c2 r! I8 j EWN Early Warning Net.; e8 A/ @& w1 i6 U( i: [1 @ g EWO Electronic Warfare Officer. ; w& }: g7 A( H$ R8 ?EWPE Electronic Warfare Pre-Processing Element.6 }, T4 q( {6 W2 _' o$ {2 b EWR Early Warning Radar.8 A( {( i$ A0 z9 D: |! I! n& p- o" z$ H EWS Early Warning System. ; \ {4 _. A6 [7 K5 c6 X. n1 y, fEXCEDE Electron Accelerator Experiment. % H% ?1 p% T( j7 V4 gExcimer A contraction for “excited dimer”; a type of lasant. A dimer is a molecule% M3 y0 G, |- @2 s1 G* _" O! Z$ k1 \ consisting of two atoms. Some dimers (e.g., xenon chloride and krypton fluoride) , ~& l4 @- V V0 T% H: A _/ j6 ware molecules, which cannot exist under ordinary conditions of approximate- ?( q" S' a) r, o4 J9 S thermal equilibrium but must be created in an “excited” (e.g., energized) condition" M8 d5 d3 X0 Z by special “pumping” processes in a laser. " H0 G3 [4 k) j" Z/ i7 z3 G) y5 EExcimer Laser" ^$ ?: H, G* A7 y8 ~3 I$ h (EXL) & u% d+ F, T0 a. sA laser in which emission is stimulated when a gas is shocked with electrical 2 y9 T/ G C3 Z' ]6 p# O3 @/ b6 w0 \energy and the excited medium emits light when returning to a ground state. ! Z0 c* n! p8 m8 ?/ U' O0 sMDA GLOSSARY, VER. 4.0 E * {( K8 y0 H* m2 B2 o. ~100& O5 r4 y t# x b+ ` EXCOM Executive Committee.4 ]+ ]6 ~0 O: W0 g Executable' b/ ]+ V* W2 f6 ]! G$ B; q n: L Program: N- T9 N- o4 b( t" i A program is executable if the PM has adequate near-term approved funding.$ j" ~0 R# k; T4 }: o Executing Agent The individual within the executing element assigned responsibility for managing 9 q$ A) Y) V) A0 [# s! d! k" t$ oMDA funded programs. * e5 E+ l, u1 A8 X, GExecuting0 ^/ y7 J# M% r/ |# T Elements' ^ A2 t! S/ b9 b8 P% o" S+ Y Agencies or organizations (DoD or non-DoD) that are managing BMD-related( [. `% J; n5 x. v, K7 V programs.8 t* Z8 V. x0 T$ s: S# @ Executing 2 M. h* u w: @/ q$ c' q- qResponsibility+ ~& g1 g i5 y Program Manager responsibility. W1 I: }' w3 g6 x& P/ o0 n Exercise A military maneuver or simulated wartime operation involving planning,- t) G* V% Z: |: r preparation, and execution. It is carried out for the purpose of training and. N4 Y" d) }( l) V) x. x evaluation. It may be a combined, joint, or single-Service exercise, depending 5 E k2 P; Y# t" k, W8 con participating organizations. See also Command Post Exercise. * C" }) ]& H3 p; }+ nExit Criteria Program specific accomplishments that must be satisfactorily demonstrated4 H4 ]% F: m) d% i5 i, l before an effort or program can progress further in the current acquisition phase 5 i. ^3 L9 x) }& eor transition to the next acquisition phase. Exit criteria may include such factors 2 v6 w8 d$ z! q, v G- f, Ias critical test issues, the attainment of projected growth curves and baseline/ w/ K( L; y: U4 J9 N7 _& t parameters, and the results of risk reduction efforts deemed critical to the% ^1 e" j, L! }8 Q- Y( s4 a decision to proceed further. Exit criteria supplement minimum required: h# @! y8 I K' d accomplishments and are specific to each acquisition phase. ; M1 z X4 W) {6 }EXL Excimer Laser.; T; g6 ?4 U) x# m N8 M Exoatmospheric Outside the Earth’s atmosphere; generally considered to be altitudes above 100. L. r* |' b, U& b' D km.: X" l0 g( d: v5 s) m& _: E/ f% D6 _ Exoatmospheric& z* q; n& t* V! m Reentry Vehicle8 X0 O/ M7 Y2 {8 K Interceptor 0 g' g" b0 @1 X j& iSubsystem ' G7 f0 o4 B) A3 i) s* L9 z(ERIS): D$ i5 d+ R; X" r: l" f0 y OBSOLETE. Interceptor designed to provide functional test validation of GBI.3 x A. ?" B- e3 j! R1 f8 h% z$ O Exoatmospheric 1 r/ y, X& w0 D8 ]2 z5 TTest Bed (XTB)2 v& g1 d. F( F5 m) A2 p Flight qualified and range integrated vehicle to support other programs such as / Q8 y: D1 a4 t4 z% u7 dGBI-X. / V$ ]# D, u5 A, R" k- u: K: A( l" G4 iExo Decoy A decoy that matches RV signature exoatmospherically. Exo decoys can use 0 G8 M, A& J. q& R! ?radar and/or optical means to deceive sensors. 3 J5 U) |1 X1 Z3 Q) gExpert Systems Software programs, which use artificial intelligence techniques to capture and w$ Y( b+ }9 @apply the non-algorithmic knowledge and procedures of human experts.1 A! `% {' i( x3 S1 G: R X1 S Expired 8 ?, |; U+ d3 W' y+ yAppropriation5 W5 R7 q s, V( e d An appropriation that is no longer available for new obligation but is still available9 \( H$ r# j& Z: b8 g5 K1 Q for disbursement to liquidate existing obligations. Under current legislation no- Z; [7 m) i1 O disbursement may be recorded or paid after a five-year expiration period. # ^; B6 Z# W) T7 O$ x3 [: ~" B9 s" Z: E2 UMaintains all original accounting identity, e.g. FY, appropriation, PE, etc. " C6 P7 F( i! i. R+ `3 F4 VEXPLAN Exercise Plan.9 X: B& T9 g$ ]' ~6 A Explicit/ Y4 _5 o |# Q( l( d) s- L+ B Coordination6 p% ^, x5 `- X. q' p) b6 t- P A battle management technique which communicates results, decisions or, s3 |$ B. z2 N, p% y1 _( F. C# g command from one battle manager to another, usually from a higher command, {# e9 a7 O, v7 p to a lower command. ) x7 t* ^4 O( V0 o( i ZMDA GLOSSARY, VER. 4.0 E5 u& ^9 Z' e+ s: P( j2 j% ^2 l0 M! U 101* `2 H& ?! t) q5 L$ X( H Extended. b; ?& P. X3 j1 O1 ^* y1 Q Planning Annex9 ^% S& i4 \) Q K( \( v9 Q' G A document providing program guidance for an additional 10 years beyond the * q: @; `' P% O7 N) wPOM.7 U% I+ d3 H |2 G2 V MDA GLOSSARY, VER. 4.0 F 4 `7 {6 u4 n9 g% `% j% X' g1036 L0 B4 _ N( ^* D4 D3 N; I: [% o F (1) Fluoride. (2) Fahrenheit. ! _2 C, r" K! P4 rF/O (1) Fiber Optic. (2) Follow-On.7 l5 a. e2 i6 t+ } FA (1) Field Artillery. (2) Feasibility Assessment. " L1 C/ q- _ `8 w) LFA/RD Functional Analysis/Requirements Definition. , H# E2 w9 |# v8 d, s6 [8 @FAA Federal Aviation Administration. 1 J4 ]' H/ V5 S. dFAAD Forward Area Air Defense (US Army).% V7 q. z* y6 [- _$ Z( F2 S FAAD C2I Forward Area Air Defense Command, Control and Intelligence. + p2 K' T8 K$ G* BFAADS Forward Area Air Defense System (JCS term).0 K+ h) P+ \, f x FAAWC Fleet/Force Anti-Air Warfare Commander./ B9 |* c3 F* U& Y% C, w6 ` FAB Fly Along Probe.: ^+ |: [4 v% H( V/ ^ Fac Facility (MILCON term). ( u; }5 X5 Q9 Y6 b- nFACP Forward Area Control Post (JFACC term). 8 B# C8 c3 u( [& t, @0 vFACSPMF Federal Agency Computer Security Program Manager’s Forum. / S7 `4 S! G0 `: v2 {# TFAD (1) Force Activity Designator. (2) Feasible Test Date. 9 d! n/ b* r2 n' @1 u8 G- CFADEC Full-Authority Electronic Controls.2 ~7 m8 {6 S; w$ @/ w FAFB Falcon AFB, CO. # z3 U. p9 o7 _" T3 x7 e4 QFAFBR Falcon AFB Regulation & R. \% {+ P A& c# J5 A+ cFairing Structure to protect the payload during ascent phase. ; D& q7 K( { S3 fFAIT Fabrication Assembly, Inspection/Integration, and Test.6 X, w6 R7 ]9 [3 d1 c4 f FALCON Fission-Activated Light Concept. o$ v1 O( ]) ]. Y' S FAM Functional Area Management.# h# a- s" b; e FAMIS Financial Accounting Management Information System. / I* {" {+ Y' X9 ~9 X% DFAMP Facilities Acquisition Management Plan. - v3 \" Z$ D: A$ ]8 }FAMSIM Family of Simulations (USA term).# \9 z7 D b. L FAR See Federal Acquisition Regulation.+ |! y1 W9 ^8 c s Far Field The region far from an antenna compared to the dimensions of the antenna and2 S4 n3 C' g: ^' f the wavelength of the radiation.+ ?5 W! W, _/ |( R* e5 d FAS (1) Fly Away Sensor (TCMP). # p- P9 o% M' r6 L2 S% K( \! o/ L(2) Federation of American Scientists. 2 n3 J! Q: Z; E! F& B+ _7 |FAST Facility Allocation Study Team. ; [2 C+ J* s0 g& X, ~3 ~$ |MDA GLOSSARY, VER. 4.0 F % C ~$ [5 l. Y3 s104 8 ?( P) m9 a' rFast-Burn ! T- L h, @% ?, V/ V" g* TBooster (FBB) 0 b2 Q- P% r1 l/ i4 [/ g: sA ballistic missile that burns out much more quickly than current versions, ' f. v: v8 m, z4 v8 |+ Q" bpossibly before exiting the atmosphere entirely. Such rapid burnout complicates" X, @/ ~6 O" X( t* Q a boost-phase defense. , i/ ^2 T$ \) v/ o/ O0 j1 Y; R3 mFAT (1) First Article Testing. (2) Factory Acceptance Test.$ E( |6 |- k9 M0 G+ F3 _: B- f Fault Tolerance The ability of a processor to maintain mission effectiveness after some 9 o7 e0 O" ?* J3 ssubsystems failed.3 a- W9 W7 L/ Z* C' W! Q. b; o Fax Facsimile. - g# M4 O, {7 p7 F" n0 t9 QFBB Fast-Burn Booster. $ w* a, \: l. e) {. s; bFBIS Foreign Broadcast Information Service (US).. t, W' o# R5 f. \$ k) N6 m FBM Fleet Ballistic Missile.8 l. z: {- c$ T; T7 a# g0 [ FBMS Fleet Ballistic Missile System (USN term). ' |( G( E w9 a) r5 u2 `FBP Forward Based Probe. + ?5 p% W. N; P7 P4 R& _0 m; CFBR Forward-Based Radar (US Army term). 5 |* A& a0 q! X; u& T; EFBS Forward-Based System.( s7 Q3 U) n, {7 P4 J: ] FBXR Forward-Based X-band Radar. 8 s% l% T) l" c, l6 g- PFC (1) Fire Control [of weapons]. / Y; w# G+ Q8 s0 s$ _9 e(2) Fund Code. 0 a2 ~7 m: K& T" J7 FFCA Functional Configuration Audit.8 U9 M& e1 M$ N% J v ?* ]: j' i FCC Federal Communications Commission. 3 V$ u: f% M' R, ]* h, ~0 aFCCM Facilities Capital Cost of Money.7 ]: E6 q4 l. I1 w0 |# ` FCN Fully Connected Network./ b5 M" V/ N& K* y ]; I% d FCO Field Change Order. " s# w+ c" m* c& jFCRC OBSOLETE. Federal Contract Research Center. + i+ i4 N( O" U4 oFCS Fire Control Section.

使用道具 举报

Rank: 9Rank: 9Rank: 9

44#
发表于 2008-12-25 20:06:20 |显示全部楼层
FCT Foreign comparative testing. , H0 ~0 H6 r u4 C6 Y# _FD First Deployment. + w( k7 D8 L& IFDA Food and Drug Administration. $ Z0 v$ W; w, }% D4 R2 BFDC Fire [of weapons] Direction Center.% S$ F' B5 B+ x; _; `* q FDG Foreign Disclosure Guide. 8 U* B6 ] C7 p3 E" yFDM Function Description Manual.% V9 i7 B6 y1 k# M; p+ h2 O4 s! f FDO Fee Determining Official.1 {, q- I( b2 b: ^3 V4 w( X MDA GLOSSARY, VER. 4.0 F8 |% w2 \/ b3 Q3 Z 1059 V' S& ^" l+ X0 F) S FDP Flight Demonstration Program. ( b& K( h1 t6 g" S# ?4 I7 NFDR Final/Formal Design Review. 4 q, P8 h) R1 zFDRU Final Design Review Update (MDA PAC term). 6 o, i9 C- d2 F f* J3 t( ?* }FDS (1) Flight Demonstration System. (2) Fault Detection System. 3 Q- M# E* i8 N8 BFDSV Flight Demonstration Space Vehicle. 3 a6 g) [2 g* A5 zFDT&E See Force Development Test and Experimentation (US Army).0 I1 h' c6 O3 Y6 h FDX Full Duplex (Telecomm/Computer term).) M" f: c- O* Q FEA Functional Economic Analysis. 6 g0 @: n' p+ I8 E9 EFeasibility Study A study of the applicability or desirability of any management or procedural : c- w6 d7 W- Y- c8 d6 wsystem from the standpoint of advantages versus disadvantages in any given * l" V- N4 t: Fcase. % s5 M' I! c- k2 s- ^FEBA Forward Edge of the Battle Area. 9 v5 \% r/ t8 M. v3 EFECA Front-End Cost Analysis / e" E% R* V# [! nFED Federal. S) l. g% y0 T& y4 _/ E: J6 B8 Y# ~ FEDAC Federal Computer Acquisition Center.2 m. W. I4 o0 Y4 y Federal+ c: h1 A( D8 k! t9 R0 E, t Acquisition4 w% r9 f# u7 R3 I Regulation 1 @ R% H; P& h; Z3 G# XThe primary regulation for use by federal executive agencies for acquisition of 6 N( \6 e8 W& a, D# usupplies and services with appropriated funds. It directs the defense program8 J7 p- P' ]4 z) ^1 h( M. V manager in many ways, including contract award procedures, acquisition ; o1 k/ N9 j A4 H/ {# N. B: I$ w2 Eplanning, warranties, and establishing guidelines for competition. The Military 5 W( o' D1 f" y2 aDepartments and DoD issue supplements to the FAR. The DoD supplement is * L( F7 b" b, c4 _4 x4 S6 Ycalled DFARS (Defense FAR Supplement). + ^+ Y5 {: ?% ~, T8 B) ^$ XFEDSIM Federal System Integration and Management.1 C0 C" P& W: c0 V: g9 C% p FEL Free Electron Laser.& W4 k6 o' |5 J FEMA Federal Emergency Management Agency.# B5 d4 D$ y1 Z C Fenced Funding An identified aggregation of resources reviewed, approved, and managed as a j' m. {0 n0 T! { n% F6 V distinct entity. The proposed program must be implemented within specified l0 g" a# ?( J* M6 j resources. Examples of fences areas are: Intelligence and Security, Support to + P4 \2 @1 n7 O: O+ bOther Nations. / m7 R: @' `" R7 m! w+ G) OFER Financial Execution Review. 5 E/ g; ^% E3 B$ {FES Facility Engineering Surveillance Plan. ; U( W0 @) m1 f* VFET Field Effect Transistor. 1 F8 S7 J% Q; S) ?FEU Flight Evaluation Unit.: I! f- `% ]) Y7 ~ `2 g- t, _$ \ FEWS Follow-on Early Warning System. : h" v) ~- P$ [FF Fire Finder Radar (US Army." l/ X' O4 }; P7 A' v3 ?; L MDA GLOSSARY, VER. 4.0 F 9 g% r6 n# H. L2 ?/ Q0 Q* g% z106% C$ u+ q) k# e8 v3 { FFBD Functional Flow Block Diagram. ' y- i+ I9 b! j) \FFCD Full, Final and Complete Disclosure (Treaty negotiation term).6 j/ e' @/ s4 h$ a* A& X/ P FFD Fraction Failure Detected. / `8 Q9 D' G* w2 D6 }( T" WFFH Fast Frequency Hopping./ r/ t* G4 N7 T, \ FFP Firm Fixed Price.3 Y! u2 o/ c9 r2 `; u FFRDC Federally Funded Research and Development Center.* N# r6 h0 K5 n+ T5 | FGC Functional Group Code (Navy ILS term). / @3 L- `$ d2 t4 n: HFGEP Fixed Ground Entry Point. $ p8 ^% b# q5 A9 ^0 Q6 NFH Flight Hours. , [: b8 i2 t0 ]1 |1 u0 r! s( GFI Fault Isolation.+ a; q1 `% z! G5 @- O FI&A Fault Isolation and Analysis. [1 J+ Q& _ P' I7 Q, K5 \% r FIDO Fighter Duty Officer (JFACC term). 1 l G1 @0 b$ w7 y8 E) p6 R: h2 gField of View9 p. K9 ~4 s. ]! u (FOV), t7 J. C v% f2 t0 C' k The angular measure of the volume of space within which the system can3 ~# { O% r% u2 N respond to the presence of a target./ O6 ] Z3 @! B$ O0 e+ X) l( w Fighting Mirror 4 }1 k2 [3 X: }8 f$ h(FMIR) ) |2 w& T) D" ?) BPart of the GBL System. The low orbit mirror, which receives laser energy and" b' a$ G6 l/ x7 [ reflects it to the target.! i; G% }) W: Y Figure of Merit 7 U9 f; v c, S3 ~(FOM)* F8 s& A' N2 A/ R) p6 p7 [ The numerical value assigned to a measure of effectiveness, parameters, or ; Q# N6 S8 b) {$ e% vother figure, as a result of an analysis, synthesis, or estimating technique.; Y/ a( m \+ ` i, u4 O: I FIP Federal Information Processing. # O) _2 K s9 |, rFIPS Federal Information Processing Standard. ; ]! |( ^0 q" C) P6 O- C) dFire Control The control of all operations in connection with the application of fire on a target." T' `& Q/ Q- L" h9 b ?3 _# g Fire Control - _+ ]8 F; L1 R, L3 L9 USystem/ W. X4 ^! R& X+ V A group of interrelated fire control equipment and/or instruments designed for 8 q. A/ d6 \5 r% s8 F( Z+ iuse with a weapon or group of weapons.4 w, I5 r2 p& J- W) z/ u Fire Support ! _! b3 r; p8 q8 b9 JCoordinating 3 W2 o9 U3 f2 i4 m. {. |Measure * N* Z- T ^! [+ N) Y/ x eA measure employed by land or amphibious commanders to facilitate the rapid# Y# q p% f6 ^$ H' w engagement of targets and simultaneously safeguard friendly forces. 3 O t2 V; P2 ^Fire Support# g3 V; K% @) J6 d4 a Coordinating Line8 j4 L4 b2 u6 D7 H+ u: a4 [ (FSCL)) |+ `! g! g8 l7 F3 e A line established by the appropriate ground commander to ensure the, K+ ^) h4 s7 J0 R5 T- L4 a7 J coordination of fire not under the commander’s control but may affect current/ r. T0 j* p2 e4 M. P( y# H! ` tactical operations. The fire support coordination line is used to coordinate fires " e4 j$ c7 {9 ? U- _, m# m# Qof air, ground, or sea weapons systems using any type of ammunition against$ i+ I9 l/ L+ F1 } surface targets. The fire support coordination line should follow well-defined 9 E# E# Y. h& B2 W' l4 ~) }terrain features. The establishment of the FSCL must be coordinated with the+ c6 a, N' L/ u) [ appropriate tactical air commander and other supporting elements of the FSCL' S4 w" }4 s3 w( X6 [$ l! n$ Q without prior coordination with the ground force commander provided the attack " N+ e9 ~2 w7 J4 l5 s% Cwill not product adverse effects on or to the rear of the line. Attacks against 9 D) ]0 q/ B, a v- f6 \surface targets behind this line must be coordinated with the appropriate ground9 y4 U( x: E, P( O0 [3 t force commander. n( @" u3 I4 c. |9 CMDA GLOSSARY, VER. 4.0 F 8 h5 D6 c/ a- N6 U- w" k1076 d6 U! Q% l6 _8 Y* v. D0 \ Firing Doctrine The ratio and manner of assigning numbers of interceptors against given / |, ?8 k9 O( Tattackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are9 j" k7 V" B3 p: d9 ~# j3 [ examples of different firing doctrine. The priority of targets being defended and. L$ W8 y0 h8 w- w the number of interceptors available relative to the number of attackers drive( q/ j5 }" g$ X' n8 w4 ?+ F0 _ doctrine./ j h& R- m2 h1 P Firing Rate The number of missiles fired per site per minute.' P4 j" N' y9 U, ~* r5 A6 W FIRMR Federal Information Resources Management Regulation. 4 A7 w m0 |0 {5 [: XFIRST Forum of Incident Response and Security Teams. * K' z- P( m) HFirst Article First article includes pre-production models, initial production samples, test3 T' J3 y) }0 Q samples, first lots, pilot models, and pilot lots. Approval involves testing and6 \; U& p& V8 f, J! f' ?" k evaluating the first article for conformance with specified contract requirements ' j! t, m" q! q4 kbefore or in the initial stage of production under a contract. ! F3 t* Y) b( E/ |; UFirst Strike The first offensive action of a war (generally associated with nuclear operations).: [- L9 w8 Z+ S1 g# M5 t& j9 O First Unit8 b, T( B. D0 s7 `9 [ Equipped Date! i, O. [! V' h( \8 h9 [ The scheduled date an end item and its support elements are issued to the/ s/ Q! K/ E5 h, R initial operational capability unit and training in the new equipment training plan $ h( Q% V# e& B4 d0 E) Q" Thas been accomplished. & w5 U0 L" J& x+ |FIS Facility Installation Standard.' K6 x) p) T5 C9 ]) d Fiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which 0 ?' n- A* K2 ]9 E, Xprovides the fiscal constraints that must be observed by the DoD Components in * ~- l* e2 D; r$ f" A4 y6 ]7 lthe formulation of force structures and the FYDP, and by the OSD in reviewing% n2 c4 Y/ Y [# E+ g proposed programs. , q+ ^2 {, A/ m+ S; Q' eFISSP Federal Information System Support Program. D& ^. o$ f9 _: M5 ]& r% I FIWC Fleet Information Warfare Center (USN term).* b; ~* K+ I' P2 R$ [/ e( b8 K FIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern * E6 ? \' W A$ BExtension). 3 J' p+ E2 \2 WFixed Costs Costs that do not vary with the volume of business, such as property taxes, h9 x! w1 F0 F( ]insurance, depreciation, security, and minimum water and utility fees. $ w9 {8 c& ?4 P; {9 ~Fixed Ground 5 r5 [4 U" o' A0 R) fEntry Point & w7 Q- F6 Q( {( `; U2 T" f(FGEP) % }8 N3 B. n4 ?3 HThe subset of GEPs, which are not transportable. GEPs provide the0 N5 w6 D8 I" V3 g: J [ communications interfaces between the SDS space orbital/sub-orbital elements + X* q3 u7 V2 R' zand the C2E.& y, A$ C! i# D" |. s Fixed Ground8 j+ P: x1 J; y4 F Station 7 g( y! D: |1 I3 w" BAll hardware, software, and facilities located at a fixed ground site necessary to* j( `; M9 ?3 L1 w( D" L% [( g/ q" r receive, process, support, and analyze mission status and data, and disseminate 0 g e/ Y! f. ioperational messages. * Y% i% y. C" yFLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor- e. F! X2 ] T program to Extended Range Interceptor (ERINT).) 4 ^% a( n$ k# XFLC Federal Laboratory Consortium." k) C5 t' A. X# _& s* } MDA GLOSSARY, VER. 4.0 F6 {9 c: G! @5 X5 Y7 b9 }( c 1084 H' E. Y; I Z) a7 A* w Fleet Satellite) C1 Z; b" _5 s4 \! |* C$ B Communications ?" w( A# H, e7 \" i2 N8 X( _ System + ~3 w' g8 o: @* b% t8 l3 p8 C(FLTSATCOM) 4 Z( H7 o" L) a& Q0 E8 mOperating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost8 C" j1 @3 I+ f terminals with simple antennas for use on highly mobile platforms. It has a 4 l, o: x8 H6 prelatively small capacity because of its much lower operating frequency. It . V* I1 l o* Oprovides a satellite communication system for high-priority communication& a) B& j. {3 \2 {4 x; V requirements for the Navy and Air Force that encompasses almost the entire # \6 a T9 z1 _% p& c$ I7 @world. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF7 M; o0 A3 I' U% O- F# | and SHF bands. The Navy has exclusive use of 10 channels for communication 2 Z" b1 U U" } T; F0 N0 v6 uwith its land, sea, and air forces. The Air Force uses 12 others as part of its% V- X% `! _4 r: d AFSATCOM system for command and control of nuclear capable forces. The ' K; r2 I* E1 E. {system has one 500 KHz channel allotted to the national command authorities./ Q' e$ e4 _* K+ T( B Flexible4 I) p( u6 A7 G: s Response 5 \6 M7 d* O' J+ K( _4 ]The capability of military forces for effective reaction to any enemy threat or$ d% G8 G$ W1 G, y/ j attack with actions appropriate and adaptable to the circumstances existing.1 W/ y( Z" U3 m$ @ FLHER Funds and Labor Hours Expenditure Report. 3 n$ I8 n+ o8 G: p: h4 RFlight 8 k4 `) d$ r4 C) F2 N- SDemonstration9 L% ]3 }8 Y) q8 O- [ System (FDS) , l$ [7 X2 c' Q7 t9 TPart of the SBIRS Low Program Definition and Risk Reduction (PDRR) program 6 i1 f4 P" \- p9 c9 _% g0 L1 tphase. The FDS will consist of two satellites and a ground system being built by $ [8 a6 _/ q9 T7 G8 RTRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test( m1 G% h8 x( J: _/ H& D4 }% A$ v program to demonstrate operations and performance of a SBIRS Low concept, : g+ w' X) f# J ]: a, xcollect target and phenomenology data to support the objective system design, . g" r3 A( t& Fand validate cost estimating models. $ S' h+ z! T3 ]! H: {' iFlight Path The line connecting the successive positions occupied, or to be occupied, by an: c0 a7 {- X! l5 L" p aircraft, missile, or space vehicle as it moves through air or space. (It is more( P/ ?$ z- f5 f! ] commonly referred to as trajectory for space vehicles, especially ICBMs.) ; l* B# J& r; C5 O1 Q2 _Flight Readiness & ^5 Q9 h: P3 D( s( S( [, k4 G* SFiring 1 |; J7 q& A, FA missile system test of short duration conducted with the propulsion system3 X8 }9 `- u' I- I* v. g* J! h operating while the missile is secured to the launcher. Such a test is performed & S% R' T( w2 qto determine the readiness of the missile system and launch facilities prior to$ \& Y2 q5 Y0 r flight test. % _9 L, m& @+ F4 m. w: jFlight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching. 6 d) |, `. |" Q2 _5 c8 m: L5 sFlight tests are planned to achieve specific test objectives and gain operational ! W' P, h' `, O# |information.+ A5 ~1 u, K7 d$ i% U Flight Test$ q/ z+ C* c: O# u Vehicle (FTV) ( u- g1 m0 Y' Q& _4 n" @Prototype of airborne or spaceborne hardware used to validate a technology 8 k2 n# h2 p" x- kconcept.

使用道具 举报

Rank: 9Rank: 9Rank: 9

45#
发表于 2008-12-25 20:06:36 |显示全部楼层
FLIR Forward Looking Infrared Radar. 0 K+ Z. y, j+ Q# P. ~FLOT Forward Line of Own Troops. 3 M) ^$ f+ w+ W* @FLT Flight. 6 Y e: A/ [4 g( ]; |1 tFLTSATCOM Fleet Satellite Communications System. - N4 v i" D4 {+ v1 sFluence (or% ~% {7 N* e( h o- u0 b- C+ s Integrated Flux)" j2 e) J# y/ u6 n: @: A The product (or integral) of particle (neutron or photon) flux and time, expressed 5 W x% T9 b5 ~5 O; M; O8 `in units of particles per square centimeter. The absorbed dose of radiation (in) g5 f& c" o, s7 u/ g, @' B rads) is related to the fluence. (It should be specified whether this is incident or / @3 f9 s+ B" F1 X5 Jabsorbed fluence).: e1 Y, Q/ m! P MDA GLOSSARY, VER. 4.0 F" L4 N4 u- B5 f$ W# ~: R# B 109& n3 C* j- x. J; F% R v Flyaway Cost The total cost related to the production of a usable end item of military hardware. $ ]1 k' |1 a& h* A) q% `3 R2 N, UFlyaway cost includes the cost of procuring the basic unit (airframe, hull, chassis,; R/ G- V$ o' z# I2 k etc.), a percentage of basic unit cost for changes allowance, propulsion : ^6 Z T% w( X5 p9 G/ Pequipment, electronics, armament, and other installed government-furnished 8 r5 B- P: c6 Hequipment, and nonrecurring production costs. Flyaway cost equates to& @0 j7 Y8 |' ^" x3 K8 f' ]9 N Rollaway and Sailaway cost.2 }+ A3 T& G- ~' S: j+ `5 r; B: p0 i6 O1 j FM (1) Flare Multiunit. 2 {( I" k p) m- U* k(2) Frequency Modulation.( l; a y' j/ t2 k2 m6 V) M5 p (3) Functional Manger. 2 p2 p/ j" {8 L' m) P(4) Force Module(s).5 y) }9 i3 b8 m8 @- n* B/ i (5) Field Manual.4 O/ F) s+ b6 f% H4 t FMA Foreign Military Acquisition.. w" ?* } ?- }& }6 Z FMB Financial Management Board.7 U1 m8 o8 S8 F/ r) ^: p FMC Flexible Manufacturing Cell. K p! D3 H" _5 tFMEA Failure Modes Effects Analysis (ILS term). ' S p- }7 n. G& WFMECA Failure Modes Effects and Criticality Analysis (ILS term). ) d; o; f/ Y6 FFMIR Fighting Mirror.9 L! b9 f8 K4 n% d2 B FMP Foreign Materiel Program. : q4 ?9 ~: N7 P+ P2 E7 c6 ^FMS (1) Flight Mission Simulator (PATRIOT), Huntsville AL.7 B8 j* O7 H$ h. g5 c4 v (2) Foreign Military Sales. 8 [( B q) ?6 ? ~FMTV Family of Medium Tactical Vehicles (USA term).8 W3 y% S! Z% S/ ` FNC Federal Network Council 1 N9 t; g& }7 ]9 g+ XFO Force Operations (PATRIOT).4 @4 K$ k, K2 c! f% k; b& E FO Link Fiber Optic Link.5 H+ t2 k5 Y6 J: h* ` FOA Future Offensive Aircraft (UK RAF term).7 W8 `- a% r% Q FOB Forward Operations Base.3 o* U% R/ S6 G; B/ o, u9 t5 g FOBS Fractional-Orbital Bombardment System./ L6 X& u% ^7 y FOC Full Operational Capability.6 l. D' Z% _3 O6 G- \/ ?$ J/ K Focal Plane The plane, perpendicular to the optical axis of the lens, in which images of points7 @, y0 w0 Y9 }/ Z* G in the object field of the lens are focused. . ^+ H, o4 E: fFocal Plane 2 }; e4 ?2 X) h/ R* W O9 i. bArray (FPA) : W; M4 d9 A' N2 Q+ h, hAn FPA is a matrix of photon sensitive detectors which, when combined with low 5 X4 P9 B5 w/ H1 w9 G7 f6 W Q2 Knoise preamplifiers, provides image data for the signal frequencies of interest.9 r/ @& r$ Y7 M8 {; ~, s FOFA Follow-On Force Attack." u1 l$ ]' V, b# { FOG Fiber-Optic Gyroscope.6 @* q4 E. S0 ]# q) v4 D, _! K FOIA Freedom of Information Act (US). ( i2 g; h; _$ q, z1 i ?' KMDA GLOSSARY, VER. 4.0 F8 \* B+ |& o1 r) B/ K6 o 110# n8 W) @6 b3 C FOL Forward Operating Location.9 I% L; L7 L8 d FOLAN Fiber Optic Local Area Network./ b N8 k" h6 F3 r5 D% Z Folded Optics Any optical system containing reflecting components for the purpose of reducing ) l4 q% G2 h# r- C$ Y6 n U* `6 r+ rthe physical length of the system or for the purpose of changing the path of the/ V" Y( s9 e5 V& E( | optical axis. z, ]. S. r& E# TFollow-On , v3 r6 r# z* q/ b9 ]Operational Test $ }4 a1 X, P- N$ x# u! `and Evaluation" Y/ _" _: _5 K$ a (FOT&E) & u6 M4 n- k9 Z: ~% WThat test and evaluation that is necessary during and after the production period - t3 h. i. Y5 W# ~4 L6 Kto refine the estimates made during operational test and evaluation, to evaluate, C! T6 a, z! [* ?3 e changes, and to reevaluate the system to ensure that it continues to meet p5 p+ m" A( E, Y- T operational needs and retains its effectiveness in a new environment or against , ~' W( H6 _4 G" sa new threat." T* @" C9 M+ b8 I% b: @9 Z9 z FOM Figure of Merit. ! D! ^2 B3 T. x0 k; K& IFON Fiber Optic Network.3 y5 \3 `1 t9 P2 h+ H9 k Footprint (1) An estimated area of possible reentry or the solid angle of a detector or/ s. a# w6 b' C; W% e linear area of a detector at a certain location. 3 Z1 q% L- O+ x' Y1 f0 ]7 \5 O+ g5 V(2) Geographic area in which a focused satellite downlink can be received. $ L; r# p* y, ?# B9 e9 iFOR Field of Regard.% E7 k3 c% P* s T Force Closure The point in time when a supported commander determines that sufficient( b i1 F# O- U1 R: A! O9 y personnel and equipment are in the assigned area of operations to carry out; G+ l% r2 C1 H# H9 D) F( U assigned tasks. ) w) g+ X) V2 L% Z hForce Development Test and. e9 F6 s8 g# O- P Experimentation0 t2 {! \% E4 E7 K8 | Tests employing representative users to examine definition of materiel : ~1 c2 m# c% A8 J6 t/ _% B6 M7 `requirements or support/assess development of doctrine, training, organization,# e2 z; c6 Q) d and logistics for system acquisition. (U.S. Army).6 W8 i3 }1 @" n9 L* G9 K; j Force Direction The operational management of the forces. 3 @: Y) {# V% \; V' aForce Integration/ b5 ?9 C; ^ _ Staff Officer+ a$ z' O# c1 d" u7 x/ ?7 Z3 P Army individual assigned to ODCSOPS to serve as HQDA user representative for * j4 q! n! h+ d. }a specific system. Provides continuous coordination necessary for integration of 3 [' f2 g' F) R8 _" _" G8 v2 Y/ M5 Qa new system into the Army force structure.* {. C3 p: `/ x: U Force; k o% L/ O. P4 N$ Z9 I& y8 y Management ) g# b9 g( c* y/ V( XThe assessment of the effectiveness of the defense forces throughout an3 r l; n4 R/ M5 e& N2 M( ? engagement and adjustment of tactics and the system configuration as6 v. o' d9 p4 Z: A2 E5 {8 m necessary to effectively allocate resources to satisfy mission objectives. p/ u9 E# {' v4 A( K& g( }6 yForce Reliability The percentage of the missile force that will successfully detonate within 3.5 . A2 b" h, y% |5 a; G& p) K3 fCEPs of the target.. a9 R, X) s. c% S1 D9 f: G9 c6 V FORDTIS Foreign Disclosure Technical Information System.' E) }- K6 I2 E$ `# S Foreign$ b3 l0 K/ V N9 j3 J0 A% s! b Government" ~9 Y' U* {2 J Information7 y3 |* c, S7 }' D9 j Information that is (1) provided to the United States by a foreign government or . w1 _/ {( g2 J) {% T, igovernments, an internal organization of governments, or any element thereof % Z8 N( v ?8 \$ H Bwith the expectation, expressed or implied, that the information, the source of% Z& o8 `4 s& q5 l3 B the information, or both, are to be held in confidence; (2) produced by the United 8 n2 f; |$ S( Y$ w6 E- RStates pursuant to or as a result of a joint arrangement with a foreign % @, T; R& T: A a! B& ogovernment or governments or international organization of governments, b* K, f4 P0 K& c4 q( ] requiring that the information, the arrangement, or both, are to be held in 1 Y U: W. [: {2 c. dconfidence. $ ~; G2 v7 e; V8 u3 ^( _MDA GLOSSARY, VER. 4.0 F& }# }( @5 [/ ~" F* p! k 111 ! z4 ?; g$ K& r! O: bForeign Military + ^! u4 J% T: s" {9 o9 c. `Sales (FMS)( t" }! B/ p2 \' o8 p- N That portion of U.S. security assistance authorized by the Foreign Assistance Act G! _, ~3 o8 F5 @% W7 ]5 Zof 1961, as amended, and the Arms Export Control Act, as amended. The7 U: U% b _, g2 X recipient provides reimbursement for defense articles and services transferred) t7 ]' |7 x; E from the U.S. Includes case sales from stocks (inventories, services, training) by: i# s# l7 ] _; P# F/ G the DoD defense services.+ M# k3 c5 M; v6 w3 I0 ?. O* P Foreign Security+ H& b/ o. U& e0 W2 u) c Policy Model5 G( ?- F" }& S6 n& q$ w8 w) M7 H- { A mathematically precise statement of a security policy. To be adequately ' Y) {: Q G% e2 j% {8 Vprecise, such a model must represent the initial state of a system, the way in ' `6 o/ S+ H N) e9 A' d7 x Mwhich the system progresses from one state to another, and a definition of a" i0 ?" ?0 X* ]- I1 { b. h “secure” state of the system.0 J' J8 K: B! y% k8 [ Form, Fit, and4 R# f8 ^, e' D; B% @ Function Data( Z y+ H1 T# D) S8 \5 e [9 |) X$ B Technical data pertaining to items, components or processes for the purpose of( \ T7 [) C0 I- f0 U! r; M identifying source, size, configuration, mating and attachment characteristics,& s8 H9 h' A) I functional characteristics and performance requirements. % ?/ P" r" E$ ?1 ]& KFormal # p: e2 A6 i- Y0 |; `9 e- D0 k3 gQualification4 k* Z% k8 U: ?1 k- C Review $ A6 n7 ^2 i- q$ n' |, a0 MA systems level configuration audit conducted after system testing is completed ' I2 o: b& i7 Y' Fto ensure that performance requirements have been met. 8 L' |$ Z ^* p" ? CFormerly # w! b0 G a' S4 U0 a. jRestricted Data 1 _6 m8 ~! O @4 r& o" h' J& U: N; hInformation removed from the RESTRICTED DATA category upon joint & S, p) C R$ _( b0 `2 h1 Ldetermination by DoE (or antecedent agencies) and DoD that such information ' m: P% q+ F% trelates primarily to the military utilization of atomic weapons and that such $ n7 ^% w5 C& kinformation can be adequately safeguarded as classified defense information.5 {6 j b- C9 S/ `$ C) o. W FORSCOM U.S. Army Forces Command, Ft. McPherson, GA.* O- Y' c/ p' p. v7 L% y& Z) A% ~ FORTRAN Formula Translation Language.

使用道具 举报

Rank: 9Rank: 9Rank: 9

46#
发表于 2008-12-25 20:06:48 |显示全部楼层
Forward Edge of # e; U8 X; E5 k/ I2 I1 S( Bthe Battle Area# Y- v8 ~/ ]9 e- H/ v( I; v! k (FEBA)* n' |1 ^9 ?% s4 {, m: H The foremost limits of a series of areas in which ground combat units are$ T/ d: h( O' r9 P deployed, excluding the areas in which the covering or screening forces are 7 r. d$ P2 ~- s% m5 S( Eoperating, designated to coordinate fire support, the positioning of forces, or the9 h3 @/ W1 K" ^/ E$ ]0 t: L maneuver of units.5 k+ M, t, d( H- S1 |: f Forward Funding Carry-over of RDT&E funding into second year of appropriations availability. 4 q5 Y3 N! R$ y) V. t; URequires permission from high authority.( F& y" y3 |/ i3 u8 [4 t FOS Family of Systems (TMD). % d. }1 H6 u1 `5 `3 Z Z' YFOSS Fiber-Optic Sensor System.; X2 B5 N' D$ S5 g FOT Follow-On Technologies.# ~3 \8 O- d% B3 _3 e FOT&E Follow-On Test & Evaluation.3 _/ L6 J* k/ L+ C FOTC Force Over-the-horizon Track Coordinator (USN term). 5 Y4 z& b* _# [# C2 CFOUO For Official Use Only./ U! s `/ n9 n Fourth8 c- c8 E+ _) H0 { Generation) z: g: t+ n3 y O7 C$ D Language & Z4 z& r9 {# a) AA programming environment that produces both screen and report utilities for , {" P0 M$ S# q% }5 [5 K# z6 D8 Zuse by lower-level programming environments. . `; u) X) d+ p" RFOV Field of View. / l B/ l6 |: b- WFOV Radar [Full] Field of View Radar " q5 w+ J) A$ M k oFP Focal Plane. + ^+ s& b+ T) l c+ gMDA GLOSSARY, VER. 4.0 F B ]7 ]+ j% [5 \: c 1125 W' B# z* ?0 m, L# G* M FPA Focal Plane Array.! [, w' G5 r6 _. k+ A FPC Facilities Protection Committee. 8 U% R+ C6 f2 m3 E/ \3 W, BFPI Fixed Price Incentive. 3 J$ g5 Y; j7 v3 D& [" GFPS Fixed Radar.' [! p6 P; U4 M2 p3 D0 K+ ?: G FPTOC Force Projection Tactical Operations Center (USA term). 4 r1 U, K' |2 f4 p3 GFQR Formal Qualification Review.& B5 V. G3 K- s6 U" Z: A FQT Formal Qualification Testing. ! C5 W- x% w) m, `FR (1) Federal Register. (2) France.& K' L2 m8 m h, i FRACAS Forward Reaction Altitude Control System.8 Q& U+ W! B4 i FRACS Forward Reaction Altitude Control System.0 j. N4 n% \8 H6 _ Fragmentation ) o! I& v- E' ]+ B7 bWarhead , n0 F# ^6 k- o: C' WA warhead, which releases small solid objects to damage or destroy its targets.% R! I5 I3 s4 a+ _1 t7 X* O4 ` FRAS Free Rocket Anti-Submarine. $ j5 m5 Z* ]2 O6 W1 b0 F: }/ cFRC Fire Control Radar , u, `. l; w# f) k4 rFRD Facilities Requirements Document.1 l2 M `! J! S* ~! O Free Electron8 U# G+ |/ R, d; C6 c( y Laser (FEL) " K/ o* L' h, G% xA type of laser, which generates radiation by the interaction of an electron beam 7 X% W% X! D3 y( a) d: {; fwith a static magnetic or electric field. Loosely speaking, free-electron laser M; a9 o6 c0 B4 s2 k. V0 Itechnology resembles and evolved from that used by particle accelerators (“atom 2 w8 ?- S8 O. A4 p3 g) g9 Z( G3 gsmashers”). Lasers, which are not free electron lasers, are bound electron " g, h2 M) I0 llasers. 5 U. C0 u3 b1 W2 B" d1 ZFree Rocket A rocket not subject to guidance or control in flight. 3 d( G- K, d6 r1 y- o; KFrequency0 ^8 i/ ?( P. Q) @ Management. a: E! @* Q% }! v( n' {' z5 K The act of allocating frequencies, or bandwidths to a telecommunications * K" w) a2 H. U Y3 w" e5 _system, necessary to minimize the potential interference between1 H) p6 k6 `( r( o) Q4 z6 U transmitting/receiving devices. Governing agencies and international agreement3 i f1 A# r0 @. Z& d controls authorized use of a particular frequency, frequencies, or bands. / X+ M2 U" C8 Q5 m$ t: lFRG Federal Republic of Germany. m' S1 _7 U; c% n7 U0 p FRN Force Requirement Number. $ [8 `* Z/ y0 Z+ Q4 j! TFROD Functionally Related Observable Differences. A% B( X. S, }9 H FROG Free Rocket Over Ground.2 [3 \" S6 P& q$ @ FRN Force Requirement Number.- g6 T8 @' r1 |1 r8 ? FRP Full-Rate Production.6 i" n5 @$ A S$ c: w/ S FRS Federal Reserve System.7 q" b X4 O# a1 ` r FS&E Facility Siting and Environment (MILCON term)., c" r/ j. w* g' c. Y$ \ d MDA GLOSSARY, VER. 4.0 F , Z) k) s, O7 ?6 L# Y& ?113 - t4 a) b* K* g$ K7 k9 ^& [4 n# ~FS3 Future Strategic Strategy Study. 9 C% a" f$ L4 B4 jFSAF Future Surface-to-Air [Missile] Family. ' P0 f" K) ?) Q; v6 bFSC (1) Fire Solution Computer. (2) Fire Support Coordination.; b2 G- [1 x( ?' C, l( A FSCATT Fire Support CATT [for Weapons] (US Army term). 4 r! P4 q1 @; t; v, C9 KFSCL Fire Support Coordination Line., L8 H, l% H) y7 y. v% J FSD OBSOLETE. Full Scale Development Phase. See EMD.5 n$ V; N- b" N/ G& k; M" g FSE Fire Support Element.3 b5 {' F( s, R+ ~ X# Y FSM Firmware Support Manual. + N% ?& n( k& vFSP Facility Security Plan.5 J! \4 M; x5 w& E8 A, H- n FSS Fixed Satellite Service." R4 z; M' h) ~* ?9 y FSST Forward Space Support in-Theater. * o# C4 q1 D6 H+ M! x/ G* AFST Flight System Testbed./ m# b/ p2 {5 N( R FSU Former Soviet Union. ' G1 R) H5 \( ZFSU Republics Former Soviet Union Republics.- I& T$ z# E2 t: q C: e: J FT Flight Test. 2 _; ?# x8 W: Q# H* E: J+ S2 E. ?! iFt Foot- {0 W7 r: x. q6 ~4 D2 ] FTC Federal Trade Commission. - E4 P5 i5 V- U4 \; P$ a# _8 Q- wFTD OBSOLETE. Foreign Technology Division (USAF), Wright-Patterson AFB, OH. 5 g- I; l( q" w' T- Y4 Y: @# n, i# iSee NAIC., q i% c8 M7 u$ x+ m7 o FTI Fixed Target Indicator3 @3 v0 ^4 e1 F6 P FTLS Formal Top-Level Specification. 6 m- E, }3 f, y3 P* Q1 lFTP File Transfer Protocol (ADP/Internet term).& M; Y2 ^! E/ U' K FTR Flight Test Round.7 s9 X2 H: U) f2 w FTS (1) Flight Test Summary (2) Federal Telephone Service4 Q: }$ F9 C2 Y FTS 2000 Federal Telecommunications System 2000.; o( D/ s) J' E1 J$ J FTV (1) Functional Technology Validation. (2) Flight Test Vehicle. 5 o) z2 ^6 k& T `FTX Field Training Exercise. 2 G6 k/ e( x7 x$ IFU Fire Unit (PATRIOT). 9 b* H2 ^! [7 ~) X8 kFUE First Unit Equipped.7 h+ S0 p0 O& k2 y, S1 M MDA GLOSSARY, VER. 4.0 F & ]! `6 J$ u3 ?8 |0 {9 a& d) R& `114( B4 G8 R& z4 O* b% q5 R, e Full Mission 5 X l' { ]) q$ O& O. Z, p1 WCapable % D' C( B2 ?7 K7 D/ I% q5 HMaterial condition of an aircraft or training device indicting that it can perform all - I; p. G- t T5 cof its missions. Also called FMC./ l# `& T2 e7 i: P4 @) g1 |% N Full Operational & o1 P$ f5 E6 {Capability (FOC)& n( v, ] @4 X4 }* J# ~3 F The full attainment of the capability to employ effectively a weapon, item of9 J* p1 C0 {) U9 N9 ^ equipment, or system of approved specific characteristics, which is manned and- _. D( g( W! y' ~+ N9 |7 i. [9 _ operated by a trained, equipped, and supported military unit or force. " R( m, j7 O( _1 T; W0 M# X. I4 BFull Rate- g1 D: @! l1 ^' L( X& b0 s+ h* s# ` Production ) R y) R) e2 r) C; V+ U6 @) cProduction of economic quantities following stabilization of the system design8 `. t K' E7 s$ R0 |$ R, t; [ and prove-out of the production process. 5 ^& d4 b! v6 S& ], MFully Configured8 y: I; }/ ^& L End Item 7 M' m; c; f8 Y* CThe final combination of end products, component parts, and/or materials, which 6 s3 Q" J- S) [is fully ready for its intended operational use. Normally all production units are / @. P2 _1 U. A `fully configured. Research and development units may be considered fully " K: `/ f: t2 Q* b/ g+ E. V& qconfigured if they are or are planned to become operationally equivalent to the 3 o1 {2 A4 q6 V- m1 p& P. Jproduction units.

使用道具 举报

Rank: 9Rank: 9Rank: 9

47#
发表于 2008-12-25 20:07:01 |显示全部楼层
Fully Connected ( t6 X( \( U |( V# ANetwork (FCN) : r) d6 ~% e0 h8 r |5 i6 A6 \A network in which each node is directly connected with every other node. ; o% W0 V( s0 D, [# iFunctional 0 U+ B9 I3 R0 f: U7 UAnalysis $ n5 I7 x. o; T( [8 b0 q% GAn approach to the solution of a problem, in which the problem is broken down# ~& X0 |# S. N. D4 C1 n into its component function, such as intelligence, firepower, or mobility. Each ' k. ~& w( k! e Y3 z9 o/ arelevant function is then further analyzed and broken down into smaller 4 y+ M: l$ k5 ?2 U( ], dfunctional components until a level of molecularity suitable for solution of the ! n: U4 W# O+ p6 h, C3 O5 Wproblem is attained.. g8 j/ e: R. j$ y' F Functional ' V- M% g5 R5 l0 M* g4 ^Baseline + R8 w/ k6 B8 B, `# q(1) Established after the system requirements analysis/design activity has$ Z3 a2 u( X; _; w3 @: q, j m# l completed the definition of the system functions and associated data,0 n. L' U( B0 ]% \: T# t4 R/ w interface characteristics, functional characteristics for key configuration7 `) ]4 R; N% C* g, g. N9 A2 H6 p4 v items, and tests required to demonstrate achievement of each specified/ [( P! s/ l' c5 d) S* S2 M P# c characteristic. This Government normally controls the baseline.$ l. D3 A. D7 B) m (2) In configuration management, the initial approved technical 1 @6 `2 l" P$ W, s, f B" W$ b0 wdocumentation for a configuration item. 8 T6 J# A6 S0 F! D& x; I# K(3) Documentation describing a system’s functional characteristics and the $ X6 n' v2 Q3 j# Z+ Uverification required to demonstrate the achievement of requirements. * l. q- a9 t+ W" RFunctional ; H' P! ^; p: w! i! ^# @7 ZConfiguration' ]& E5 ]( ?3 u) ? Audit (FCA) ' X1 c+ L; K) [0 U+ C4 c' DThe formal examination of functional characteristics test data for configuration1 M) J9 c) @1 E3 H6 M! Q item, prior to acceptance, to verify that the item has achieved the performance % } x* B& `% ?specified in its functional or allocated configuration identification.9 [' C7 f; {! e/ W2 ` Functional 9 E: _/ F/ R& mEconomic , a2 {5 K% N' c2 ~4 ~: C0 DAnalysis (FEA) ) ?) O. }, a2 G8 dA structured proposal that serves as the principal part of a decision package for 3 _. B+ y0 J" b$ S+ l- yenterprise leadership. It includes an analysis of functional process needs or* n& c, \' V( n) Q problems; proposed solutions, assumptions, and constraints; alternatives; lifecycle costs; benefits and/or cost analysis; and investment risk analysis. It is ! G' \8 Z3 ~2 z2 O4 c! Cconsistent with, and amplifies, existing DoD economic analysis policy in DoD 5 p6 x4 {7 B% [6 ^/ Q5 _Instruction 7041.3. . l. F3 S% d, iFunctional Kill The destruction of a target by disabling vital components in a way not. H2 q% K! j" k immediately detectable, but which nevertheless prevents the target from- }* q- ^; f8 Q4 E7 z functioning properly. An example is the destruction of electronics in a guidance6 O) T7 Y B% ?7 y$ ]9 E system by a neutral particle beam. Also referred to as “soft kill.”2 I' x9 \0 [; _1 H% |0 Z8 B Functional) m6 N3 D O$ @ Support / p( ~4 x* Q9 j2 a! }2 FSystematized methodologies and procedures, or a common set of standards, ! @0 e9 t* D1 R, q0 Q; Xapplied to materiel acquisition programs. . W% {3 ]2 R3 JFunctional2 t' v; T* J0 B Technology " H& f, E7 v7 n0 o# X5 z/ ]Validation (FTV)" W3 z, a0 P& [9 j4 o' w Program with the intent of proving or disproving a technology is useful for a given7 d' u7 W- p7 O& w application. 8 R+ E( b- p/ RMDA GLOSSARY, VER. 4.0 F% F. n+ L( e. H8 L" d! O# o* \ 1152 g r, i9 v, V Functional # G5 j8 J1 S' d9 P4 qTesting - i' {6 k1 V8 }* K! E. GThe portion of testing in which the advertised features of a system are tested for * L4 q& ]- q# Q2 q6 y x& z- Dcorrect operation. G5 I1 n4 ~3 o# D, Y& tFunding Profile Program funding, usually displayed in columnar spreadsheet format by years, T: _& C' }7 Q% ystarting with previous year through current year and out-years. # Y6 {- x: t O1 c' g6 ]' b0 J% s8 UFuture Years ' |( } |1 W7 y( A- U- Y$ hDefense Program6 k' O! h/ ]7 { (FYDP)1 f: L1 t) j; A" M4 W: F2 o% ?# t The official DoD document that summarizes forces and resources associated with : r) R/ F; C1 V. nprograms approved by the Secretary of Defense. Its three parts are the ' t# Y3 Y' p: U6 [; x# Iorganizations affected, appropriations accounts and the 11 major force programs * C7 P% w0 _$ x* T% |(strategic forces, airlift, R&D, etc.). Under the biennial PPBS cycle, the FYDP is. D, X' Z7 j( B6 j$ O. l6 v2 Z updated in even years in April (POM); October (budget); and then in January+ ?) L! F- n# M6 z( J/ ~: t4 U (President’s budget) of odd years. The primary data element in the FYDP is the 6 ~0 P6 i% b5 O9 c# X. c* YProgram Element (P.E.). Formerly known as the Five Years Defense Program. ' S, _1 d- [$ y! U/ ]FWCA Fixed Wing Combat Aircraft.0 U4 d) @* `- W5 g: O8 E Fwd Forward. + ]. l1 K$ \+ e/ a6 VFXBR Forward-based X-Band Radar.9 H: g! m6 x* A/ M! { FY Fiscal Year. " P$ d# X B* n. E ~) w, DFYDP Future Years Defense Program. 6 E: W& A5 M5 x TMDA GLOSSARY, VER. 4.0 G ) ?5 d4 l" x! {5 i/ Y- Y$ T4 Z' }6 p116 5 u8 T4 E- j* v: I. y9 sG Giga (one thousand million).$ I2 {, v3 M# H- X) N7 ^ g Gram. 1 A" B6 z$ r7 d7 M7 M' [7 D6 KG&A General and Administrative costs.) I3 \4 h4 L7 J5 b& @ G&C Guidance and Control. A2 n: j- O3 ^$ h0 }% C; A. z3 v8 J: E G&O Goals and Objectives.8 W! @: W, n8 }7 i( I! h B G/A Ground-to-Air+ c g$ R( i, c* @! E- [ G/G Ground-to-Ground.: |: b' b; }$ H: F6 q% C GaAs Gallium Arsenide. # V3 y# o Z, g; nGalosh The Soviet Anti-Ballistic Missile system built to defend Moscow from missile 7 ?# G! h# @, R% y9 z6 O+ uattack. 7 J: u: z( f. z1 t! SGamma-Ray Electromagnetic radiation resulting from nuclear transitions. Although incorrect, 3 f2 j, D% N% J4 Shigh-energy radiation, particularly “bremsstrahlung,” is sometimes referred to as$ I2 e, o2 E5 D% z gamma radiation.- w% ]2 `2 |$ o8 c N Gamma-Ray ' u8 S0 [, o0 i; XLaser " t. i7 X: J. z& @# k1 q# vA laser which generates a beam of gamma rays; also called a “graser.” A0 R% m# M! C6 v) i5 \8 P6 E, O gamma-ray laser, if developed, would be a type of x-ray laser; although it would9 P Q9 c. |! c+ Z+ |) h employ nuclear reactions, it need not (but might) employ nuclear fission or fusion , X0 H1 l. p. {) \$ Treactions or explosions. , e I* [2 U+ B4 R% AGAMS GPS (Global Positioning System)-Aided Munitions. - l. y" ~' t1 G9 J7 I+ Z* T% wGaNMPA Gallium Nitride Microwave Power Amplifiers. (A demonstration program to develop4 P8 \$ K* i5 X& _8 J% ^ GaN based transistors and integrated circuits for power amplifiers in systems ' Q/ Q! P7 Y% }' x& L9 E8 G' _such as Ground Based Radar. Goal is to reduce total weight and size by a ! |0 r6 T3 x3 Sfactor of 10). ' J! Y7 I' R* n: i8 L2 @GAO General Accounting Office. . ]( J' X/ g4 p! Q1 RGARDIAN General Area Defense Integrated Anti-missile Laser System. ; J4 p ?. Q/ h7 ^8 ^6 nGAT Government Acceptance Testing.) b# w6 n) Z, }3 G5 }' \1 ?6 c GAT CALL Guidance, Apportionment, and Targeting Call (JFACC term). 5 t+ Z8 j M1 [. B# kGATE Graphic Analysis Tool Environment.+ O* J) D4 Y9 `9 j Gateway An element that contained a node on the SDS backbone network as well as on' {9 m! Q- z+ w, v some other network(s) and would have performed protocol and format 3 ^2 l( j$ ?& W5 l: N) W6 dconversions necessary to accept messages from one network and retransmit S" [4 H1 p9 E x( W& V6 K; Gthem on the other. / l; ?6 g. q% o2 q5 R+ xGATS GPS (Global Positioning System)-Aided Targeting System.4 i( n- g& }1 T: W2 i( ]% j GB (1) Ground-Based. (2) Gigabyte. ~3 l6 v1 u: g( }4 M7 ` GBD Global Burst Detector. . i& H" `0 @4 I/ X* f4 GGBDL Ground-Based Data Link.$ U$ Z' t' @' Z% ^# ~# a. m MDA GLOSSARY, VER. 4.0 G 6 ]. c1 O1 h7 @5 P/ V3 P117 # U0 D$ E. Z2 Q& L8 r3 n \- AGBEV Ground Based Experimental Version.9 Z/ r2 ?4 p; c4 {: J0 } GBFEL Ground-Based Free Electron Laser. * f" L) e4 f( B# X* @0 mGBHE Ground-Based Hypervelocity Gun Experiment. , G6 q" T: j8 e4 i6 |GBHRG Ground-Based Hypervelocity Rail Gun. * c8 h8 ?6 M( i" CGBI OBSOLETE. See Ground-Based Interceptor. 5 M( z- A2 S: \GBI-P Ground-Based Interceptor – Prototype.) _6 J0 b, u& A; m/ {# T/ j4 u GBI-X Ground-Based Interceptor Experiment.* t, R) [2 m6 @( f6 E' ~/ z GBKV Ground-Based Kinetic Kill Vehicle. 3 g- C& P/ { V* N- h- R1 ^GBL Ground-Based Laser. J0 @4 A3 `( F0 {' `9 Y0 f2 fGBLD Ground-Based Launcher Demonstration. 3 e& C( Z0 [ h5 |GBLRS Ground-Based Laser Repeater Station." `# J+ l, E% Z+ l GBM Global Battle Managers. * s5 Q* H2 z8 x TGBMD Global Ballistic Missile Defense. ! }( ]0 _2 P! M# _GBMI Ground-Based Midcourse Interceptor. . P' @+ w! }: g) ]% ?GBOS Ground-Based Optical System.! m! Q' L& F0 `2 P. t0 D GBPST Ground-Based Passive Signal Tracking. ' n5 k3 f) M& T/ y7 hGBR See Ground-Based Radar.+ Z/ E ]& C; v7 G0 N) @ GBR-M Ground-Based Radar-Midcourse. 5 C8 @" n/ Y6 j* A2 lGBR-O Ground-Based Radar-Objective.( A" J, D0 G; V0 B+ a/ X3 g GBR-P Ground-Based Radar-Prototype. * X- h9 [* @+ B$ V' @5 @GBRT Ground-Based Radar Terminal.3 c/ [: j$ h( X GBR-X The experimental version of the GBR.* ?' M& d) g; J& w9 X GBRF Ground-Based Radio Frequency.

使用道具 举报

Rank: 9Rank: 9Rank: 9

48#
发表于 2008-12-25 20:07:14 |显示全部楼层
GBRI Ground-Based Rocket Interceptor.7 M, H9 E2 t$ ?" M3 h; H6 h GBRT Ground-Based Radar Terminal. 8 j3 ^2 q% _$ s& N: KGBS Ground-Based Sensor.3 s, W; v+ s8 X GCA (1) Guidance, Control, and Avionics. (2) Guidance, Control, and Airframe.3 u# m2 ?( \( u GCC Ground Component Commander (JFACC term).2 ?4 H8 [, U) h GCCS Global Command and Control System.0 `' |/ f" b7 N MDA GLOSSARY, VER. 4.0 G! } |, `; q% _/ { 1189 L! e u( E; Y% |: p/ _ GCI Ground Control Intercept. , S- g% n1 h7 o5 e6 s6 g: I# _8 \GCN Ground Communications Network.% P! H$ Y) W1 q' h* N4 U) q GCS Ground Control Station. . B) ]8 y( p' ~3 O0 g3 g* W+ OGD General Dynamics.; O( w, }5 d/ Z1 L( l, S6 K) o GDL Gas Dynamic Laser.- M' r, W& z- ~- P( M GEDI Ground-Based Electromagnetically-Launched Defensive Impactors.$ w4 N( |% L" U) [* G GEM Guidance Enhancement Missile (PATRIOT).5 [7 t* b8 s4 G) l+ v; N* f5 F General Manager & ]0 j$ A0 W' w( @" O% jProgram . h) y8 Y, j0 p9 t! G' [6 A# QManagement; i0 j& \: o7 R1 M* @3 N Directive (GPMD) 9 Z0 v" O. J. c0 q( ]OBSOLETE. The primary document used by the GM to direct the Service BMD4 u B1 T& q! p, r PEO on the specific actions necessary to fulfill BMD program requirements.6 B/ D" L' R4 y/ w# b1 L0 A) q3 f General 2 g! h3 D" W) }Specifications 3 u* b" [# l1 V# d6 }* u9 GA general specification covers requirements common to two or more types,7 j. X4 Z- I4 W4 T5 @! O' Q classes, grades, or styles of products, services or materials; this avoids the ' p1 |7 x( {5 z prepetition of common requirements in detail specifications. It also permits ( ^4 e( C% G0 N, Cchanges to common requirements to be readily affected. General specifications9 C5 j' a' Z6 ~5 ?5 `% R/ m may also be used to cover common requirements for weapons systems and, h5 Q/ _5 Q1 q2 x5 t3 ^5 x subsystems. 4 P% S+ p1 B& _( z0 zGeneric Rest of 7 C/ |8 T) S( P# Y3 Q2 |: t: VWorld Target ' ~, G2 C0 }1 c- o, f(GROW) 6 Y. P1 r. j* ?/ qStrategic target being developed for GMD program./ k4 D4 j7 X* R3 H3 q. P$ J GEO Geo-synchronous Earth Orbit. & ~( P" o$ F* e( }GEODSS Ground-based Electro-Optical Deep Space Surveillance System. ! n! M& n4 e! g; j, |Geo-stationary. X' h1 M8 Y; M6 d Orbit (GSO) * f# `6 Y h$ [* y8 c$ wAn orbit 35,784 km above the equator. A satellite placed in such an orbit - ~& y" X, A' a% `( G$ a$ K/ M7 L" Brevolves around the earth once per day, maintaining the same position relative) r2 l5 D, _4 H3 }* W to the surface of the earth. It appears to be stationary, and is useful as a2 h8 p z& Q; d; @0 {$ w communications relay or as a surveillance post., F% f9 _" q' I* s GEP OBSOLETE. Ground Entry Point. IFICS.0 o6 k# z* t6 l GES Ground Engineering System. U2 u6 N( N' c( JGFE Government Furnished Equipment. See Government Furnished Property.$ e0 Y9 a2 @+ M! n+ j c4 `: T GFI Government Furnished Information.! h- I7 W) N" a& ?8 U! E GFM Government Furnished Material. ! P7 {1 H, P% L1 l1 q$ \$ o5 D5 OGFM/P Government Furnished Material and Property. See Government Furnished1 q4 }, o) e# M3 N! j* D Property.+ f/ F/ D9 ]9 T( s( s. @/ O9 x GFP Government Furnished Property." w: H! b! K# z5 }9 p5 o5 ` GFS Government Furnished Software. See Government Furnished Property. 0 ~4 U, a: ?4 p% {) {8 R! p9 P! g. cMDA GLOSSARY, VER. 4.0 G' x! U4 m/ K* T( W, H8 G 119( s" [- T- n& z Ghosting This condition occurs when two or more targets reside close to the same plane . }. i/ C3 T4 z, h3 e$ Halso containing two sensors viewing the targets so they are within experimental) F5 H2 c: A! b2 J) j+ ? r4 V determination of having the same hinge angle F. Thus, ghosting depends on 4 n. C; H' B2 ^+ h( `' rLOS error and positions.- b; p* o8 G9 t9 r {: I# J GHz Giga Hertz (1 x 10(9) Hz)." s! u7 d# r5 k GIDEP Government/Industry Data Exchange Program. 7 c8 @: ^. R, v3 Q. S( k9 FGIF Generic Interface.' Z2 z+ c$ O5 j5 M5 K GII Global Information Infrastructure.+ ~! T; ~2 R3 ^: B, a/ ` GIP Ground Impact Point.& a) Y, X; e& Y9 E GIS Geographic Information System.8 o2 [3 `2 D+ x/ V- P GITIS Government Integrated Technical Information System. # V) N6 J' k! I k, PGLCM Ground-Launched Cruise Missile.+ W: A# X/ ~8 C6 K4 G" a/ `. x J GLP Ground Launched Probe. See Brilliant Eyes Probe. % p) u1 T, j( C1 h7 D& wGlobal) K) r6 x7 }2 H. F+ @ Environment & K( v, M; c2 P w5 _The ISTC Global Environment is responsible for the creation, propagation, and 7 I2 z4 e. w$ N# g: ~1 Jmaintenance of test scenario common knowledge, how subsets of this, v2 b; @. \' i: h+ Q& F3 S. V6 j information will be determined, and how common knowledge will be disseminated. u/ H% q5 q0 f to the various element representations (nodes). The Global Environment ' J) z1 a; @5 R; `, V8 dperforms functions which are common to the scenario such as timing, health,; \' b9 h* M' w M g" g status, state vectors of objects, and effects models. & S, ~3 ^" L) N, pGlobal* C# d* p- x& r/ v! ]1 C; m Positioning1 h. c8 V# d# R+ V System (GPS) ' G! F/ r1 u% d! B6 Z) B$ g- g" fThe NAVSTAR Global Positioning System is a space-based radio navigation h7 Q! I3 u* c& w network providing precise positioning and navigation needs of all the military & y5 H% C f( A) X) w$ f3 xservices. In the fully operational configuration, there will be 18 satellites in six# d1 v0 y+ T/ A- ?, o" U orbital planes with an orbit period of 12 hours at 10,900 nautical miles altitude.5 [: Y. @" @7 ^1 |6 c2 p! c W Each satellite transmits three L-band, pseudo-random noise-coded signals, one: a; ]; @4 o A/ j. M S-band, and one ultra high frequency for spacecraft-to-spacecraft data relay. / _% Q" `7 w. t- b; ~9 t/ lGlobal Protection $ y8 H. |0 r1 J) r. V# iAgainst Limited( F H5 {+ P* G9 D8 q* r Strikes (GPALS)* g' f2 M7 t f% s7 S OBSOLETE. GPALS was an architecture denoting an anti-missile system - l! P& }- C4 p2 B8 X5 G4 ldesigned to provide protection against limited ballistic missile strikes, be they! S& D( z* [) t' _ deliberate, accidental or unauthorized—whatever their source. GPALS was2 q6 D% W9 m; T; D: X composed of three interrelated segments: (1) theater ballistic missile defenses,0 L) @3 b* {1 C0 G4 D and associated space-based sensors, to protect U.S. forces deployed abroad,2 T. `5 U. q. I; L+ D0 ~% f( s& c! ~ and our friends and allies; (2) ground-based defenses, with space sensors, to 5 Z( y1 V' x$ X2 }$ t) i2 wprotect the entire United States against long-range ballistic missiles; and (3)' s* a1 i4 @# ]" P1 g: @4 ~ interceptors based in space – Brilliant Pebbles – capable of providing ! T [+ F) G. A% Icontinuous, global coverage by intercepting enemy ballistic missiles with ranges* E- t4 z r8 n" q% f d greater than several hundred miles. : p& z( y+ C7 S, k6 U) g/ [Global Protection* L+ j- ?0 E8 G( ~ Against Limited : u+ Q3 s- c( \* {% g% c% dStrikes (GPALS) , h" k9 M) e7 M! d1 |Program6 q( J& s j5 W7 @ OBSOLETE. The GPALS Program consisted of six Major Defense Acquisition 7 F v( X5 i% O7 g) _3 o, ZPrograms: GPALS System/BMC 35 e, t- A7 {* L) X: q- | , National Missile Defense (NMD), Global Missile8 D* D A) H% R+ a4 G. d2 U Defense (GMD), Upper Tier Theater Missile Defense (UTTMD), Corps SAM, and ! I2 n6 o' e8 t# R7 w& _4 c: vPATRIOT. Army PEO GPALS was re-designated PEO Missile Defenses in 1992. " S: T4 p: q. B* oGLOBIXS Global Information Exchange System. / `' R" V3 m+ k9 CGLONASS Global Navigational Satellite System.) R; H5 z: C& w- _2 y6 K MDA GLOSSARY, VER. 4.0 G. i+ V0 Y4 p( u) T) D* h& _. Z 1205 n! p D6 P' Q* C GLOW Gross Lift-Off Weight.6 T8 t+ l* G( R0 D% T GLP Ground Launched Probe. See Brilliant Eyes Probe.' Q$ N ^3 _9 O. w0 e GLS Ground-Launched Sensor.1 q- p1 [$ Z. c GM (1) Guided missile. (2) General Manager.+ _3 O4 E5 @2 N8 c# K8 @ GMACC Ground Mobile Alternate Command Center.. R; [8 A& E2 L. g p: c* _ GMAOC Ground Mobile Alternate Operations Center.3 `8 Q0 Z/ m, m( Q' T GMCC Ground Mobile Command Center. & M, K3 P* r) V, l1 YGMCP Ground Mobile Command Post. ' n" K( Y9 @2 FGMD (1) Ground-based Midcourse Defense (formally National Missile Defense) (2) ( @6 K6 N) r; IGlobal Missile Defense (OBSOLETE).5 a- x5 S) f8 x! W8 e6 W GMT Greenwich Mean Time.( h" u: k( R! w3 X3 r5 G GMTT&C Ground Mobile Tracking, Telemetry, and Control.; Y) I2 w- n6 x2 ]' ]- J GN&C Guidance, Navigation, and Control.% t& `# |* k5 B( N V* Y+ k GNC&P Guidance, Navigation, Control and Propulsion. L8 R5 o- i* q- X) s9 S+ ~' X8 ZGND Ground.: w) i( } W' D- }: k GOCO Government Owned, Contractor Operated. 4 X# x/ T# Z% ]+ K1 W K$ q" aGOES Geo-stationary Operational Environmental Satellite.4 [! B1 G- K8 n( L0 } GOI Government of Israel.4 t$ P T8 j7 T+ X/ i B; O GOJ Government of Japan.

使用道具 举报

Rank: 9Rank: 9Rank: 9

49#
发表于 2008-12-25 20:07:26 |显示全部楼层
GOSG General Officer Steering Group.7 M k F& O; F* V2 v0 R* @ GOSIP Government Open Systems Interconnect Profile (CALS term). / y8 q$ W/ F% E- {- `" WGOSP Government Open System Protocol (CALS term). 1 o$ z9 R- a7 w/ q6 L% A7 T6 lGOTS Government Off-the-Shelf. , z7 ~. h; V3 K e+ lGov’t Government.. t3 H! V h6 x Government3 ]% z+ r: O! b& _) D Furnished7 y" I" B8 l1 x) n; W1 } Property: Q3 C* L& h4 Z; e) Q Property in the possession of, or directly acquired by, the Government and+ Y, z5 M( O0 c; c subsequently made available to the contractor. (See FAR 45.101.)/ C6 Y2 ^# f9 M2 ~) X" c" i Government - ~; _$ U' w+ A" ?% m+ xVerification : S; H! S9 `% H, WManagement 8 r) G0 F8 U" z5 J0 m& ^/ IPlan (GVMP)' H- _; f0 }" s6 i A management document that provides the overall framework for BMDS , I2 L* V; }) F7 ?/ t* kverification. It includes processes for implementation, organizational " ^" r2 E/ q/ }* prelationships, and stakeholder responsibilities. It covers the full scope of BMDS ) g8 C4 q$ h, d: D1 jverification and identifies how all BMDS verification activities will come together to 9 c3 E& n& Q4 U) tconfirm BMDS capability. # ]* s( L- x% `* x# m2 VMDA GLOSSARY, VER. 4.0 G7 }( O! a7 h& Q1 v/ ~ 121 / \+ C% [# i5 ]# {7 l; j fGP Group." B6 o6 p' p( q' Y, P2 I GPALS Global Protection Against Limited Strikes.( @4 L, @! I: e$ |; d7 ?. x+ D GPC Global Protection Center. 1 \! @4 M" n0 \ Q# oGPMD General Manager Program Management Directive. 6 X/ }/ k E$ w& i5 h/ J8 e3 XGPO Government Printing Office (US). " v# v2 r* e1 X) K* ?GPP General Purpose Processor.% U+ t6 }; |$ ]8 u: c GPS (1) Global Positioning System. (2), Global Protection System. 7 g; R8 P B8 M( ?) zGPSIU GPS Interface Unit. $ r1 |9 R7 t* C: L( {% mGPU Guidance Processor Unit (US Army term). * i+ n0 D* h E1 f6 ~/ }: \4 hGraceful9 X1 o% c; L; u% e Degradation# ?9 J2 l( |7 s( y& d) `1 H2 v A condition in which a system continues to operate, providing service in a - C9 `. v ~0 p I; H9 adegraded mode rather than failing completely or catastrophically.: A+ g1 E3 J) f- I; l: z GRASER Gamma-Ray Amplification by Stimulated Emission of Radiation. (See Gamma- : E6 F7 k5 R2 Y; ~( ]1 N; K; ORay Laser.)2 i! a3 N! }1 x+ u0 y: r5 S GRC General Research Corporation.7 d$ \& y9 h9 h- A2 J( ?3 n5 v8 } Green Code Interface Software.# i- H) m! Z$ X1 L4 Q: x Ground-Based0 u9 g: T5 j8 D/ k& ^ Defense ) n1 m+ R2 h4 ]& J& bThe ground-based sensor and weapon systems of BMD.3 j& ], O% \7 o# f. ~/ E Ground-Based + E2 f9 N- U9 h3 FInterceptor (GBI) 0 D5 f3 X7 C) S* S2 c, n- O5 n- YA kinetic energy exoatmospheric interceptor with long flyout range to provide, ?0 b, L. m0 x! S* E2 m! I0 s where possible, a multiple engagement capability for defense of the U.S. with a# l8 T; K) Y8 X% O8 m0 X4 @5 i& B. r7 U relatively small number of missile launch locations. It is designed to engage) P Z8 }; b2 M/ ` post-boost vehicles and/or RVs in the midcourse phase of flight.( L4 a+ L6 j; X A+ l# Z (USSPACECOM) (Successor to Exoatmospheric Reentry Vehicle Interceptor 4 P }# U4 Z' [; [Subsystem (ERIS).) See EKV. 2 H3 D5 S/ S: Z' i4 E7 zGround-Based* g" X8 K( O$ m7 o' D, r( f0 ^ Interceptor* j+ ]' V2 Q# W( Q" } Experiment - ~! n5 s" m8 q$ G7 w! j(GBI-X). q0 ?9 x% t. u1 @; P; c* ^$ \ Designed to infuse advanced technology and promote competitive environment 3 u: U3 w8 k, ]! i5 |for GBI.8 [0 C6 T2 u; ]& Q( M( }* a Ground-Based$ w' j- n9 X' Q: a, @, _' K Radar (GBR)3 g, H( U, @$ `4 N: T* J A task-able, modular, multi-function, phased-array radar that provides , F* F& J8 h. n) zsurveillance, tracking and engagement planning data in post-boost, midcourse, 6 ?# z" |6 E# _7 Z U# Mand terminal flight phases within its capabilities. It also provides target% B% c% }7 ?# z5 A0 R discrimination, in-flight target updates (IFTUs), and target object maps (TOMs) to * X& D5 ?( ~' [: f( Z4 E3 w$ Einterceptor vehicles. See THAAD. (USSPACECOM) A' o: r1 \# E) g/ y4 W Ground-Based 4 |" h" h; o" H+ j# FRadar Terminal $ f, G4 I, [& t1 l9 E+ |; d2 ^(GBRT) u( b, i9 q) e | The sensor for the NMD system. An X-band, ground-based, phased array radar + f. q. K2 `% Jcapable of detecting, tracking, and providing discrimination information to a3 q8 h; i# ^# g5 T8 h& V1 ^' ^ ground-based interceptor. 7 B0 F# K4 s$ U" \9 HGround-based) x7 ~( U3 _7 U( S l Surveillance and8 N6 a& ^8 e" M# u7 I Tracking System # u( `2 H* L- A+ E% m& R8 Q, N(GSTS)* j- G; ?* k9 v. O }* K. S, n$ g A fast-response rocket-launched sensor, which can support the SDS midcourse . Q9 Q7 |2 l5 P* M5 p* Nsensor suite by employing multiple Long Wavelength Infrared (LWIR) wavebands# q6 j7 U) q( F% ^' \/ A and a visible waveband sensor to provide tracking and discrimination of/ v! A3 D: r H potentially lethal targets. : n, Y$ P) x8 f0 T0 X; Y3 c6 R& OMDA GLOSSARY, VER. 4.0 G6 a+ g4 b, C3 U# u1 x4 j5 F" k 1225 w, [ z$ U$ i% S5 R7 [2 } Ground Entry/ h) J! I! ?; C! l: g: p Point (GEP) 4 V& k% U1 E9 Z4 O5 d3 J: ~1 nOBSOLETE. GEPs provide the communications interfaces between the SDS 0 D2 f# O( q) l' tspace orbital/sub-orbital elements and the C2 E. See IFICS. 5 A8 b1 m' S# C& QGround Mobile9 a5 S# b$ a& @3 \ Regional' H+ z' ?, K/ y7 g: [+ O& i Operations) L: K, s* z7 L8 R Center1 f9 h7 K0 ]! S (GMROC)) m! ^& ^0 F! P( G# A Transportable ground segment of the Regional Operations Center. ' C! R" Z a$ Z9 |$ {3 ?( d3 mGround Zero The point on the surface of the earth at, or vertically below or above, the center - u2 z1 L. N9 G3 i7 j: yof a planned or actual nuclear detonation. * N& } k6 y& \( M3 mGS Garrison Support (US Army term). $ }! [0 _8 ]: r: z" K% p0 bGSA General Services Administration (US).0 W5 V! V3 ?) g! u8 b GSDC Ground Station Demonstration Lab.% X9 @" i: k- c GSE (1) Ground Support Equipment. (2) Government Support Equipment.! S6 Q* M0 A9 @9 j GSFC Goddard Space Flight Center, Greenbelt, MD. b& h, [" R5 v! b/ f, ^GSII Government Services Information Infrastructure. / `6 |3 k' v( u4 ?9 H" j" JGSM Ground Station Module.' z. R. J8 W7 |/ u GSO Geo-stationary Orbit. # ?% Z# z4 m. ~' B: P) k+ m5 L. j" EGSR Ground Station Radar. 9 A* l& v: d; X* r% SGSTS OBSOLETE. A fast-response, rocket-launched, Long Wavelength Infrared 7 ?& d7 j {/ x5 A9 I/ ]) u) _: y(LWIR) and visible waveband sensor, which would have enhanced the , c. D9 Q+ j# N- a/ ~, v0 |information available from the SDS’ midcourse sensor suite by providing tracking9 M: h+ T$ p( v, z; m+ ?6 I and discrimination data on potentially lethal targets.* U; D# D# f7 h; {, v GSTS (F) GSTS Farm.6 ?$ n7 r* j$ q& V' f- V+ S0 |3 J& c- N GTA Ground Test Accelerator.0 ~% ]6 g, f2 K: L( K; a GTACS Ground Theater Air Control System. 2 ^+ P! E8 i. l: A5 E6 lGTE GTE Corporation. 8 |. a& l, F) N9 q! {& y' FGTF Guided Test Flights. x! ^, r8 l' \$ WGTM Global Track Manager. 5 j' |% o/ O1 [& r+ w$ lGTN General Technical Note.+ Q/ I' d y! S" ] GTR Gulf Test Range, Eglin AFB, FL. 8 b3 J9 ^) |1 d5 {. EGTSF Guidance Test and Simulation Facility (PATRIOT), Huntsville, AL. 4 t5 b& n; v9 }" q* M; KGTV Guided Test Vehicle. , t" S; i9 e' q! A7 \GUI Graphic User Interface. ! w) Q) k) ?. o7 F! M* rMDA GLOSSARY, VER. 4.0 G " p( ^" Q5 v/ r$ v6 c123 * u9 y* Z6 v( F. G! \7 RGuidance (1) Direction, altitude control, and navigation (where appropriate) of sensors 3 z1 ~0 V- Z& ]) W: ?. O5 z9 L" Mor interceptor vehicles. 1 E+ V: n% V! r7 Q# V$ [(2) The entire process by which target intelligence information received by a8 _5 u2 B4 d, j4 L! I, Y% h! z6 y, @ guided missile is used to effect proper flight control to cause timely3 A$ r! ?; R2 D N4 Y& |9 `. I i direction changes for effective target interception. ( |+ v) ~: f1 D4 Q5 z, DGuidance . a0 k+ e5 C% N& l" VEnhanced " T# w( [) K2 E7 q) e6 E/ m. R" EMissile (GEM) / T+ n2 n+ r: f3 q' H) _. tA companion program to PATRIOT PAC-2, which includes enhancements to the . f. W( |1 L( Dradar to increase intercept range and performance. $ E& Y u) _. D: Y- y2 l( QGuidance . x6 ?9 c" I, HSystem (Missile). Q5 A$ C9 d1 ]0 @ A system, which evaluates flight information, correlates it with target data, * D; _, S* X; U' D$ Mdetermines the desired flight path of the missile, and communicates the # q' w/ [% v7 J" H o# onecessary commands to the missile flight control system. 8 C! i: `1 H5 D$ G. C$ ?0 oGuided Missile An unmanned vehicle moving above the surface of the earth, whose trajectory or+ c/ I( M; E0 Y/ r# D flight path is capable of being altered by an external or internal mechanism. \, Z0 q7 T& U, [4 lGVSC Generic VHSIC (Very High Speed Integrated Circuit) Spaceborne Computer.0 Z/ |$ l$ \' P2 O& T/ W$ I GWAPS Gulf War Air Power Survey, 1994 [a DoD-sponsored survey].& J3 B7 ]6 t& c- t/ N( A8 p/ w$ i( D Gwd Giga watt-days.1 n, q$ ]% i7 ?4 o& H GWEN Ground Wave Emergency Network. 8 z& r& A' [- T8 K/ [8 D3 VGZ Ground Zero. 6 L9 N' {6 j3 xMDA GLOSSARY, VER. 4.0 H , |4 s% Z5 L' v4 f- j0 r, x& n* s124 # P) E/ U0 M% eH Hour.9 i c3 t" W/ x3 ?* a6 v H&S Health and Status. " g6 c( y5 ?5 L1 PH/W Hardware.2 R9 m1 F) T) _! f, ` HA Higher Authority.& Q. z; e$ w! L HABE High Altitude Balloon Experiment. 1 z9 q9 u( D; s9 t: V3 b+ _9 sHAC House Appropriations Committee (US).; B' m/ W8 n! {3 T$ a HADS High Altitude Defense System.; ]; u, q: D( a2 g" X HALE High Altitude Long-Endurance. $ k' P$ s# r. W( i. YHALE UAV High Altitude Long Endurance Unmanned Aerial Vehicle. ; o/ ^% t& [" ]& P3 THalf-Value . r# k7 A4 Z$ G9 g- ]; m* L4 n* kThickness (HVT) {9 _7 }" ~3 H. _( @The thickness of a given material, which will absorb half the gamma radiation- ?/ c g& n9 A incident upon it. This thickness is inversely proportional to its density and also$ ~" a$ O% X' m( ` depends on the energy of the gamma rays. & C' D! o( t; r$ i3 b! C) X/ sHALO II High Altitude Observatory II & }8 \; f1 a5 C: IHAMS Hardness Assurance, Maintenance and Surveillance. - M" k# d/ w0 w3 s9 @. Q, R" Y' Y K9 mHandoff This occurs when information on positions, velocities and tracks are given by one ! R) f( {$ u4 n# hsensor or system to another and the first sensor or system continues to track the . t {' U! ^" w5 m" V& |' Xobjects.- |9 u8 I6 h$ a& H Handover This occurs when information is passed on to another sensor or system in which: c, @* j. Y; c the first does not continue to track.+ g9 P# N$ p. i, D8 e4 l. M( F 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 |显示全部楼层
HAOIS High Altitude Optical Imaging System. 3 m2 z4 T. t2 \: W# E( d, ^HAP High Altitude Probe.4 a7 F2 ] Y9 D: J3 g! S Hard Kill (HK) Destruction of a target in such a way as to produce unambiguous visible# G8 b3 s7 v' _ evidence of its neutralization. 4 r7 v# L) k J' i$ ZHardening Design and manufacturing process and other measures, which may be employed # {4 F) k4 l' f' B0 _% ^8 nto render military assets less vulnerable. 1 o6 R0 Y9 }/ eHARDMAN Hardware/Military Manpower Integration (Navy ILS term).2 `# F% V. t$ R) U Hardness A property of a target; measured by the power needed per unit area to destroy4 c) ]5 B7 w3 h& C- i the target. A hard target is more difficult to kill than a soft target. 3 o2 Z4 z i9 @. _Hardware-in-the-1 [, W% [7 @2 C2 u Loop (HWIL); ?( w7 `$ [5 E Tests in which BM/C3 computer and communication test systems will be in0 z0 c1 `# I. G7 R% K. F communication with some of the hardware test facilities developed for other BMD ' G8 Z% L: C( `technology programs.1 ]2 Y4 _) `. S Hardware2 \# C& b- j7 J' k+ I, ^9 f- \ Security e) y8 L- i% I7 U. ]) {Computer equipment features or devices used in an ADP system to preclude5 ?- p. r1 l( ]! G2 s0 ~- U7 r- o unauthorized access to data or system resources. 5 d5 l8 S6 @1 `+ x) PHARM High Speed Anti-Radiation Missile.; B% [4 p4 n& B' H- P D) P MDA GLOSSARY, VER. 4.0 H % x% R' P; k% \9 i8 u125 % U/ [: T9 ?) N! C3 ]. n6 iHASC House Armed Services Committee (US). ; O9 S8 ?- @& L0 R, v# P8 n+ vHASP Hardened Ada Signal Processor.! s) I! n# [; k. X HATELM High-speed Anti-TEL Missile.# c9 p* ?& w* L% _& L HATMD High-Altitude Theater Missile Defense. (U.S. Army) # Q' D5 N9 g" a+ tHAVE STARE Name assigned a proven sensor capability. 2 e9 ^1 A U. e2 o' PHAWK Homing All-the-Way Killer. 6 u( R4 E4 }+ x+ I `HBCU/MI Historically Black Colleges and Universities/Minority Institutions. % Z9 m' t1 L/ l7 H qHBHO Hard-body Hand-over [algorithms]. * t; L! T; I: C, }5 v0 v3 E- UHCO High Consequence Option (Safety Engineering term). 5 e; Z7 T9 ?; Y6 z; P: N. G+ j' THCT Mercury Cadmium Telluride. 6 z5 z6 ?" |7 w& T oHDA Hybrid Detector Assembly.7 v0 A) h( J: u2 B" ~9 y, i7 s+ u HDBK Handbook.. P; |0 g6 V" a( y# X' W HDR High Data Rate.9 n: ?: Y% O+ [2 I9 b8 m HDX Half Duplex (TelComm/Computer term).2 {8 j4 C. S3 ?. Z HE (1) High Explosive. (2) High Energy. 3 d+ S" X/ J \. KHealth and Status $ W2 t1 B9 j3 H/ H" {2 C- a(H&S) ! B! V' V7 ~# }) SHealth and Status pertains to a unit’s ability to assess the conditions of its9 K% O0 r7 A1 P7 ?. | subsystem functions. The term H&S is used for units in remote locations, such ; A; g# s" b: c: Q+ cas satellites, where ground controls must interface with BITE to determine' F: ]. t1 q1 x+ w d& J6 t operational status of the satellite and its equipment.7 y2 G! t6 a/ N" w$ L Heavy Replicas* V: V, `7 T3 G' j( J (HREPS)0 F: k7 x0 R0 ?7 A4 F0 X) P. ^ Decoys, which by virtue of shape, size, and mass, closely approximate an RV’s" _- |9 F8 I+ q( h( F% [9 J% Z signature. HREPS have significant off- load penalty./ ]/ x" _9 W6 P$ C; V8 V HEDI OBSOLETE. See High Endoatmospheric Defense Interceptor.: d' a$ v- C, o$ n6 N; } HEDR High Endoatmospheric Defense Radar. 2 g/ }. W! \5 {9 {9 wHEDS High Endoatmospheric Defense System. ! R+ g. O# ~) U# N# bHEI High Endoatmospheric Interceptor.9 ?) ^6 u( u; j3 o HEL High Energy Laser. & Z8 A( R6 n, d6 ~9 w: p% H2 ^5 a3 _HELKS High Energy Laser Kill System.) ^( a) A$ O9 h! u3 R" F1 S HELLO High Energy Laser Light Opportunity.+ o% x6 p9 j" R# t9 s HELSTF High Energy Laser Systems Test Facility. ) C# T+ U7 |, k* z: CHELWS High Energy Laser Weapon System. 7 G$ t; R0 ?. aHEMP High Altitude Electromagnetic Pulse. u' T0 A0 {3 E MDA GLOSSARY, VER. 4.0 H' {7 q+ E8 C9 G( B5 A1 G, `! ~* ~ 126- K3 H, `* D. b0 R, [ HEMTT Heavy Expanded Mobility Tactical Truck (US Army prime mover). ! w3 F& _3 \" [3 IHen House Soviet area defense radar used as a component of the Moscow ABM system q) R0 b8 b% Uthat provides VHF coverage of space to monitor orbiting satellites and early " V% b! @6 Y: T! o& Gwarning of ICBMs launched from the U.S. ' j. L* g% M% X9 `/ ], iHEO See High Earth Orbit. % F" J3 i/ H. gHERA (1) An improved surrogate TBM test target. 8 p/ G- D; D: q* X) j* ~- f3 J(2) Two-stage, ground launched solid propellant theater target vehicle. (MDA J3 }# |! j. A4 j Lexicon)6 u% j- s- v8 u3 L HERO Hazards of Electromagnetic Radiation to Ordnance (SM-2 Bk IVA).; O- W; l5 d6 l' [8 ~ HESP High Efficiency Solar Panel. 0 F3 L) V q, }# [, y0 P" A7 J2 L6 jHEU Highly Enriched Uranium.) ^; P3 X3 D4 ?9 U4 I3 w HF (1) High Frequency. (2) Hydrogen fluoride.4 o0 A5 }2 _. N1 P% m6 k HF/DF (1) High Frequency/Direction Finding. & s1 g- \8 k$ V) }# j. N3 @+ }# B(2) Hydrogen Fluoride/Deuterium Fluoride. (Chemicals used in IR chemical 6 b( m7 k' R4 A4 @) b7 t6 H! ]lasers). : e* S: p8 P' J1 `& q$ R% D. @6 SHFCNR High Frequency Combat Net Radio. % a0 m/ e* p& ~& `9 BHFE Human Factors Engineering. ! Z9 a! K4 [& `8 VHgCdTe Mercury Cadmium Telluride. 7 v( y; R! ]( yHHB Headquarters and Headquarters Battery.7 j8 Y: o, S. O+ L HIBEX High-Acceleration Boost Experiment. w* S1 U5 f8 j P2 P HIBREL High Brightness Relay. 2 {7 G1 P' v6 `6 Q( CHIC Human-in-Control. 4 p2 m5 h4 b L. g3 g$ dHICOM High Command (Navy term).% a, g) p: _' x+ l" c HICTB Human-in-Control Test Bed." U5 } f R) i- ]+ C2 x7 M+ K* Y HIDACZ High Density Aerospace Control Zone. # `2 ~. l) k7 }6 UHIDAR High Data Rate.( V& `0 I$ ]% i High Earth Orbit 4 ~$ B) s( s2 Y" h5 _' Y(HEO) ; c" W, U' s0 t8 z7 ^9 E- g' jAn orbit about the earth at an altitude greater than 3,000 nautical miles (about " I8 T& ?; s- w- f( e+ _. b5,600 kilometers)., E2 R0 f9 R5 B6 ~ High / p; f% F6 x4 i* N2 I" A6 K! lEndoatmosphere; |/ M/ y3 ` D3 C* P1 a z6 H That portion of the earth’s atmosphere, generally above 40 km altitude. / {; M. n$ b3 ?% OHigh( y6 H2 A; T4 l2 `% N Endoatmospheric 9 D& `, D( H' E) sDefense! D/ ~. j1 l* t3 G+ ^1 }. Y( n Interceptor (HEDI) # z7 _+ F# r* Y2 ?( a' WOBSOLETE. Interceptor concept designed to engage RVs within the (upper or0 j4 l1 ~9 O- b0 A6 g, C# B high endo) atmosphere. (Predecessor to Endo-Exoatmospheric Interceptor$ U j0 b4 L ]% a) s (E2I).)# M' @0 u* o; N# Z7 e MDA GLOSSARY, VER. 4.0 H* Z/ [ y/ f# C4 [# r L0 v8 y 127 % @; P: \/ H& `. C" X' wHigh Density V) o. ~ T; c; ?# rAerospace9 X! O6 t; r6 q* M& { Control Zone9 K! L" s5 ~+ F3 E- B3 t (HIDACZ)/ Z0 f+ Y, s% T: a Airspace designated in an airspace control plan or airspace control order, in: w' [+ G0 M/ c6 n$ e which there is a concentrated employment of various weapons and users. A% o+ @% l2 ?1 \- z! m HIDACZ has defined dimensions, that usually coincide with geographical$ i! s/ x8 @$ k( w! n o7 L) i& E features or navigational aides. Access to a HIDACZ is normally controlled by the9 H- }9 }3 v; a4 N6 l) I maneuver commander. The maneuver commander can also direct a more8 O5 h' Z6 m, Q. t# s- E' V) j8 c restrictive weapons status within the HIDACZ.. X- V- T; y8 H& N- T# b" F4 G Higher Authority " u; |6 L, q. U3 T8 S, m- x$ sInterface ) X h6 X% s7 v J+ A! v4 rPolicy, strategy, doctrine, readiness conditions, and rules of engagement from( Q$ T0 r/ a: d0 _8 k6 K9 T, L. T# y higher authorities for use by the defense system in conducting system" L, H4 F5 ^" {5 ^" R5 i operations including specific orders specifying actions such as testing, defense 6 ^& u5 K+ Y4 B; J- [' B- Benabling, pre-delegation of authority, etc. Also the reporting of situation% v8 H; `. u; n% m$ ] assessment and system readiness to higher authority.: |8 ^/ n% p Y. {; V- n High Order& n! U% S1 N0 j9 ?7 k6 m Language (HOL) ; K: p9 _6 \9 M4 b0 r4 @A programming language that requires little knowledge of the computer on which% e5 f& b# r- M/ }% t5 r/ _ a program will run, can be translated into several different machine languages, # w4 i* z! Y4 {) s" A1 B f$ Uallows symbolic naming of operations and addresses, provides features7 T6 o/ T4 E1 ?* k4 @$ Z! U designed to facilitate expression of data structures and program logic, and6 c+ v; d- F5 c* A usually results in several machine instructions for each program statement.0 Y* i2 h9 [2 I9 w2 u/ p: z- G HIL Human In-the-Loop. . U% W- g- h ^0 n6 y; l' x( pHIMAD High to Medium Altitude Air Defense.3 _) } Q N/ E6 I2 q, f% g HIMEZ High Altitude Missile Engagement Zone.6 ~5 k7 B1 f8 y0 P HIP Hot Isostatic Processing.! c, ~& q) `/ u3 O HIRAM High Resolution Infrared Auroral Measurements. & }0 G8 @, [' e) g6 Z- eHISEM High Speed Environmental Multi-burst Model. : D. f) |$ L9 x! N! n, x) cHIT (1) Heterojuncture Internal Photomissive. (2) Homing Interceptor Technology. 0 F8 \, R9 x( g3 r9 r, VHK Hard Kill.' w0 N. m0 G- {, {. [) t3 W( `7 r HKV Hit to Kill Vehicle. ' }8 ~2 i( A8 G2 qHLD Hardware Description Language. % \3 m9 p# C5 W$ o. H* |* mHLLV Heavy Lift Launch Vehicle. , h, Q$ N1 ^. j2 w; mHMC&M Hazardous Material Control and Management.& t+ ]# z+ s9 h* V HMI Human Machine Interface.+ p+ [; v7 m/ |) S6 {$ k7 m: X" x HMMWV High Mobility Mutli-purpose Whealed Vehicle (USA term) (pronounced Hum Vee).( e! P% O! w4 `1 u% [$ V0 C HMPC Hazardous Maintenance Procedure Code.3 Y- f. ^4 f% p1 z* j0 Y HMSC Hughes Missile System Corporation. : \ a( R( o4 n$ ^! VHOB Height of Burst. 9 R9 R# ~% L$ B7 w- bHOE OBSOLETE. Homing Overlay Experiment. (Predecessor program to & f- `/ @0 a: }Exoatmospheric Reentry Vehicle Interceptor Subsystem (ERIS).) 1 S, }* @+ u9 e) e3 u9 eHOL High Order Language. 8 D |8 X" i( `2 E9 l3 E, CMDA GLOSSARY, VER. 4.0 H ! X: v- ?* @9 r1 y- A, ?4 _128 , p/ @( S& R. i9 E$ H& M- nHoming All-the- . N$ i7 y) t9 b3 {1 k, sWay Killer3 E* D. ^! x W: F (HAWK). R' m7 d3 G U: Y; N" F (1) Upgrades to the HAWK interceptor and radar system to provide the$ X1 g$ X. y0 A5 f7 ? Marine Corps with a mobile point theater ballistic missile defense8 u! c+ R7 V' Z9 b capability. & ]# W" |5 B" {' g(2) A mobile air defense artillery, surface-to-air missile system that provides* K. g; H- ?3 F non-nuclear, low to medium altitude air defense coverage for ground# C9 f! U( g7 P2 Y4 I; ]7 @ forces. Designated as MIM-23.5 p6 H r* S( i; x7 X" z Homing Device A device, mounted on a missile, to aid its guidance to a target. The homing/ N# x% b% A7 z device uses sensors to detect the position of, or to help predict the future 0 r6 Y% L4 P/ X$ gposition of a target, and then directs the missile to intercept it. The homing 0 o& B# n' w0 y A4 o3 W1 d# ]device usually provides frequent target position updates during the flight of the3 H, Z6 T. j! V' G9 h8 E missile. 7 u! q. i5 i+ x! T6 ]/ P) BHoming; E ?% @: X! q0 h0 G$ n1 r$ Z: u$ c Guidance * F7 H* m5 |2 A7 G8 X. hA system by which a missile steers itself towards a target by means of a selfcontained mechanism which is activated by some distinguishing characteristics of 9 _, z$ J' D z% G2 zthe target, such as an infrared signature.: e' I f. r3 Z) D/ z; x2 e HOMS Homing Overlay Mission Simulation. ) |! Q. J+ _ v* u2 JHOST Hardened Optical Sensor Testbed. 4 j% S7 d! p& w! m' N8 rHost Installation A designated DoD facility that provides non peculiar SDS support of SDS8 O2 w! T% w ~: {, F( U* p elements. 1 H" m- ]; D3 ~! B, B) PHostile , z# N" k3 C6 H" x1 G% }Environment' O' Q; H7 x7 {& K* b Those environments that result from a BMD system engagement of an enemy . p3 j9 h6 U4 _! P* w- U$ |threat or collateral conditions resulting from deliberate hostilities. Hostile / v, ?- G( z( Wenvironment categories currently applicable to National Missile Defense are ) N5 k( d4 {: w4 u u( U& N6 a% xNuclear, Battle Debris, and Electronic Warfare. 8 A/ a7 E( \0 _7 NHostile Track The classification assigned to a track that, based upon established criteria, is( u/ ]# g9 J# E7 p# J G determined to be an enemy threat. % [1 i: j/ S" e7 W- z& pHost Interface The interface between a communications processor and a host computer. % V; h" i/ L2 h1 PHost Nation 9 y* `; m) S) J2 B6 _Support 0 |) p6 n0 M6 k+ j$ r$ ?% eCivil and/or military assistance rendered by a nation to foreign forces within its . |$ ?& v4 l" R& }: N6 p0 N* l3 Rterritory during peacetime, crisis or emergencies, or war based on agreements5 L7 [: w* R E) ]7 w+ l7 v* D2 Z% h concluded between nations.: V% a' g- m" z8 M4 s/ j' y N/ L/ f hp Horsepower.; E5 r: n+ L+ A! {2 G HPA High Power Amplifier.9 J% w2 p0 G# a$ r HPC High Performance Computing. 9 G+ p* e+ c$ b) [HPCC High Performance Computing and Communications. , Z: @2 p0 n3 T- s9 zHPG Homopolar Generator.- d G' W' n" } S HPI High Power Illuminator (Hawk). 1 J6 P" m# X' U$ Q% O# {- ?HPIR High Power Illuminator Radar. / [8 r0 x W3 M: v5 y6 ^HPL High Power Laser. 4 Y) [! s: y$ m: j0 bHPM High Power Microwave./ m- t) h5 z' E HQ Headquarters. . p4 G. u* r: t* pMDA GLOSSARY, VER. 4.0 H * @* u9 U; g9 ?. o/ p. z8 M129+ y' u) r0 @ ~2 i) w: `$ I: e- q HQMC Headquarters, Marine Corps. ) H. ]: G4 i9 | j" uHRDS High Resolution Display System. $ E: S% \2 l3 i9 \; _HREPS Heavy Replicas. ; x% G- O0 P0 W: i. i! A( K8 D/ `HRR High Range Resolution., `3 ?% M2 ~; H7 h& ~ HRSA HICTB Requirements, Support and Analysis.; B+ y" T J* r4 L5 y0 F2 v/ L; _ HSDB High Speed Data Bus (TelComm/Computer term).# P2 w5 s" Z3 { HSFB High Speed Fleet Broadcast (Navy term). $ C, ^5 j. b4 ^8 b* QHSI Human Systems Integration.' H' g- L, Y- r5 C G; O HSV Huntsville, Alabama. 0 ]1 K8 P% p% Z+ R( WHTICIA High Technology Crime Investigation Association.9 i, S* i8 r9 Z5 `' D, Z% b HTI Horizontal Technology Initiative.- ]' p( V0 Z {* W4 Q4 r* j+ k HTK Hit-to-Kill. # R- n8 m) i) p3 tHTMIAC High Temperature Materials Information Analysis Center. 6 x+ \' v3 P) x" @HTML Hypertext Markup Language.% L8 y |* ^, R9 ~' T HTPB Hydroxy-Terminated Poly Butadiene. - k# y' R& l% F) K# Z+ o$ EHTS (1) High Temperature Super-conducting. (2) Hawaii Tracking Station. 6 ]! S! p; i1 T% ]1 ^) JHTSA Host Tenant Support Agreement.8 U: l" c+ d% f5 ?0 S8 Z HTSS Hardened- sub-miniature Telemetry and Sensor System. 7 `$ {9 q' |- B# D; B- ^HTTP Hypertext Transfer Protocol.5 o: ^+ ~& B! F$ E) k HUD Heads Up Display. : f, \9 y. I/ ^' l& JHuman Factors A body of scientific facts about human characteristics. The term covers all0 `" C9 A5 i$ s% V- {! y9 l biomedical and psychosocial considerations; it includes, but is not limited to,( ]7 o0 }5 t% n+ ^ z( A principles and applications in the areas of human engineering, personnel3 V2 M! D& M0 X! e selection, training, life support, job performance aids, and human performance # H+ n; Q3 d: o8 [& t+ H/ V, Z+ Sevaluation." {& |* y; @3 u3 `; g' u! O* @$ X- h Human Factors. H. F9 W2 c; ~3 ~8 _% f' T Engineering % J& O) s. X: s* Q8 Y9 E9 I1 Y" gThe design of man-made devices, systems, and environments to enhance their/ q; d1 D; ~, d% m1 l4 c 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, 2024-5-11 18:32 , Processed in 0.046800 second(s), 10 queries .

Powered by Discuz! X2

© 2001-2011 MinHang.CC.

回顶部