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FCT Foreign comparative testing.- U3 z O! ?9 W% ]8 O1 z @
FD First Deployment.
* n) i% E' |# }2 e- uFDA Food and Drug Administration.
& i; }# y- Z! [FDC Fire [of weapons] Direction Center.4 C( v* `8 X, k) l) j; ]
FDG Foreign Disclosure Guide.
) r, R/ b7 t3 \4 m+ s% zFDM Function Description Manual.# u3 y+ F1 ^: h8 O1 M( e1 [" G
FDO Fee Determining Official.
1 p9 h4 a- R1 n# i: K0 Q6 A/ oMDA GLOSSARY, VER. 4.0 F; j3 W9 k8 x `! h+ ]9 J. u
1057 ^: F. [% M$ V0 R: Q
FDP Flight Demonstration Program.
- p, R1 ?, Y1 C% d. P8 ]. _5 ?; n- _FDR Final/Formal Design Review.1 a; q: v d% |, B8 e/ T4 u; g
FDRU Final Design Review Update (MDA PAC term).
. X8 L9 e0 l6 w, O5 X6 S4 B) w5 QFDS (1) Flight Demonstration System. (2) Fault Detection System.
) u% ~- p0 F- F+ q0 @7 G( X) |) sFDSV Flight Demonstration Space Vehicle.- W+ W9 U9 h; U( Q, l+ \$ y/ j
FDT&E See Force Development Test and Experimentation (US Army).1 I" G; ]# J, @3 U( r- z
FDX Full Duplex (Telecomm/Computer term).
# c4 {7 B/ p$ g9 X# k* V. qFEA Functional Economic Analysis./ t: D* P! J* n, u
Feasibility Study A study of the applicability or desirability of any management or procedural9 ?5 A/ `, s2 Q
system from the standpoint of advantages versus disadvantages in any given
7 |4 [! i w+ S6 Q) ]6 n1 X" _& Z4 acase.
" ^: w& T' ~9 a- Z! @8 mFEBA Forward Edge of the Battle Area.
: f2 V- y" M# V9 |* rFECA Front-End Cost Analysis5 ]# N7 K! h4 Q2 x
FED Federal.
) Y& T+ \/ B. p9 ^% `6 |" C: JFEDAC Federal Computer Acquisition Center.
4 g6 `+ D( w' o9 ~9 \& x( WFederal' c/ w u( Z6 f$ G% l1 }
Acquisition) o" r* F5 [3 f) x$ W+ q
Regulation5 J% X0 c# ]& C) u; g) c9 p
The primary regulation for use by federal executive agencies for acquisition of
+ G1 b: }4 C0 ?3 [) \9 T; A. Wsupplies and services with appropriated funds. It directs the defense program
; G2 E: a' e% h. T( r9 bmanager in many ways, including contract award procedures, acquisition2 {, y2 U/ k3 s" H, S$ H. {8 ~2 J
planning, warranties, and establishing guidelines for competition. The Military$ p0 Y% g+ j( y
Departments and DoD issue supplements to the FAR. The DoD supplement is
$ L1 q1 a' I4 s2 ncalled DFARS (Defense FAR Supplement).
O1 Q) J3 D- m* f3 y1 aFEDSIM Federal System Integration and Management.
& i3 b4 C; m8 g) `4 _& eFEL Free Electron Laser.
7 p: C$ _& D+ tFEMA Federal Emergency Management Agency.
6 d! J5 R1 C& n7 o! K: HFenced Funding An identified aggregation of resources reviewed, approved, and managed as a: l$ {- M/ k: c( _; y; s
distinct entity. The proposed program must be implemented within specified
% G/ k, E3 G/ |- wresources. Examples of fences areas are: Intelligence and Security, Support to6 U& g3 g& s- n9 q
Other Nations.
e( }7 z& f- n- @! j5 uFER Financial Execution Review.
9 ~; N, u! A" A) V/ D, g0 |FES Facility Engineering Surveillance Plan.# |/ o6 R- O; }6 H% J0 O
FET Field Effect Transistor.% ^* S% j+ _1 C3 } G3 Y' G8 d5 @
FEU Flight Evaluation Unit.
9 v$ m6 _$ ^. N; W: _, xFEWS Follow-on Early Warning System.
0 P& m+ ]- o: FFF Fire Finder Radar (US Army.* s0 I$ a- g8 v1 i7 k3 r! o
MDA GLOSSARY, VER. 4.0 F
: I6 b. ?) U% F* E/ A" p; S106; }' @) B; A) J F, A
FFBD Functional Flow Block Diagram.0 @) @8 n' ~9 c0 A2 l: I
FFCD Full, Final and Complete Disclosure (Treaty negotiation term).7 b. I- y( h; C, h& H5 _( J! h4 d
FFD Fraction Failure Detected.* K4 |% u) z) c. s, F
FFH Fast Frequency Hopping.4 Q2 ^$ e/ G+ j& n$ J/ c
FFP Firm Fixed Price.: o0 N `* g) I& `/ v
FFRDC Federally Funded Research and Development Center.
, G+ M6 G: G+ j4 f6 W$ b; v8 NFGC Functional Group Code (Navy ILS term).
8 e* }1 S( \# G+ B3 r; ~FGEP Fixed Ground Entry Point.
* a7 c0 T9 m9 {) q, OFH Flight Hours.( J* C/ X, |3 T8 A' Q+ \
FI Fault Isolation.8 @5 q n0 x0 B- f
FI&A Fault Isolation and Analysis.
( b( l! g* b) LFIDO Fighter Duty Officer (JFACC term).+ A2 x# F) |$ i# ~$ Z+ m
Field of View4 L( h7 C+ U! N% g
(FOV)5 o/ G9 B5 w; \% E
The angular measure of the volume of space within which the system can/ o0 D `4 i0 @
respond to the presence of a target.
; k# I0 N% o5 ~5 T6 i( sFighting Mirror) y! D6 w! A3 D1 i; y& E/ _
(FMIR)$ _0 {1 Y8 P- o$ v# S5 V; Q0 s
Part of the GBL System. The low orbit mirror, which receives laser energy and
9 ?! Y m4 k/ `1 `8 l0 jreflects it to the target.$ k3 v+ d k$ n8 \6 H& Z$ a1 g
Figure of Merit
" T8 _) b. ?% }! E5 O1 f, @(FOM)* Y9 `7 G9 M5 [0 V
The numerical value assigned to a measure of effectiveness, parameters, or) V: \ Y9 ?( p8 K0 V: l8 b7 t
other figure, as a result of an analysis, synthesis, or estimating technique.
$ o- k$ M$ A4 L+ J9 D P m* P1 iFIP Federal Information Processing.
- D, e7 e; k! T0 L1 g$ fFIPS Federal Information Processing Standard.) h# L: x( l, X- o1 |# K# j5 c
Fire Control The control of all operations in connection with the application of fire on a target.6 a& g6 ^" i7 u$ k$ c7 U" ^! Z! Q
Fire Control
' S9 p9 O* f, t( X" g j) J' zSystem& v& z4 g) n; K: |/ B& g
A group of interrelated fire control equipment and/or instruments designed for
8 j$ o5 p7 G& a$ f4 g% n9 yuse with a weapon or group of weapons.
, H; ]) _, Y& F) l: d' KFire Support
, @" @6 P- j2 I1 gCoordinating1 H9 }3 i0 _9 ]4 k9 g4 E
Measure
4 p* |2 ~& w, A) B5 ^; l/ @$ y, }A measure employed by land or amphibious commanders to facilitate the rapid
8 S( a# w8 ~& Sengagement of targets and simultaneously safeguard friendly forces.
# z4 o+ T9 p4 d0 v- DFire Support4 M- w3 Z! n: o' F
Coordinating Line
$ ?, Y7 s/ @" F9 }, }& N(FSCL)
0 ?9 ?: ?$ _* V' g1 HA line established by the appropriate ground commander to ensure the! J! u8 X2 |; F- }" a2 Z% C
coordination of fire not under the commander’s control but may affect current- G, @4 ^) S- ]% Z5 D' h" ^( F
tactical operations. The fire support coordination line is used to coordinate fires
# f& [& T3 F; q- wof air, ground, or sea weapons systems using any type of ammunition against
" d' n; G/ H- Zsurface targets. The fire support coordination line should follow well-defined! d9 W7 F, W1 [% {
terrain features. The establishment of the FSCL must be coordinated with the
7 |$ h: N7 d, M- b+ {: _appropriate tactical air commander and other supporting elements of the FSCL
* X+ S6 x) \0 T3 ]* Hwithout prior coordination with the ground force commander provided the attack
" E; |8 e) f! k# E, P) fwill not product adverse effects on or to the rear of the line. Attacks against3 M( t5 q% g3 n ]( P; q9 T
surface targets behind this line must be coordinated with the appropriate ground
# R+ W% ?0 \& ]- i1 {1 Tforce commander.
! H3 C$ a, r( M. d+ BMDA GLOSSARY, VER. 4.0 F- O4 O" K) ~9 o, {3 K) _
1077 [' Y3 J" t2 u5 g0 _1 K
Firing Doctrine The ratio and manner of assigning numbers of interceptors against given
; b- A" h) \% ^- wattackers. One-on-one, salvo, shoot-look-shoot, shoot-fail-shoot, etc. are
/ O* {8 ~& s! z7 [9 ^examples of different firing doctrine. The priority of targets being defended and5 p9 \) E+ }' }4 T9 P% |$ K0 G
the number of interceptors available relative to the number of attackers drive; D4 r; f3 h; A2 j6 _ }( o
doctrine." j" p" W3 c7 z6 a. o
Firing Rate The number of missiles fired per site per minute.
8 a1 ?! e+ ^0 d; lFIRMR Federal Information Resources Management Regulation.5 y9 h; T8 i' w, Y6 p
FIRST Forum of Incident Response and Security Teams.
! R3 z8 O0 l5 w- O7 K% C9 W2 uFirst Article First article includes pre-production models, initial production samples, test
9 T& x/ T" H! o2 z& ^samples, first lots, pilot models, and pilot lots. Approval involves testing and1 H" t' k( F; T( q. ]
evaluating the first article for conformance with specified contract requirements. w1 F8 s$ e; n, J, Y
before or in the initial stage of production under a contract.
& |: a+ R& f7 I8 v. pFirst Strike The first offensive action of a war (generally associated with nuclear operations).
0 @ I& E' X* c R3 _" q J+ h' ~First Unit# K; I' ]/ G$ m; s$ k7 r$ _
Equipped Date
& d! g! v/ K- S$ a2 b* V, n+ i# @The scheduled date an end item and its support elements are issued to the* s( r; Y, w% s# k1 _9 n: {: n
initial operational capability unit and training in the new equipment training plan" r) g1 n/ G) s: s
has been accomplished.* a1 D, ~3 }5 L+ k
FIS Facility Installation Standard.
" U' w9 K4 ^: C, i+ o! iFiscal Guidance The annual guidance issued by the SECDEF in the Defense Guidance which# X9 W# \5 m3 m! y
provides the fiscal constraints that must be observed by the DoD Components in
6 p8 K( D+ n% y9 w( @the formulation of force structures and the FYDP, and by the OSD in reviewing
1 a: m% R" ~7 Y- }2 mproposed programs.
( t% H1 D: q6 V" }1 H# F8 tFISSP Federal Information System Support Program.) Q' J* R* @- Q+ f$ P: L
FIWC Fleet Information Warfare Center (USN term).3 _" u7 r- H$ B& W
FIX Site Firing-in-Extension (Target Launch site in White Sands Missile Range Northern
8 b# G( i$ U. S" O) jExtension).
9 j# M. G% l1 d! H( {1 j3 hFixed Costs Costs that do not vary with the volume of business, such as property taxes,* w" `* Z- n* B0 c) e
insurance, depreciation, security, and minimum water and utility fees.
\' H8 I' x- A* T! H) e; WFixed Ground
: Z O9 P# u3 a& w, GEntry Point
$ U3 f: H) a* x& Q(FGEP)
Y& x3 p- P( A( D2 ?The subset of GEPs, which are not transportable. GEPs provide the
2 Y- D+ I& P" n1 O1 icommunications interfaces between the SDS space orbital/sub-orbital elements
4 G6 L5 |$ f8 Eand the C2E.+ [' C- G& l k3 _2 }
Fixed Ground
& {& _% Z+ s: O* n" Z9 G: `& IStation
' I& [& A1 X$ i6 B. z7 g5 k7 zAll hardware, software, and facilities located at a fixed ground site necessary to
' {$ s8 o6 n# U# G+ vreceive, process, support, and analyze mission status and data, and disseminate
+ e; l2 N' T7 H6 v' L& Ooperational messages.& ^; @+ N/ p9 d0 |) i3 t6 o0 b
FLAGE OBSOLETE. Flexible Lightweight Agile Guided Experiment. (Predecessor% n f' m O3 ~" T# C( N0 F
program to Extended Range Interceptor (ERINT).)7 j0 @: a0 `) y2 L8 L
FLC Federal Laboratory Consortium.
5 y! ~: H+ Q1 ^! ]# Y- f* ]/ WMDA GLOSSARY, VER. 4.0 F b7 P& Y" h2 a& _* G$ ~
108
X9 M' q) Z a, H& \2 R0 E5 W8 tFleet Satellite
9 |: w L& [9 }6 gCommunications
. X0 y3 `2 x6 V ?- d7 DSystem) w* @- ?$ C& a6 J+ i6 P2 {
(FLTSATCOM)2 X( Z4 [$ l/ }
Operating at ultra high frequency (UHF), FLTSATCOM allows relatively low-cost
5 v( ?, k, P4 Q5 l0 Z/ [terminals with simple antennas for use on highly mobile platforms. It has a
% L# p* z9 E8 s: v1 D8 mrelatively small capacity because of its much lower operating frequency. It
% _! D' U* {, C! |5 }provides a satellite communication system for high-priority communication
- j5 D$ s: {+ Lrequirements for the Navy and Air Force that encompasses almost the entire
* Q$ y( ]; ]3 B( C, z( Tworld. It supports other DoD needs as well. It consists of satellites in geosynchronous equatorial orbit, each with 23 communication channels in the UHF' d0 C8 {0 c- ~0 L2 }1 p0 w W
and SHF bands. The Navy has exclusive use of 10 channels for communication9 h+ N: m3 a. h% ]9 W
with its land, sea, and air forces. The Air Force uses 12 others as part of its* s! P8 r% G* [( \- T
AFSATCOM system for command and control of nuclear capable forces. The) k- F" E4 Y9 Y/ ?, K
system has one 500 KHz channel allotted to the national command authorities.
! G2 \( a# _5 D# X; ^Flexible
7 s& u8 [' ]7 E+ _- WResponse* B" b, b8 s3 M: \
The capability of military forces for effective reaction to any enemy threat or
5 y! j+ _ _0 t& U% v& u& j- oattack with actions appropriate and adaptable to the circumstances existing.- _1 K9 d u4 i* T, I7 z" e; g9 o
FLHER Funds and Labor Hours Expenditure Report. G6 i3 [: }# ~+ g6 t
Flight
! I; @5 f" v% NDemonstration
, j* n# t6 n! VSystem (FDS)
0 |+ e; C# U1 H3 dPart of the SBIRS Low Program Definition and Risk Reduction (PDRR) program% x7 N& i# x7 r+ d, }5 X1 ?
phase. The FDS will consist of two satellites and a ground system being built by
: c0 `. U+ s0 B6 F& O* @TRW/Hughes. The FDS satellites are to be launched in FY99 for a two-year test* e' o+ q3 q: C# {6 `& W% U
program to demonstrate operations and performance of a SBIRS Low concept,; }0 x) T! ^# \$ F. r7 u1 B
collect target and phenomenology data to support the objective system design,
- \& j" L: H9 f) Land validate cost estimating models.
. g0 B& z: y% k! M6 _ s/ LFlight Path The line connecting the successive positions occupied, or to be occupied, by an) B, E4 p* N3 X% b- [: }. L' N
aircraft, missile, or space vehicle as it moves through air or space. (It is more
0 i3 Y) S( \$ B, n# i+ lcommonly referred to as trajectory for space vehicles, especially ICBMs.)
' `! t- v/ o9 S3 GFlight Readiness/ C3 W" F! q. S
Firing7 p2 s# W$ }& Z6 V1 Q% U, n! i
A missile system test of short duration conducted with the propulsion system! s) K' k% w$ t/ l C. |
operating while the missile is secured to the launcher. Such a test is performed% X8 b# j9 M3 t# m0 B `4 l
to determine the readiness of the missile system and launch facilities prior to' E% C7 ]( H: v; P/ i) }
flight test.. h. R- C0 K/ K3 j$ s
Flight Test Test of an aircraft, rocket, missile, or other vehicle by actual flight or launching.
9 n O* V0 c$ y3 U& z4 RFlight tests are planned to achieve specific test objectives and gain operational9 y j# H# X. L) v2 m8 g
information.3 U; P) M8 O" Y3 [
Flight Test: G5 P* R/ k7 w; v( G9 C
Vehicle (FTV)2 j2 l9 B1 o7 [% R8 _
Prototype of airborne or spaceborne hardware used to validate a technology( x s! H2 @( z/ x7 _) Z/ E
concept. |
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