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Technical
8 d) k! }+ @( O6 {Evaluation: x7 Q% P6 g4 g7 s+ X6 z! s
The study, investigation, or test and evaluation by a developing agency to
+ ?4 K2 k0 k1 U Ndetermine the technical suitability of materiel, equipment, or a system, for use in* ` c& C9 a! E: Z" h& V" k
the military services. (See Development Test and Evaluation.), m6 q! p3 A2 k5 ^% _+ d
Technical
# f2 L, x( Y' j$ Q/ f; A' R7 OObjectives/ F1 X$ x0 f7 p. h5 u
The “target” values for the development effort when insufficient data is available
1 O* C$ y! {3 r7 l5 y* g9 [for stating binding technical requirements.# _) _9 x. e7 u# t) L, v2 V
Technical, ^$ G7 Q. Z0 O; i( j- N: u* U
Objectives &
: g# n; x; g9 `* c( i- a$ C( IGoals (TOG)+ t7 S N5 q$ T. T3 Y
High-level acquisition document to guide decision making for BMDS; ]5 g/ b2 I' y
development; communicates objectives and goals. j: V) C8 D: i" P" @
Technical% J2 `" a# ? p" V, l2 |# u2 l
Parameters (TPs)
$ }; ~$ @: i: TA selected subset of the system’s technical metrics tracked in Technical t; u7 y# C1 `& m8 f
Performance Measurement. Critical technical parameters are identified from risk7 h% I% N2 q9 t! w/ q8 k, u
analyses and contract specification or incentivization, and are designed by
6 `' L3 V# L, E$ R2 o- e# Z' A l6 Vmanagement.
' S' L; w" Y* x9 W7 U& gTechnical
, D, I& j P: {9 {8 L. D/ p8 RPerformance
2 z* R _( w; y6 i, Q* e4 |, c, k, AMeasurement
$ B* O3 C0 s" B1 _' _5 W3 u(TPM). E( B& |. p( \6 o7 S. l+ t% p! I
Describes all the activities undertaken by the government to obtain design status& S; c, ]' a e
beyond that treating schedule and cost. TPM is defined as the product design9 c7 Y$ j. i7 i1 i8 [
assessment, which estimates, through tests the values of essential performance/ v/ y! R0 N' u( W" ]
parameters of the current design of WBS product elements. It forecasts the2 y2 Z. m5 P% K1 z8 a' e. ? t
values to be achieved through the planned technical program effort, measures0 W- x+ E) q# ]0 q+ w
differences between achieved values and those allocated to the product
' b8 w* q5 l4 r+ H, `element by the system engineering process, and determines the impact of these: E% p: n! Z" C
differences on system effectiveness.
9 f# j$ O. [" j, g$ @Technical
1 Z) X2 s; N7 k% m6 F5 e# c7 }Specification3 s0 M/ o6 U, o4 q9 P! P' K1 G
A detailed description of technical requirements stated in terms suitable to form# \9 N6 o$ X1 Q8 J% f
the basis for actual design development and production.
) w; ]1 |+ I/ H. y) `Technical
& K; `) b' \: A, z- ZSurveillance* u0 P2 v |" S8 F! L! d3 z: b
Intelligence gathering methods in which clandestine listening, photographic or
- L/ Y: [2 d$ j2 u1 w+ eemanations gathering instruments are placed within SDS facilities, or otherwise, l" \5 U: f3 P& z U; Q
targeted against SDS assets to gain access to denied information.
- d# m! a9 x% ITechnology
' }" s& d7 @' F5 `0 XExecuting Agent
: M# Q2 W2 t0 l$ F9 M5 `4 UThe Service or agency (DoD or non-DoD) that has been delegated management, [8 k! @( ?! z e' e
responsibility for a particular critical supporting technology by MDA or Executing
3 i# c) E& f0 y8 h, d: @$ w PAgent.- N. u( i" z: k# N% O, w
Technology6 l: P l5 _( J; W. `0 ]; o5 N
Program
, m- J. o2 i( XDescription
3 D3 L" j8 H/ `! B* VThe generic description of the applicable supporting technology or critical$ o$ p8 s# S& d- c
supporting technology.
0 [: ~9 ?. S( \( {5 ~: FTECOM Test and Evaluation Command.
, ~; t1 r9 p% F. VTED Technology Exploitation Demonstration.7 r+ D' `) g J, m" u7 I
MDA GLOSSARY, VER. 4.0 T7 z3 M/ D c" t7 f5 g( W- A
295
" ?" a9 N& n& E5 }TEIPT Test and Evaluation Integrated Product Team.
( o" R0 P- b2 \; _( {5 J& q. t% D5 sTEL Transporter-Erector-Launcher.
: `: W) h8 @7 wTelemetry,
1 F2 U; ]7 ^/ R; p0 K' B0 ZTracking, and, H$ P& F) ^* t4 n
Command (TT&C)
* f+ ~7 j' a) r' t; ]1 vFunctions performed by the satellite control network to maintain health and/ R# V* a+ q3 p J" P5 s( h
status, measure specific mission parameters and processing over time a
0 ^, _1 B- W7 E- i. Osequence of these measurement to refine parameter knowledge, and transmit
( N) Q. k" p% k* v3 K3 x: X emission commands to the satellite.3 Y; B; D" D7 e* i4 t
Teleprocessing The combining of telecommunications and computer operations interacting in the
( C4 D, Q+ c& ]9 f" T7 ~automatic processing, reception, and transmission of data and/or information.
5 R; I) Q: `& l6 K& s7 H+ _TELESAT Telecommunications Satellite.
; R: q z, j9 W& N ETELINT Telemetry Intelligence." X3 M: O- l2 p
TEMO Training Exercises and Military Operations.
9 i) \1 H* K7 h, X+ NTEMP See Test and Evaluation Master Plan.4 M |$ M% b9 J/ d( a
TEMPEST TEMPEST is an unclassified short name referring to investigation and studies of
' H& n5 d) i, K- [ Pcompromising emanations. It is often used synonymously for the term
' r* j( o" S5 v; c7 Y"compromising emanations,” e.g. TEMPEST tests, TEMPEST inspection. (See. Y0 ]$ G4 m6 c! x6 A6 Q
Compromising Emanations.)
3 O [) H l! x; W+ d% S2 |6 N/ ATENCAP Tactical Exploitation of National Capabilities. J9 c9 ~; S6 O( o
TEP Test and Evaluation Plan.
) K; h! @7 D3 L. _ tTER Test and Evaluation Report$ G$ n! Y8 z/ k0 c) }" B! W
TERC Test and Evaluation Resource Committee./ N% J8 D% j# u/ [
TERCOM Terrain Contour Matching.
& ~8 D5 ]% _3 O) HTerminal Defense
! e/ ^* d* s3 q$ c. bSegment (TDS)3 ~9 Z' J0 T& M7 ?3 y4 p' s
The portion of the BMDS that defeats ballistic missiles in period of flight between
, H: a4 H: T% d3 Natmospheric reentry and impact.
' E. ] W: D% cTerminal
8 b0 n: c! u( |: lGuidance
4 x; e1 x2 k9 K# q8 E* E8 aThe guidance applied to a guided missile between midcourse and arrival in the" X: l" d8 ^2 x7 ^# f: D
vicinity of the target.
4 T8 y. M- D) ?$ r7 O" o, ITerminal Phase That final portion of a ballistic missile's trajectory between the midcourse phase
# S2 U8 t8 }* Zand trajectory termination.+ ]8 ~; M% W; f }2 [
Terminal Phase
( W S, ?& j6 r! IInterceptor- Q7 ]/ H$ x$ s k2 Y) Z3 R+ \. c
A ground-based interceptor designed to intercept and destroy RVs in the
$ y8 j2 M, Y5 N% M, m% n# {terminal phase of flight. It may also be assigned to intercept and destroy enemy! {$ A7 I/ F: m) @! z4 \
PBVs and RVs in the midcourse phase. (USSPACECOM)
5 H4 L. O9 ~8 `' S8 vTerminator Transition from sunlight to earth's shadow in space., O3 [9 j* s/ l: p% v
TERS Tactical Event Reporting System.
. f1 D, G! L, j5 zTES Tactical Event System.1 O0 _" {1 t, O
TESP Test and Evaluation Security Plan.
' L* f1 y: h4 r0 v+ v# o: tTESSE Test Environment Support System Enhancement.
- m }; i" y( r ?2 Z, h7 d! XMDA GLOSSARY, VER. 4.0 T
" f9 `, w" u6 a. T1 r9 }296; }' ?% f) s8 p
Test and Control The ISTC Test and Control provides the human interface for testing system
, n1 U( R1 _& u7 z' Yhardware and software. The Test and Control will consist of the necessary( f- H6 N8 V& a0 u5 E* O
consoles, processors, and storage devices in order to be able to control all# ?3 o; t$ R! E( s
operations of the ISTC such as configuring the system, running a scenario,9 o, x8 F3 }$ {! \. C! P7 [
analyzing data, generating reports, and testing system hardware and software.
' K7 l% R' Q( A) ~% K7 h& V1 X' j& dTest and5 J1 g5 K1 Z+ g5 B4 E3 v
Evaluation (T&E)( c" ~- C2 G: i6 w( k z
Process by which components or systems are tested and the results evaluated
# M1 D2 v" J+ [9 S& H |- \to assess progress of design, performance, supportability, etc. There are three: @" p" g9 Z( U* D
types of T&E -- Development (DT&E), Operational (OT&E), and Production
1 C C; J+ }8 L% mAcceptance (PAT&E)--occurring during the acquisition cycle. DT&E is conducted
9 p9 \. u& [5 B1 }3 f9 Tto assist the engineering design and development process, to proof
' l* z4 h+ t; a; i1 w# Omanufacturing processes and control and to verify attainment of technical0 ^$ Z/ N+ F1 C0 F
performance specifications and objectives. OT&E is conducted to estimate a$ ]; Q/ A5 o% o+ q% ~# X/ z3 u) c! z
system's operational effectiveness and suitability, identify needed modifications,$ i& m# i) O3 X# E" m4 p% {
and provide information on tactics, doctrine, organization, and personnel
+ x/ B; w7 X1 J7 |' brequirements. PAT&E is conducted on production items to demonstrate that
" E: c- g' {" M0 g( J$ rthose items meet the requirements and specifications of the procuring contracts+ F2 Z& p/ c- r q
or agreements. OT&E is further subdivided into two phases--Initial Operational. J2 J) q4 r( A m
(IOT&E) and Follow-on Operational (FOT&E). IOT&E must be conducted before7 I: z5 c4 h* H
the production decision (Milestone III) to provide a credible estimate of$ y8 m1 Z* n, R6 ]. x8 Z
operational effectiveness and suitability. Therefore, IOT&E is a field test
; D( ]) N v6 k5 y" qconducted on a production representative system in an operationally realistic
( N" V9 ?7 L6 G, ]% W: N( ~+ u7 yenvironment, by typical user personnel and includes use of realistic threats.
: N. N2 j. k& k# z6 u. lFOT&E is conducted on the production system to verify operational effectiveness/ t8 v9 p* p, a& t6 d) @& J
and suitability, to fill data voids from the IOT&E, or to verify correction of
7 n$ ?0 D9 B6 I7 J; E' \8 jdeficiencies in materiel, training, or concepts. |
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