Difference between revisions of "List of Acronyms and Abbreviations"
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;AORP:'''A'''utonomous '''O'''rbiter '''R'''apid '''P'''rototype, a system to allow a [[STS|shuttle]] orbiter to land without [[crew]]. | ;AORP:'''A'''utonomous '''O'''rbiter '''R'''apid '''P'''rototype, a system to allow a [[STS|shuttle]] orbiter to land without [[crew]]. | ||
;atmo:[[atmosphere]] | ;atmo:[[atmosphere]] | ||
+ | ;AR:'''a'''cceptance '''r'''eview | ||
;AU:[[astronomical unit]] | ;AU:[[astronomical unit]] | ||
Line 53: | Line 54: | ||
;CaLV:'''Ca'''rgo '''l'''aunch '''v'''ehicle, see [[Ares V]] | ;CaLV:'''Ca'''rgo '''l'''aunch '''v'''ehicle, see [[Ares V]] | ||
;CDI:[[course deviation indicator]] | ;CDI:[[course deviation indicator]] | ||
− | ;CDR:commander | + | ;CDR: |
+ | #commander | ||
+ | #'''c'''ritical '''d'''esign '''r'''eview | ||
;CEV:'''C'''rew '''e'''xpedition '''v'''ehicle, see [[CEV]] | ;CEV:'''C'''rew '''e'''xpedition '''v'''ehicle, see [[CEV]] | ||
;CFD:computational fluid dynamics | ;CFD:computational fluid dynamics | ||
Line 66: | Line 69: | ||
==D== | ==D== | ||
;DN:[[descending node]] | ;DN:[[descending node]] | ||
+ | ;DDT&E:'''d'''esign, '''d'''evelopment, '''t'''est and '''e'''valuation | ||
;DG:[[Delta-glider]] | ;DG:[[Delta-glider]] | ||
;DGIII:[[DeltagliderIII]], a famous enhanced version of the [[Delta-glider]]. | ;DGIII:[[DeltagliderIII]], a famous enhanced version of the [[Delta-glider]]. | ||
Line 84: | Line 88: | ||
;Ecc:[[eccentricity]] | ;Ecc:[[eccentricity]] | ||
;ECL:plane of the [[ecliptic]] | ;ECL:plane of the [[ecliptic]] | ||
+ | ;ECSS:'''e'''uropean '''c'''ooperation for '''s'''pace '''s'''tandardization | ||
;EELV:Evolved Expendable Launch Vehicle | ;EELV:Evolved Expendable Launch Vehicle | ||
;ESA:[[European Space Agency]] | ;ESA:[[European Space Agency]] | ||
Line 127: | Line 132: | ||
==L== | ==L== | ||
;LAN:longitude of [[ascending node]] or local-area network | ;LAN:longitude of [[ascending node]] or local-area network | ||
+ | ;LCC: | ||
+ | #'''l'''aunch '''c'''ontrol '''c'''enter | ||
+ | #'''l'''ife '''c'''ycle '''c'''ost | ||
;LDEF:[[Long Duration Exposure Facility]] | ;LDEF:[[Long Duration Exposure Facility]] | ||
;LEO:[[Low earth orbit]] | ;LEO:[[Low earth orbit]] | ||
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;MCC-H:'''m'''ission '''c'''ontrol '''c'''enter '''h'''ouston | ;MCC-H:'''m'''ission '''c'''ontrol '''c'''enter '''h'''ouston | ||
;MCC-M:'''m'''ission '''c'''ontrol '''c'''enter '''m'''oscow | ;MCC-M:'''m'''ission '''c'''ontrol '''c'''enter '''m'''oscow | ||
+ | ;MDR:'''m'''ission '''d'''efinition '''r'''eview | ||
;MECO:'''M'''ain '''E'''ngine '''C'''ut'''o'''ff | ;MECO:'''M'''ain '''E'''ngine '''C'''ut'''o'''ff | ||
;MFD:multifunction display, see [[MFD]] | ;MFD:multifunction display, see [[MFD]] | ||
Line 163: | Line 172: | ||
;p0:atmospheric pressure at sea level | ;p0:atmospheric pressure at sea level | ||
;PAPI:'''P'''recision '''A'''pproach '''P'''ath '''I'''ndicators, lit runway centreline. | ;PAPI:'''P'''recision '''A'''pproach '''P'''ath '''I'''ndicators, lit runway centreline. | ||
− | ;PB: | + | ;PB:[[Shuttle PB]] |
+ | ;PDR:'''p'''reliminary '''d'''esign '''r'''eview | ||
+ | ;PRR:'''p'''reliminary '''r'''equirements '''r'''eview | ||
;PeA:[[periapsis]] altitude | ;PeA:[[periapsis]] altitude | ||
;PeD:[[periapsis]] distance | ;PeD:[[periapsis]] distance | ||
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;PRJ:[[projection]], as seen on the [[orbit MFD]] | ;PRJ:[[projection]], as seen on the [[orbit MFD]] | ||
;PSx:Payload Specialist x | ;PSx:Payload Specialist x | ||
+ | ==Q== | ||
+ | ;QR: '''q'''ualification '''r'''eview | ||
==R== | ==R== | ||
;R: | ;R: | ||
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;Rate:rate of change, as seen on the [[align orbital plane MFD]] | ;Rate:rate of change, as seen on the [[align orbital plane MFD]] | ||
;RCS:[[reaction control system]], spacebourne orientation rocket system. | ;RCS:[[reaction control system]], spacebourne orientation rocket system. | ||
+ | ;R&D:'''r'''esearch and '''d'''evelopment | ||
+ | ;RDT&E:'''r'''esearch, '''d'''evelopment, '''t'''esting and '''e'''valuation | ||
;RInc:[[relative inclination]], as seen on the [[align orbital plane MFD]] | ;RInc:[[relative inclination]], as seen on the [[align orbital plane MFD]] | ||
;RVel:relative [[velocity]] | ;RVel:relative [[velocity]] | ||
Line 193: | Line 208: | ||
#'''S'''earch '''a'''nd '''r'''escue. | #'''S'''earch '''a'''nd '''r'''escue. | ||
#'''S'''yntetic '''a'''perture '''r'''adar, a [[radar]] mode used for creating navigation maps or detect slowly moving ground vehicles. | #'''S'''yntetic '''a'''perture '''r'''adar, a [[radar]] mode used for creating navigation maps or detect slowly moving ground vehicles. | ||
+ | ;S/C: [[spacecraft|'''s'''pace'''c'''raft]] | ||
;SDK:Software Development Kit [http://en.wikipedia.org/wiki/SDK] | ;SDK:Software Development Kit [http://en.wikipedia.org/wiki/SDK] | ||
;SDLV:'''S'''huttle '''D'''erived '''L'''aunch '''V'''ehicle, see [[Ares]] | ;SDLV:'''S'''huttle '''D'''erived '''L'''aunch '''V'''ehicle, see [[Ares]] | ||
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;TRK:Track ship, as displayed by [[map MFD]] | ;TRK:Track ship, as displayed by [[map MFD]] | ||
;TrL:[[true longitude]] | ;TrL:[[true longitude]] | ||
+ | ;TRL:'''t'''echnology '''r'''eadiness '''l'''evel | ||
;Ts:length of siderial day | ;Ts:length of siderial day | ||
;Tth:predicted thrust time, as seen on the [[align orbital plane MFD]] | ;Tth:predicted thrust time, as seen on the [[align orbital plane MFD]] | ||
;TVEL:tangential [[velocity]] | ;TVEL:tangential [[velocity]] | ||
==U== | ==U== | ||
+ | ;UNKS:known unknowns | ||
+ | ;UNK-UNKS:unknown unknowns | ||
;UT:'''u'''niversal '''t'''ime, GMT. Not to be confused with [[UTC]] (Universial Time Co-ordinated). The latter is based on atomic clocks not astronomy, hence the occasional ''leap-second'' to correct UTC to GMT. | ;UT:'''u'''niversal '''t'''ime, GMT. Not to be confused with [[UTC]] (Universial Time Co-ordinated). The latter is based on atomic clocks not astronomy, hence the occasional ''leap-second'' to correct UTC to GMT. | ||
==V== | ==V== | ||
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;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ||
==W== | ==W== | ||
+ | ;WBS:'''w'''ork '''b'''reakdown '''s'''tructure | ||
+ | ;WPD:'''w'''ork '''p'''ackage '''d'''escription | ||
;Wrp:time acceleration factor, seen in the [[general information display]] | ;Wrp:time acceleration factor, seen in the [[general information display]] | ||
==X== | ==X== |
Revision as of 19:43, 27 June 2006
This list contains definitions for Orbiter or important spaceflight acronyms or abbreviations, especially those appearing in MFDs and various HUD modes.
One entry in this list consists of a term with one or more definitions, like:
- Term
- Definition
;Term:Definition
Don't use links in the term part of a entry, please do so in the definition part, for keeping a consistent look-and-feel and don't putting to much emphasis on a single definition.
Terms without definitions will get moved to the talk page into the section "Wanted definitions". If you have multiple definitions for a term, the definition part should turn into a numbered list, like:
- Term
- Definition 1
- Definition 2
- Definition 3
;Term: #Definition 1 #Definition 2 #Definition 3
The order of the definitions should be like that:
- Orbiter HUD definitions
- Orbiter MFD definitions
- General Orbiter definitions
- Orbiter addon definitions
- General spaceflight definitions
If you don't agree to a ordering of definitions, please complain in the talk page about the entry.
Contents: Top - 0–9 A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
A
- AF
- AgP
- argument of periapsis
- AN
- ascending node
- ApA
- apoapsis altitude
- ApD
- apoapsis distance
- ApR
- apoapsis radius
- ApT
- time to apoapsis
- Alt
- altitude
- AORP
- Autonomous Orbiter Rapid Prototype, a system to allow a shuttle orbiter to land without crew.
- atmo
- atmosphere
- AR
- acceptance review
- AU
- astronomical unit
B
- BMW
- Bate, Mueller, White - authors of Fundamentals of Astrodynamics (1971)
C
- CaLV
- Cargo launch vehicle, see Ares V
- CDI
- course deviation indicator
- CDR
- commander
- critical design review
- CEV
- Crew expedition vehicle, see CEV
- CFD
- computational fluid dynamics
- CLV
- Crew launch vehicle, see Ares I
- COM
- communication or communicator
- CTD
- crash to desktop
- CTRL
- Control
- CVEL
- closing velocity
- Common Vessel Extensions Light, see CVEL
D
- DN
- descending node
- DDT&E
- design, development, test and evaluation
- DG
- Delta-glider
- DGIII
- DeltagliderIII, a famous enhanced version of the Delta-glider.
- DG-S
- Delta-glider equiped with two scramjets.
- DIV
- divergent, i.e. yaw gimbal mode.
- Dir
- direction
- Dist
- distance
- DLng
- longitude difference, as seen on the synchronise orbit MFD
- DNP
- dynamic pressure
- DNS
- atmospheric density
- DST or Dst
- distance (to target)
- DTe
- time to ejection, as seen on the transfer MFD
- DTi
- time to intercept, as seen on the transfer MFD
- DTmin
- time of arrical difference, as seen on the synchronise orbit MFD
- Dv
- delta velocity, as seen on the transfer MFD, see also Delta-V
E
- Ecc
- eccentricity
- ECL
- plane of the ecliptic
- ECSS
- european cooperation for space standardization
- EELV
- Evolved Expendable Launch Vehicle
- ESA
- European Space Agency
- ESAS
- Exploration Systems Architecture Study
- ET
- external tank
- EQU
- plane of the equator
- EVA
- Extra vehicular activity, see EVA
F
- FGB
- russian acronym for Functional Cargo Block. See FGB
- FoV
- field of view, as seen in the general information display
- FPS
- frame rate, as seen in the general information display
G
- G
- an unit of acceleration. 1 G equals the gravity acceleration on earths surface, 9.81 m/s²
- GL
- Used often as vehicle name prefix for a Delta-glider
- GMT
- Greenwich Mean Time.See UT [1]
- GPS
- global positioning system
- GS
- ground speed
- GTO
- Geostationary transfer orbit, see GTO
H
- H
- Horizon
- HLLV
- heavy lift launch vehicle
- HUD
- heads up display
- HSI
- horizontal situation indicator
- HST
- Hubble Space Telescope
- HTO
- hypothetical orbit, as seen on the transfer MFD
I
- IAS
- indicated air speed [2]
- IDS
- instrument docking system
- ILS
- instrument landing system
- International launch services, a US-russian joint venture marketing Atlas and Proton launches
- Inc
- Inclination
- ISP
- specific impulse, see ISP
- ISS
- International Space Station
J
- JD
- julian date
- JWST
- James Webb Space Telescope
K
- KISS
- "Keep it simple, stupid!" Famous engineering dogma.[3]
- KSC
- Kennedy Space Center
L
- LAN
- longitude of ascending node or local-area network
- LCC
- launch control center
- life cycle cost
- LDEF
- Long Duration Exposure Facility
- LEO
- Low earth orbit
- LOX
- Liquid Oxygen
- LPe
- longitude of periapsis
M
- m
- metre
- M
- Mega (SI prefix). Occasionally mass or mach number
- MCC
- mid course correction
- mission control center
- MCC-H
- mission control center houston
- MCC-M
- mission control center moscow
- MDR
- mission definition review
- MECO
- Main Engine Cutoff
- MFD
- multifunction display, see MFD
- MJD
- modified julian date
- MMU
- manned maneuvering unit, see MMU
- MnA
- mean anomaly
- MnL
- mean longitude
- MSx
- Mission Specialist x
- m/s
- meters per second, the SI base unit of velocity
N
- NAV
- navigation
- navigation aid
O
- OAT
- outside air temperature
- Ob
- obliquity of ecliptic (tilt of axis of rotation against plane of ecliptic)
- OBS
- omni bearing selector
- OBT
- orbit, as seen on the orbit MFD
- OMS
- orbital maneuvering system, the 'main engines' of the space shuttle orbiter
- OS
- orbital speed
P
- P
- position (sometimes radius) vector, as seen on the align orbital plane MFD
- p0
- atmospheric pressure at sea level
- PAPI
- Precision Approach Path Indicators, lit runway centreline.
- PB
- Shuttle PB
- PDR
- preliminary design review
- PRR
- preliminary requirements review
- PeA
- periapsis altitude
- PeD
- periapsis distance
- PeR
- periapsis radius
- PG
- prograde
- PLT
- Pilot
- PMI
- Principal moments of inertia, see PMI
- Pos
- position
- PRJ
- projection, as seen on the orbit MFD
- PSx
- Payload Specialist x
Q
- QR
- qualification review
R
- R
- mean radius
- specific gas constant
- r0
- atmospheric density at sea level
- Rad
- radial distance
- angular unit radians
- RAnm
- true anomaly of reference axis, as seen on the synchronise orbit MFD
- Rate
- rate of change, as seen on the align orbital plane MFD
- RCS
- reaction control system, spacebourne orientation rocket system.
- R&D
- research and development
- RDT&E
- research, development, testing and evaluation
- RInc
- relative inclination, as seen on the align orbital plane MFD
- RVel
- relative velocity
- RG
- retrograde
- RKA
- Russian Space Agency
- RMS
- Remote Manipulator System
S
- SAR
- Search and rescue.
- Syntetic aperture radar, a radar mode used for creating navigation maps or detect slowly moving ground vehicles.
- S/C
- spacecraft
- SDK
- Software Development Kit [4]
- SDLV
- Shuttle Derived Launch Vehicle, see Ares
- SDHLV
- Shuttle Derived Heavy Launch Vehicle, see Ares V
- SECO
- Secondary Engine Cutoff
- Sustainer Engine Cutoff
- Sim
- simulation time (in seconds), as seen in the general information display
- a common abbreviation for "simulator"
- SHP
- ship, as seen on the orbit MFD
- Sh-ToR
- ship time-on-reference, as seen on the synchronise orbit MFD
- SLF
- shuttle landing facility, see Cape Canaveral
- SMa
- semi-major axis
- SSME
- Space Shuttle Main Engines [5]
- SMi
- semi-minor axis
- SRB
- Solid Rocket Booster [6]
- SRTM
- Shuttle radar topography mission, see SRTM.
- SSTO
- Single Stage to Orbit
- STOVL
- Short take-off, vertical landing. As performed by the DG on full fuel employing hover thrusters during takeoff.
- STP
- static pressure
- STS
- space transportation system, AKA space shuttle, see space transportation system
T
- Tgt
- target, esp. in docking mode
- Tg-ToR
- target time-on-reference, as seen on the synchronise orbit MFD
- T
- orbit period, measured in seconds
- TAS
- true air speed [7]
- TKS
- russian spacecraft for the Almaz program, see TKS
- TLE
- two-line elements
- TLe
- eject longitude, as seen on the transfer MFD
- TLi
- intercept longitude, as seen on the transfer MFD
- TLI
- Trans Lunar Injection
- Tn
- time to node, as seen on the align orbital plane MFD
- TOFS
- tangential offset docking MFD
- TrA
- true anomaly
- TRK
- Track ship, as displayed by map MFD
- TrL
- true longitude
- TRL
- technology readiness level
- Ts
- length of siderial day
- Tth
- predicted thrust time, as seen on the align orbital plane MFD
- TVEL
- tangential velocity
U
- UNKS
- known unknowns
- UNK-UNKS
- unknown unknowns
- UT
- universal time, GMT. Not to be confused with UTC (Universial Time Co-ordinated). The latter is based on atomic clocks not astronomy, hence the occasional leap-second to correct UTC to GMT.
V
- VASI
- Visual Approach Slope Indicator, the glideslope lighting system ajacent to runways to guide pilots onto the correct angle of glideslope (normally 3 degrees).
- VC
- virtual cockpit
- Visual C++, an IDE and C++ compiler by Microsoft.
- Vel
- velocity
- VOR
- very high frequency omnidirectional radio
- VS
- vertical speed
- VTOL
- Vertical Take Off and Landing
W
- WBS
- work breakdown structure
- WPD
- work package description
- Wrp
- time acceleration factor, seen in the general information display
X
- XPDR
- transponder
Y
- YSC
- Yokohama Science Center
Z
- ZM
- zoom, as seen on the map MFD
Contents: Top - 0–9 A B C D E F G H I J K L M N O P Q R S T U V W X Y Z