Difference between revisions of "List of Acronyms and Abbreviations"
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− | + | =A= | |
;AF: | ;AF: | ||
;AgP:[[argument of periapsis]] | ;AgP:[[argument of periapsis]] | ||
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;AU:[[astronomical unit]] | ;AU:[[astronomical unit]] | ||
− | + | =B= | |
;BMW:'''B'''ate, '''M'''ueller, '''W'''hite - authors of ''Fundamentals of Astrodynamics'' (1971) | ;BMW:'''B'''ate, '''M'''ueller, '''W'''hite - authors of ''Fundamentals of Astrodynamics'' (1971) | ||
− | + | =C= | |
;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]] | ||
Line 72: | Line 72: | ||
#'''C'''ommon '''V'''essel '''E'''xtensions '''L'''ight, see [[CVEL]] | #'''C'''ommon '''V'''essel '''E'''xtensions '''L'''ight, see [[CVEL]] | ||
− | + | =D= | |
;DN:[[descending node]] | ;DN:[[descending node]] | ||
;DDT&E:'''d'''esign, '''d'''evelopment, '''t'''est and '''e'''valuation | ;DDT&E:'''d'''esign, '''d'''evelopment, '''t'''est and '''e'''valuation | ||
Line 91: | Line 91: | ||
;Dv:delta [[velocity]], as seen on the [[transfer MFD]], see also [[Delta-V]] | ;Dv:delta [[velocity]], as seen on the [[transfer MFD]], see also [[Delta-V]] | ||
− | + | =E= | |
;Ecc:[[eccentricity]] | ;Ecc:[[eccentricity]] | ||
;ECL:plane of the [[ecliptic]] | ;ECL:plane of the [[ecliptic]] | ||
Line 102: | Line 102: | ||
;EVA:'''E'''xtra '''v'''ehicular '''a'''ctivity, see [[EVA]] | ;EVA:'''E'''xtra '''v'''ehicular '''a'''ctivity, see [[EVA]] | ||
− | + | =F= | |
;FGB:Russian abbreviation for Functional Cargo Block. See [[FGB]] | ;FGB:Russian abbreviation for Functional Cargo Block. See [[FGB]] | ||
;FoV:field of view, as seen in the [[general information display]] | ;FoV:field of view, as seen in the [[general information display]] | ||
;FPS:[[frame rate]] (frames per second), as seen in the [[general information display]] | ;FPS:[[frame rate]] (frames per second), as seen in the [[general information display]] | ||
− | + | =G= | |
;g:a unit of acceleration. 1g equals the gravity acceleration on earths surface, 9.81 m/s² | ;g:a unit of acceleration. 1g equals the gravity acceleration on earths surface, 9.81 m/s² | ||
;GL:Used often as vehicle name prefix for a [[Delta-glider]] | ;GL:Used often as vehicle name prefix for a [[Delta-glider]] | ||
Line 124: | Line 124: | ||
;HTO:[[hypothetical transfer orbit]], as seen on the [[transfer MFD]] | ;HTO:[[hypothetical transfer orbit]], as seen on the [[transfer MFD]] | ||
− | + | =I= | |
;IAS:indicated air speed [http://en.wikipedia.org/wiki/Indicated_air_speed] | ;IAS:indicated air speed [http://en.wikipedia.org/wiki/Indicated_air_speed] | ||
;IDS:[[instrument docking system]] | ;IDS:[[instrument docking system]] | ||
Line 134: | Line 134: | ||
;ISS:[[International Space Station]] | ;ISS:[[International Space Station]] | ||
− | + | =J= | |
;JD:[[Julian date]] | ;JD:[[Julian date]] | ||
;JWST:'''J'''ames '''W'''ebb '''S'''pace '''T'''elescope | ;JWST:'''J'''ames '''W'''ebb '''S'''pace '''T'''elescope | ||
− | + | =K= | |
;KISS:"Keep it simple, stupid!" Famous engineering dogma.[http://en.wikipedia.org/wiki/KISS_principle] | ;KISS:"Keep it simple, stupid!" Famous engineering dogma.[http://en.wikipedia.org/wiki/KISS_principle] | ||
;KSC:[[Kennedy Space Center]] | ;KSC:[[Kennedy Space Center]] | ||
− | + | ||
+ | =L= | ||
;LAN:longitude of [[ascending node]] or local-area network | ;LAN:longitude of [[ascending node]] or local-area network | ||
;LCC: | ;LCC: | ||
Line 151: | Line 152: | ||
;LPe:longitude of [[periapsis]] | ;LPe:longitude of [[periapsis]] | ||
− | + | =M= | |
;m:metre | ;m:metre | ||
;M:Mega (SI prefix for 10<sup>6</sup>). Occasionally mass or [[mach]] number | ;M:Mega (SI prefix for 10<sup>6</sup>). Occasionally mass or [[mach]] number | ||
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;m/s:meters per second, the SI base unit of [[velocity]] | ;m/s:meters per second, the SI base unit of [[velocity]] | ||
− | + | =N= | |
;NAV: | ;NAV: | ||
#navigation | #navigation | ||
#[[navigation aid]] | #[[navigation aid]] | ||
− | + | ||
+ | =O= | ||
;OAT:outside air temperature | ;OAT:outside air temperature | ||
;Ob:obliquity of ecliptic (tilt of axis of rotation against plane of ecliptic) | ;Ob:obliquity of ecliptic (tilt of axis of rotation against plane of ecliptic) | ||
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;OMS:'''o'''rbital '''m'''aneuvering '''s'''ystem, the 'main engines' of the [[space shuttle]] orbiter | ;OMS:'''o'''rbital '''m'''aneuvering '''s'''ystem, the 'main engines' of the [[space shuttle]] orbiter | ||
;OS:[[orbital speed]] | ;OS:[[orbital speed]] | ||
− | + | ||
+ | =P= | ||
;P:position (sometimes radius) vector, as seen on the [[align orbital plane MFD]] | ;P:position (sometimes radius) vector, as seen on the [[align orbital plane MFD]] | ||
;p0:atmospheric pressure at sea level | ;p0:atmospheric pressure at sea level | ||
Line 196: | Line 199: | ||
;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 | ;QR: '''q'''ualification '''r'''eview | ||
− | + | ||
+ | =R= | ||
;R: | ;R: | ||
#mean radius | #mean radius | ||
Line 216: | Line 221: | ||
;RKA:Russian Space Agency | ;RKA:Russian Space Agency | ||
;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ||
− | + | ;RS:Russian-side, used as prefix for orientation when describing ISS components. | |
+ | |||
+ | =S= | ||
;SAR: | ;SAR: | ||
#'''S'''earch '''a'''nd '''r'''escue. | #'''S'''earch '''a'''nd '''r'''escue. | ||
Line 243: | Line 250: | ||
;STS:'''s'''pace '''t'''ransportation '''s'''ystem, AKA space shuttle, see [[space transportation system]] | ;STS:'''s'''pace '''t'''ransportation '''s'''ystem, AKA space shuttle, see [[space transportation system]] | ||
− | + | =T= | |
;Tgt:target, esp. in [[docking]] mode | ;Tgt:target, esp. in [[docking]] mode | ||
;Tg-ToR:target [[time-on-reference]], as seen on the [[synchronise orbit MFD]] | ;Tg-ToR:target [[time-on-reference]], as seen on the [[synchronise orbit MFD]] | ||
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;TVEL:tangential [[velocity]] | ;TVEL:tangential [[velocity]] | ||
− | + | =U= | |
− | ;UNKS: | + | ;UNKS:unknown problems, you are aware of. |
− | ;UNK-UNKS:unknown | + | ;UNK-UNKS:unknown problems, you are not aware of. |
;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= | ||
;VASI:'''V'''isual '''A'''pproach '''S'''lope '''I'''ndicator, the glideslope lighting system ajacent to runways to guide pilots onto the correct angle of glideslope (normally 3 degrees). | ;VASI:'''V'''isual '''A'''pproach '''S'''lope '''I'''ndicator, the glideslope lighting system ajacent to runways to guide pilots onto the correct angle of glideslope (normally 3 degrees). | ||
;VC: | ;VC: | ||
Line 277: | Line 285: | ||
;VS:vertical speed | ;VS:vertical speed | ||
;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ||
− | + | =W= | |
;WBS:'''w'''ork '''b'''reakdown '''s'''tructure | ;WBS:'''w'''ork '''b'''reakdown '''s'''tructure | ||
;WPD:'''w'''ork '''p'''ackage '''d'''escription | ;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= | |
;XPDR:[[transponder]] | ;XPDR:[[transponder]] | ||
− | + | =Y= | |
;YSC:Yokohama Science Center | ;YSC:Yokohama Science Center | ||
− | + | =Z= | |
;ZM:zoom, as seen on the [[map MFD]] | ;ZM:zoom, as seen on the [[map MFD]] | ||
{{compactTOC}} | {{compactTOC}} |
Revision as of 17:29, 26 June 2007
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.
See also
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.
- DG4
- Orbiter's stock DG
- 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 abbreviation for Functional Cargo Block. See FGB
- FoV
- field of view, as seen in the general information display
- FPS
- frame rate (frames per second), as seen in the general information display
G
- g
- a unit of acceleration. 1g 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
H
- H
- Horizon
- HAC
- Heading Alignment Cone
- HLLV
- heavy lift launch vehicle
- HUD
- heads up display
- HSI
- horizontal situation indicator
- HST
- Hubble Space Telescope
- HTO
- hypothetical transfer 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
- 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 for 106). 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
- RS
- Russian-side, used as prefix for orientation when describing ISS components.
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
- TLA
- Three letter acronym for a three letter acronym.
- 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
- unknown problems, you are aware of.
- UNK-UNKS
- unknown problems, you are not aware of.
- 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