Difference between revisions of "List of Acronyms and Abbreviations"
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(finished reformatting, added a few new items. will define a styleguide RFC later.) |
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==A== | ==A== | ||
− | + | ;AF: | |
− | + | ;AgP:[[argument of periapsis]] | |
− | + | ;AN:[[ascending node]] | |
− | + | ;ApA:[[apoapsis]] altitude | |
− | + | ;ApD:[[apoapsis]] distance | |
− | + | ;ApR:[[apoapsis]] radius | |
− | + | ;ApT:time to [[apoapsis]] | |
− | + | ;Alt:[[altitude]] | |
− | + | ;atmo:[[atmosphere]] | |
− | + | ;AU:[[astronomical unit]] | |
==B== | ==B== | ||
− | + | ;BMW:'''B'''ate, '''M'''ueller, '''W'''hite - author team of a very famous book on astrodynamics and spaceflight (written in 1971) | |
==C== | ==C== | ||
− | + | ;CDI:[[course deviation indicator]] | |
− | + | ;CDR:commander | |
− | + | ;CEV:'''C'''rew '''E'''xpedition '''V'''ehicle, see [[CEV]] | |
− | + | ;COM:communication or communicator | |
− | + | ;CTRL:Control | |
− | + | ;CVEL: | |
− | + | #[[closing velocity]] | |
+ | #'''C'''ommon '''V'''essel '''E'''xtensions '''L'''ight, see [[CVEL]] | ||
==D== | ==D== | ||
− | + | ;DN:[[descending node]] | |
− | + | ;DG:[[Delta-glider]] | |
− | + | ;DG-S:[[Delta-glider]] equiped with two [[scramjet|scramjets]]. | |
− | + | ;DIV:[[divergent]], i.e. [[yaw]] [[gimbal]] mode. | |
− | + | ;Dir:'''dir'''ection | |
− | + | ;Dist:'''dist'''ance | |
− | + | ;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== | ==E== | ||
− | + | ;Ecc:[[eccentricity]] | |
− | + | ;ECL:plane of the [[ecliptic]] | |
− | + | ;ESA:[[European Space Agency]] | |
− | + | ;ET:[[external tank]] | |
− | + | ;EQU:plane of the [[equator]] | |
− | + | ;EVA:'''E'''xtra '''v'''ehicular '''a'''ctivity, see [[EVA]] | |
==F== | ==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== | ||
− | + | ;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 [http://en.wikipedia.org/wiki/Universal_Time] | |
− | + | ;GPS:'''g'''lobal '''p'''ositioning '''s'''ystem | |
+ | ;GS:[[ground speed]] | ||
==H== | ==H== | ||
− | + | ;H:Horizon | |
− | + | ;HLLV:'''h'''eavy '''l'''ift '''l'''aunch '''v'''ehicle | |
− | + | ;HUD:[[heads up display]] | |
− | + | ;HSI:[[horizontal situation indicator]] | |
− | + | ;HST:[[Hubble Space Telescope]] | |
− | + | ;HTO:[[hypothetical orbit]], as seen on the [[transfer MFD]] | |
==I== | ==I== | ||
− | + | ;IAS:indicated air speed [http://en.wikipedia.org/wiki/Indicated_air_speed] | |
− | + | ;IDS:[[instrument docking system]] | |
− | + | ;ILS: | |
− | + | #[[instrument landing system]] | |
− | + | #'''I'''nternational '''l'''aunch '''s'''ervices, a US-russian joint venture marketing [[Atlas]] and [[Proton]] launches | |
− | + | ;Inc:Inclination | |
+ | ;ISP:specific impulse, see [[ISP]] | ||
+ | ;ISS:[[International Space Station]] | ||
==J== | ==J== | ||
− | + | ;JD:julian date | |
==K== | ==K== | ||
− | + | ;KISS:"Keep it simple, stupid!" Famous engineering dogma.[http://en.wikipedia.org/wiki/KISS_principle] | |
− | + | ;KSC:[[Kennedy Space Center]] | |
==L== | ==L== | ||
− | + | ;LAN:longitude of [[ascending node]] or local-area network | |
− | + | ;LDEF:[[Long Duration Exposure Facility]] | |
− | + | ;LEO:[[Low earth orbit]] | |
− | + | ;LPe:longitude of [[periapsis]] | |
==M== | ==M== | ||
− | + | ;m:metre | |
− | + | ;M:Mega (SI prefix). Occasionally mass or [[mach]] number | |
− | + | ;MCC: | |
− | + | #'''m'''id '''c'''ourse '''c'''orrection | |
− | + | #'''m'''ission '''c'''ontrol '''center''' | |
− | + | ;MCC-H:'''m'''ission '''c'''ontrol '''c'''enter '''h'''ouston | |
− | + | ;MCC-M:'''m'''ission '''c'''ontrol '''c'''enter '''m'''oscow | |
− | + | ;MECO:'''M'''ain '''E'''ngine '''C'''ut'''o'''ff | |
− | + | ;MFD:multifunction display, see [[MFD]] | |
− | + | ;MJD:[[modified julian date]] | |
− | + | ;MMU:'''m'''anned '''m'''aneuvering '''u'''nit, see [[MMU]] | |
+ | ;MnA:[[mean anomaly]] | ||
+ | ;MnL:[[mean longitude]] | ||
+ | ;MSx:Mission Specialist x | ||
+ | ;m/s:meters per second, the SI base unit of [[velocity]] | ||
==N== | ==N== | ||
− | + | ;NAV: | |
+ | #navigation | ||
+ | #[[navigation aid]] | ||
==O== | ==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:'''o'''rbital '''m'''aneuvering '''s'''ystem, the 'main engines' of the [[space shuttle]] orbiter | |
− | + | ;OS:[[orbital speed]] | |
==P== | ==P== | ||
− | + | ;P:position (sometimes radius) vector, as seen on the [[align orbital plane MFD]] | |
− | + | ;p0:atmospheric pressure at sea level | |
− | + | ;PAPI:'''P'''recision '''A'''pproach '''P'''ath '''I'''ndicators, lit runway centreline. | |
− | + | ;PB: | |
− | + | ;PeA:[[periapsis]] altitude | |
− | + | ;PeD:[[periapsis]] distance | |
− | + | ;PeR:[[periapsis]] radius | |
− | + | ;PG:[[prograde]] | |
− | + | ;PLT:Pilot | |
− | + | ;Pos:position | |
− | + | ;PRJ:[[projection]], as seen on the [[orbit MFD]] | |
− | + | ;PSx:Payload Specialist x | |
==R== | ==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. | |
− | + | ;RInc:[[relative inclination]], as seen on the [[align orbital plane MFD]] | |
+ | ;RVel:relative [[velocity]] | ||
+ | ;RG:[[retrograde]] | ||
+ | ;RKA:Russian Space Agency | ||
+ | ;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ||
==S== | ==S== | ||
− | + | ;SDLV:'''S'''huttle '''D'''erived '''L'''aunch '''V'''ehicle, see [[Ares]] | |
− | + | ;SDHLV:'''S'''huttle '''D'''erived '''H'''eavy '''L'''aunch '''V'''ehicle, see [[Ares V]] | |
− | + | ;SECO: | |
− | + | #'''S'''econdary '''E'''ngine '''C'''ut'''o'''ff | |
− | + | #'''S'''ustainer '''E'''ngine '''C'''ut'''o'''ff | |
− | + | ;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 [http://en.wikipedia.org/wiki/SSME_%28rocket_engine%29] | |
− | + | ;SMi:[[semi-minor axis]] | |
− | + | ;SRB:'''S'''olid '''R'''ocket '''B'''ooster [http://en.wikipedia.org/wiki/Solid_rocket_booster] | |
+ | ;SSTO:[[Single_Stage_To_Orbit | 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:'''s'''pace '''t'''ransportation '''s'''ystem, [[space shuttle]] | ||
==T== | ==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 [http://en.wikipedia.org/wiki/True_air_speed] | |
− | + | ;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]] | |
− | + | ;Ts:length of siderial day | |
− | + | ;Tth:predicted thrust time, as seen on the [[align orbital plane MFD]] | |
+ | ;TVEL:tangential [[velocity]] | ||
==U== | ==U== | ||
− | + | ;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== | ||
− | + | ;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: | |
− | + | #virtual cockpit | |
− | + | #Visual C++, an IDE and C++ compiler by Microsoft. | |
− | + | ;Vel:[[velocity]] | |
− | + | ;VOR:[[very high frequency omnidirectional radio]] | |
+ | ;VS:vertical speed | ||
+ | ;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ||
==W== | ==W== | ||
− | + | ;Wrp:time acceleration factor, seen in the [[general information display]] | |
==X== | ==X== | ||
− | + | ;XPDR:[[transponder]] | |
==Y== | ==Y== | ||
− | + | ;YSC:Yokohama Science Center | |
==Z== | ==Z== | ||
− | + | ;ZM:zoom, as seen on the [[map MFD]] |
Revision as of 18:01, 15 March 2006
A
- AF
- AgP
- argument of periapsis
- AN
- ascending node
- ApA
- apoapsis altitude
- ApD
- apoapsis distance
- ApR
- apoapsis radius
- ApT
- time to apoapsis
- Alt
- altitude
- atmo
- atmosphere
- AU
- astronomical unit
B
- BMW
- Bate, Mueller, White - author team of a very famous book on astrodynamics and spaceflight (written in 1971)
C
- CDI
- course deviation indicator
- CDR
- commander
- CEV
- Crew Expedition Vehicle, see CEV
- COM
- communication or communicator
- CTRL
- Control
- CVEL
- closing velocity
- Common Vessel Extensions Light, see CVEL
D
- DN
- descending node
- DG
- 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
- ESA
- European Space Agency
- 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
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
K
- KISS
- "Keep it simple, stupid!" Famous engineering dogma.[3]
- KSC
- Kennedy Space Center
L
- LAN
- longitude of ascending node or local-area network
- LDEF
- Long Duration Exposure Facility
- LEO
- Low earth orbit
- 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
- 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
- PeA
- periapsis altitude
- PeD
- periapsis distance
- PeR
- periapsis radius
- PG
- prograde
- PLT
- Pilot
- Pos
- position
- PRJ
- projection, as seen on the orbit MFD
- PSx
- Payload Specialist x
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.
- 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
- 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 [4]
- SMi
- semi-minor axis
- SRB
- Solid Rocket Booster [5]
- 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, space shuttle
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 [6]
- 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
- Ts
- length of siderial day
- Tth
- predicted thrust time, as seen on the align orbital plane MFD
- TVEL
- tangential velocity
U
- 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
- 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