Difference between revisions of "List of Acronyms and Abbreviations"
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#Orbiter MFD definitions | #Orbiter MFD definitions | ||
#General Orbiter definitions | #General Orbiter definitions | ||
− | #Orbiter [[ | + | #Orbiter [[Add-on]] definitions |
#General spaceflight definitions | #General spaceflight definitions | ||
Line 34: | Line 34: | ||
==See also== | ==See also== | ||
− | [[Russian glossary]] | + | * [[Russian glossary]] |
+ | * [[List of Acronyms and Abbreviations/ISS|List of Acronyms and Abbreviations for the ISS]] | ||
---- | ---- | ||
{{compactTOC}} | {{compactTOC}} | ||
− | + | =A= | |
− | + | ;AgP:[[Argument of periapsis]]:The angle in the orbit from the point of the ascending node to the point of periapsis, Used in OrbitMFD. | |
− | ;AgP:[[ | + | ;AN:[[ascending node]]:a vector in an orbit where the body passes from south to north of the plane of reference (i.e. ecliptic or equatorial). Shown in OrbitMFD as a dotted vector line connecting to a solid square on the orbit. |
− | ;AN:[[ascending node]] | + | ;ApA:[[apoapsis]] apoapsis altitude |
− | ;ApA:[[apoapsis]] altitude | + | ;ApD:[[apoapsis]] apoapsis distance |
− | ;ApD:[[apoapsis]] distance | + | ;ApR:[[apoapsis]] apoapsis radius |
− | ;ApR:[[apoapsis]] radius | ||
;ApT:time to [[apoapsis]] | ;ApT:time to [[apoapsis]] | ||
;Alt:[[altitude]] | ;Alt:[[altitude]] | ||
Line 51: | Line 51: | ||
;atmo:[[atmosphere]] | ;atmo:[[atmosphere]] | ||
;AR:'''a'''cceptance '''r'''eview | ;AR:'''a'''cceptance '''r'''eview | ||
+ | ;ATV: | ||
+ | #'''A'''utonomous '''T'''ransfer '''V'''ehicle, an unmanned cargo spacecraft, see [[ATV]]. | ||
+ | #'''A'''utomated '''T'''ransfer '''V'''ehicle[http://www.orbiterwiki.org/wiki/ATV#The_ATV] | ||
;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 65: | Line 68: | ||
;CFD:computational fluid dynamics | ;CFD:computational fluid dynamics | ||
;CLV:'''C'''rew '''l'''aunch '''v'''ehicle, see [[Ares I]] | ;CLV:'''C'''rew '''l'''aunch '''v'''ehicle, see [[Ares I]] | ||
+ | ;COAS:'''C'''rew '''O'''ptical '''A'''lignment '''S'''ight | ||
;COM:communication or communicator | ;COM:communication or communicator | ||
;CTD:[[crash to desktop]] | ;CTD:[[crash to desktop]] | ||
;CTRL:Control | ;CTRL:Control | ||
+ | ;CTV: | ||
+ | #'''C'''rew '''T'''ransfer '''V'''ehicle, a manned spacecraft derived from the [[ATV]], see [[CTV]] | ||
+ | #'''C'''ompatibility '''T'''est '''V'''an, '''NASA''' | ||
;CVEL: | ;CVEL: | ||
#[[closing velocity]] | #[[closing velocity]] | ||
#'''C'''ommon '''V'''essel '''E'''xtensions '''L'''ight, see [[CVEL]] | #'''C'''ommon '''V'''essel '''E'''xtensions '''L'''ight, see [[CVEL]] | ||
− | + | =D= | |
+ | ;D3D9:refers to the advanced graphics client in [[Orbiter]]. | ||
;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 | ||
;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]]. | ||
+ | ;DGIV:[[DeltaGliderIV]], an improved version of the [[DeltaGliderIII]]. | ||
;DG4:Orbiter's stock '''DG''' | ;DG4:Orbiter's stock '''DG''' | ||
;DG-S:[[Delta-glider]] equiped with two [[scramjet|scramjets]]. | ;DG-S:[[Delta-glider]] equiped with two [[scramjet|scramjets]]. | ||
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;DNP:dynamic [[pressure]] | ;DNP:dynamic [[pressure]] | ||
;DNS:atmospheric density | ;DNS:atmospheric density | ||
+ | ;DPS:'''D'''ata '''P'''rocessing '''S'''ystem. Term describing the general purpose computers and their interfaces onboard various manned spacecraft. | ||
;DST or Dst:distance (to target) | ;DST or Dst:distance (to target) | ||
;DTe:time to [[ejection]], as seen on the [[transfer MFD]] | ;DTe:time to [[ejection]], as seen on the [[transfer MFD]] | ||
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;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]] | ||
;ECSS:'''e'''uropean '''c'''ooperation for '''s'''pace '''s'''tandardization | ;ECSS:'''e'''uropean '''c'''ooperation for '''s'''pace '''s'''tandardization | ||
+ | ;ECLSS:'''E'''nvironmental '''c'''ontrol and '''l'''ife '''s'''upport '''s'''ystem | ||
;EELV:Evolved Expendable Launch Vehicle | ;EELV:Evolved Expendable Launch Vehicle | ||
;ESA:[[European Space Agency]] | ;ESA:[[European Space Agency]] | ||
− | ;ESAS:[[Exploration Systems Architecture Study]] | + | ;ESAS:[[w:Exploration Systems Architecture Study|Exploration Systems Architecture Study]] |
;ET:[[external tank]] | ;ET:[[external tank]] | ||
;EQU:plane of the [[equator]] | ;EQU:plane of the [[equator]] | ||
;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]] | ||
+ | ;FRF:'''F'''light '''R'''eadiness '''F'''iring, a launch countdown test of the Shuttle running all except SRB ignition and lift-off. | ||
− | + | =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]] | ||
− | ; | + | ;GET:'''G'''round '''E'''lapsed '''T'''ime [http://history.nasa.gov/SP-4029/Apollo_00c_Introduction.htm] |
+ | ;GLOC:'''G'''ravity-induced '''L'''oss '''o'''f '''C'''onsciousness | ||
+ | ;GMT:Greenwich Mean Time.See [[w:Universal Time|Universal Time on Wikipedia]] | ||
+ | ;GPDS:[[GPDS|Generic Payload Description System]] | ||
;GPS:'''G'''lobal '''P'''ositioning '''S'''ystem | ;GPS:'''G'''lobal '''P'''ositioning '''S'''ystem | ||
;GS:[[ground speed]] | ;GS:[[ground speed]] | ||
;GTO:[[GTO|'''g'''eostationary '''t'''ransfer '''o'''rbit]] | ;GTO:[[GTO|'''g'''eostationary '''t'''ransfer '''o'''rbit]] | ||
− | + | =H= | |
;H:Horizon | ;H:Horizon | ||
+ | ;HAC:[[Heading Alignment Cone]] | ||
;HLLV:'''h'''eavy '''l'''ift '''l'''aunch '''v'''ehicle | ;HLLV:'''h'''eavy '''l'''ift '''l'''aunch '''v'''ehicle | ||
;HUD:[[heads up display]] | ;HUD:[[heads up display]] | ||
Line 123: | Line 139: | ||
;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]] | ||
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#[[instrument landing system]] | #[[instrument landing system]] | ||
#'''I'''nternational '''l'''aunch '''s'''ervices, a US-russian joint venture marketing [[Atlas]] and [[Proton]] launches | #'''I'''nternational '''l'''aunch '''s'''ervices, a US-russian joint venture marketing [[Atlas]] and [[Proton]] launches | ||
− | ;Inc:Inclination | + | ;Inc:Inclination (http://en.wikipedia.org/wiki/Inclination) |
;ISP:[[specific impulse]] | ;ISP:[[specific impulse]] | ||
;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 | ||
+ | ;JSC: Lyndon B. '''J'''ohnson '''S'''pace '''C'''enter | ||
− | + | =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 147: | Line 165: | ||
;LDEF:[[Long Duration Exposure Facility]] | ;LDEF:[[Long Duration Exposure Facility]] | ||
;LEO:[[Low earth orbit]] | ;LEO:[[Low earth orbit]] | ||
+ | ;LH2:Liquid Hydrogen | ||
+ | ;LOCV: Loss of crew and vehicle | ||
;LOX:Liquid Oxygen | ;LOX:Liquid Oxygen | ||
;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 | ||
Line 160: | Line 180: | ||
;MDR:'''m'''ission '''d'''efinition '''r'''eview | ;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 | ||
+ | ;MET:'''M'''ission '''E'''lapsed '''T'''ime. See [[w:Mission Elapsed Time|Mission Elapsed Time on Wikipedia]]. | ||
;MFD:multifunction display, see [[MFD]] | ;MFD:multifunction display, see [[MFD]] | ||
;MJD:[[modified Julian date]] | ;MJD:[[modified Julian date]] | ||
+ | ;MLP:[[Mobile Launcher Platform]] | ||
+ | ;MMOD:'''M'''icro'''m'''eteorites and '''o'''rbital '''d'''ebris | ||
;MMU:'''m'''anned '''m'''aneuvering '''u'''nit, see [[MMU]] | ;MMU:'''m'''anned '''m'''aneuvering '''u'''nit, see [[MMU]] | ||
;MnA:[[mean anomaly]] | ;MnA:[[mean anomaly]] | ||
Line 168: | Line 191: | ||
;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) | ||
;OBS:[[omni bearing selector]] | ;OBS:[[omni bearing selector]] | ||
;OBT:[[orbit]], as seen on the [[orbit MFD]] | ;OBT:[[orbit]], as seen on the [[orbit MFD]] | ||
− | ;OMS:''' | + | ;OMBUU: '''O'''rbiter '''M'''id'''b'''ody '''U'''mbilical '''U'''nit |
+ | ;[[OMP]]:'''O'''rbiter '''M'''ultiplayer '''P'''roject, an ongoing program to create a multiplayer server in 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 | ||
− | ;PAPI:'''P'''recision '''A'''pproach '''P'''ath '''I'''ndicators, lit runway | + | ;PAM:'''P'''ayload '''A'''ssist '''M'''odule, a family of solid upper stages for the [[Space Shuttle]] |
+ | ;PAPI:'''P'''recision '''A'''pproach '''P'''ath '''I'''ndicators, lit runway centerline. | ||
;PB:[[Shuttle PB]] | ;PB:[[Shuttle PB]] | ||
;PDR:'''p'''reliminary '''d'''esign '''r'''eview | ;PDR:'''p'''reliminary '''d'''esign '''r'''eview | ||
+ | ;PDRS:'''P'''ayload '''D'''eployment and '''R'''etrieval '''S'''ystem, the official name of the robot arm of the Space Shuttle | ||
;PRR:'''p'''reliminary '''r'''equirements '''r'''eview | ;PRR:'''p'''reliminary '''r'''equirements '''r'''eview | ||
− | ;PeA:[[periapsis]] altitude | + | ;PeA:[[periapsis]] altitude. Altitude of periapsis above the surface of the orbited body |
− | ;PeD:[[periapsis]] distance | + | ;PeD:[[periapsis]] distance. See PeR. |
− | ;PeR:[[periapsis]] radius | + | ;PeR:[[periapsis]] radius. Distance of periapsis from the center of the orbited body |
+ | ;PeT:time to [[periapsis]] in seconds. | ||
;PG:[[prograde]] | ;PG:[[prograde]] | ||
;PLT:Pilot | ;PLT:Pilot | ||
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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 | ;QR: '''q'''ualification '''r'''eview | ||
− | + | ||
+ | =R= | ||
;R: | ;R: | ||
#mean radius | #mean radius | ||
Line 206: | Line 238: | ||
#angular unit ''radians'' | #angular unit ''radians'' | ||
;RAnm:[[true anomaly]] of reference axis, as seen on the [[synchronise orbit MFD]] | ;RAnm:[[true anomaly]] of reference axis, as seen on the [[synchronise orbit MFD]] | ||
− | |||
;RCS:[[reaction control system]], spacebourne orientation rocket system. | ;RCS:[[reaction control system]], spacebourne orientation rocket system. | ||
;R&D:'''r'''esearch and '''d'''evelopment | ;R&D:'''r'''esearch and '''d'''evelopment | ||
Line 215: | Line 246: | ||
;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. | |
+ | ;RSLS:'''R'''edundant '''s'''et '''l'''aunch '''s'''equencer, the computer systems responsible for the ignition of the SSMEs in the [[Space Shuttle]] orbiter. | ||
+ | ;RTFM:'''R'''ead '''t'''he '''f'''ine (or many other '''f'''-words) '''m'''anual, a typical forum answer for questions already answered extensivly in the manual. | ||
+ | ;RTLS:'''R'''eturn '''t'''o '''l'''aunch '''s'''ite, a [[Space Shuttle]] abort mode. | ||
+ | |||
+ | =S= | ||
;SAR: | ;SAR: | ||
#'''S'''earch '''a'''nd '''r'''escue. | #'''S'''earch '''a'''nd '''r'''escue. | ||
Line 231: | Line 267: | ||
;SHP:[[ship]], as seen on the [[orbit MFD]] | ;SHP:[[ship]], as seen on the [[orbit MFD]] | ||
;Sh-ToR:ship [[time-on-reference]], as seen on the [[synchronise orbit MFD]] | ;Sh-ToR:ship [[time-on-reference]], as seen on the [[synchronise orbit MFD]] | ||
+ | ;SI unit: The metric system of measurement, the modern name, see [[SI unit]] | ||
;SLF:shuttle landing facility, see [[Cape Canaveral]] | ;SLF:shuttle landing facility, see [[Cape Canaveral]] | ||
;SMa:[[semi-major axis]] | ;SMa:[[semi-major axis]] | ||
Line 242: | Line 279: | ||
;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]] | ||
;T:orbit period, measured in seconds | ;T:orbit period, measured in seconds | ||
;TAS:true air speed [http://en.wikipedia.org/wiki/True_air_speed] | ;TAS:true air speed [http://en.wikipedia.org/wiki/True_air_speed] | ||
+ | ;TAEM:Terminal Area Energy Management | ||
+ | ;TEI:'''T'''rans '''E'''arth '''I'''njection[http://en.wikipedia.org/wiki/Trans_Earth_Injection] | ||
;TKS:russian spacecraft for the Almaz program, see [[TKS]] | ;TKS:russian spacecraft for the Almaz program, see [[TKS]] | ||
;TLA:Three letter acronym for a '''t'''hree '''l'''etter '''a'''cronym. | ;TLA:Three letter acronym for a '''t'''hree '''l'''etter '''a'''cronym. | ||
Line 263: | Line 302: | ||
;TVEL:tangential [[velocity]] | ;TVEL:tangential [[velocity]] | ||
− | ==U | + | =U= |
− | ;UNKS: | + | ;UMMU:'''U'''niversal '''m'''anned '''m'''aneuvering '''u'''nit, popular add-on, see [[Universal MMU]]. |
− | ;UNK-UNKS:unknown | + | ;UNKS:unknown problems, you are aware of. |
+ | ;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 275: | Line 316: | ||
;VOR:[[very high frequency omnidirectional radio]] | ;VOR:[[very high frequency omnidirectional radio]] | ||
;VS:vertical speed | ;VS:vertical speed | ||
+ | ;VSA: [[Virtual Space Agency]] | ||
;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}} | ||
+ | |||
+ | [[Category: Articles]] | ||
+ | [[Category:Glossary]] |
Latest revision as of 13:40, 8 April 2024
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 Add-on 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[edit]
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[edit]
- AgP
- Argument of periapsis:The angle in the orbit from the point of the ascending node to the point of periapsis, Used in OrbitMFD.
- AN
- ascending node:a vector in an orbit where the body passes from south to north of the plane of reference (i.e. ecliptic or equatorial). Shown in OrbitMFD as a dotted vector line connecting to a solid square on the orbit.
- ApA
- apoapsis apoapsis altitude
- ApD
- apoapsis apoapsis distance
- ApR
- apoapsis 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
- ATV
B[edit]
- BMW
- Bate, Mueller, White - authors of Fundamentals of Astrodynamics (1971)
C[edit]
- 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
- COAS
- Crew Optical Alignment Sight
- COM
- communication or communicator
- CTD
- crash to desktop
- CTRL
- Control
- CTV
- Crew Transfer Vehicle, a manned spacecraft derived from the ATV, see CTV
- Compatibility Test Van, NASA
- CVEL
- closing velocity
- Common Vessel Extensions Light, see CVEL
D[edit]
- D3D9
- refers to the advanced graphics client in Orbiter.
- DN
- descending node
- DDT&E
- design, development, test and evaluation
- DG
- Delta-glider
- DGIII
- DeltagliderIII, a famous enhanced version of the Delta-glider.
- DGIV
- DeltaGliderIV, an improved version of the DeltaGliderIII.
- 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
- DPS
- Data Processing System. Term describing the general purpose computers and their interfaces onboard various manned spacecraft.
- 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[edit]
- Ecc
- eccentricity
- ECL
- plane of the ecliptic
- ECSS
- european cooperation for space standardization
- ECLSS
- Environmental control and life support system
- 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[edit]
- 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
- FRF
- Flight Readiness Firing, a launch countdown test of the Shuttle running all except SRB ignition and lift-off.
G[edit]
- 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
- GET
- Ground Elapsed Time [2]
- GLOC
- Gravity-induced Loss of Consciousness
- GMT
- Greenwich Mean Time.See Universal Time on Wikipedia
- GPDS
- Generic Payload Description System
- GPS
- Global Positioning System
- GS
- ground speed
- GTO
- geostationary transfer orbit
H[edit]
- 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[edit]
- IAS
- indicated air speed [3]
- IDS
- instrument docking system
- ILS
- instrument landing system
- International launch services, a US-russian joint venture marketing Atlas and Proton launches
- Inc
- Inclination (http://en.wikipedia.org/wiki/Inclination)
- ISP
- specific impulse
- ISS
- International Space Station
J[edit]
- JD
- Julian date
- JWST
- James Webb Space Telescope
- JSC
- Lyndon B. Johnson Space Center
K[edit]
- KISS
- "Keep it simple, stupid!" Famous engineering dogma.[4]
- KSC
- Kennedy Space Center
L[edit]
- 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
- LH2
- Liquid Hydrogen
- LOCV
- Loss of crew and vehicle
- LOX
- Liquid Oxygen
- LPe
- longitude of periapsis
M[edit]
- 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
- MET
- Mission Elapsed Time. See Mission Elapsed Time on Wikipedia.
- MFD
- multifunction display, see MFD
- MJD
- modified Julian date
- MLP
- Mobile Launcher Platform
- MMOD
- Micrometeorites and orbital debris
- 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[edit]
- NAV
- navigation
- navigation aid
O[edit]
- 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
- OMBUU
- Orbiter Midbody Umbilical Unit
- OMP
- Orbiter Multiplayer Project, an ongoing program to create a multiplayer server in Orbiter.
- OMS
- Orbital Maneuvering System, the 'main engines' of the space shuttle orbiter
- OS
- orbital speed
P[edit]
- P
- position (sometimes radius) vector, as seen on the align orbital plane MFD
- p0
- atmospheric pressure at sea level
- PAM
- Payload Assist Module, a family of solid upper stages for the Space Shuttle
- PAPI
- Precision Approach Path Indicators, lit runway centerline.
- PB
- Shuttle PB
- PDR
- preliminary design review
- PDRS
- Payload Deployment and Retrieval System, the official name of the robot arm of the Space Shuttle
- PRR
- preliminary requirements review
- PeA
- periapsis altitude. Altitude of periapsis above the surface of the orbited body
- PeD
- periapsis distance. See PeR.
- PeR
- periapsis radius. Distance of periapsis from the center of the orbited body
- PeT
- time to periapsis in seconds.
- 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[edit]
- QR
- qualification review
R[edit]
- 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
- 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.
- RSLS
- Redundant set launch sequencer, the computer systems responsible for the ignition of the SSMEs in the Space Shuttle orbiter.
- RTFM
- Read the fine (or many other f-words) manual, a typical forum answer for questions already answered extensivly in the manual.
- RTLS
- Return to launch site, a Space Shuttle abort mode.
S[edit]
- 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 [5]
- 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
- SI unit
- The metric system of measurement, the modern name, see SI unit
- SLF
- shuttle landing facility, see Cape Canaveral
- SMa
- semi-major axis
- SSME
- Space Shuttle Main Engines [6]
- SMi
- semi-minor axis
- SRB
- Solid Rocket Booster [7]
- 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[edit]
- 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 [8]
- TAEM
- Terminal Area Energy Management
- TEI
- Trans Earth Injection[9]
- 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[edit]
- UMMU
- Universal manned maneuvering unit, popular add-on, see Universal MMU.
- 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[edit]
- 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
- VSA
- Virtual Space Agency
- VTOL
- Vertical Take Off and Landing
W[edit]
- WBS
- work breakdown structure
- WPD
- work package description
- Wrp
- time acceleration factor, seen in the general information display
X[edit]
- XPDR
- transponder
Y[edit]
- YSC
- Yokohama Science Center
Z[edit]
- ZM
- zoom, as seen on the map MFD
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