Editing List of Acronyms and Abbreviations
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=A= | =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. | |
− | + | ;Alt:[[altitude]], distance from the body surface | |
− | ;AgP:[[Argument of periapsis]]:The angle in the orbit from the point of the ascending node to the point of periapsis, | + | ;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 [[Orbit MFD]] as a dotted vector line connecting to a solid square on the orbit. |
− | ; | ||
− | |||
− | |||
− | ;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 | ||
− | |||
− | |||
;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]]. | ||
− | + | ;ApA:[[apoapsis]] apoapsis altitude, the lowest altitude of an orbit. Used in OrbitMFD mode. | |
− | ;ApA:[[apoapsis]] apoapsis altitude, the lowest altitude of an orbit | ||
;ApD:[[apoapsis]] apoapsis distance | ;ApD:[[apoapsis]] apoapsis distance | ||
− | ;ApR:[[apoapsis]] apoapsis radius | + | ;ApR:[[apoapsis]] apoapsis radius |
− | ;ApT:time to [[apoapsis]] in seconds | + | ;ApT:time to [[apoapsis]] in seconds |
− | ;AR: | + | ;AR:'''a'''cceptance '''r'''eview |
− | |||
− | |||
− | |||
;atmo:[[atmosphere]] | ;atmo:[[atmosphere]] | ||
− | |||
;ATV: | ;ATV: | ||
#'''A'''utonomous '''T'''ransfer '''V'''ehicle, an unmanned cargo spacecraft, see [[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] | #'''A'''utomated '''T'''ransfer '''V'''ehicle[http://www.orbiterwiki.org/wiki/ATV#The_ATV] | ||
;AU:[[astronomical unit]] | ;AU:[[astronomical unit]] | ||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=B= | =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) | ||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
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;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 | ||
− | |||
;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 | ;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 | ||
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#'''C'''rew '''T'''ransfer '''V'''ehicle, a manned spacecraft derived from the [[ATV]], see [[CTV]] | #'''C'''rew '''T'''ransfer '''V'''ehicle, a manned spacecraft derived from the [[ATV]], see [[CTV]] | ||
#'''C'''ompatibility '''T'''est '''V'''an, '''NASA''' | #'''C'''ompatibility '''T'''est '''V'''an, '''NASA''' | ||
− | |||
;CVEL: | ;CVEL: | ||
#[[closing velocity]] | #[[closing velocity]] | ||
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[[#top|Back to top]] | [[#top|Back to top]] | ||
=D= | =D= | ||
− | ;D3D9:refers to the advanced graphics client in [[Orbiter]] | + | ;D3D9:refers to the advanced graphics client in [[Orbiter]]. |
− | |||
− | |||
;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]] | ||
;DG4:Orbiter's stock '''DG''' | ;DG4:Orbiter's stock '''DG''' | ||
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;Dir:'''dir'''ection | ;Dir:'''dir'''ection | ||
;Dist:'''dist'''ance | ;Dist:'''dist'''ance | ||
− | |||
;DIV:[[divergent]], i.e. [[yaw]] [[gimbal]] mode. | ;DIV:[[divergent]], i.e. [[yaw]] [[gimbal]] mode. | ||
− | ;DLng:difference | + | ;DLng:longitude difference, as seen on the [[synchronise orbit MFD]] |
− | ;DN: | + | ;DN:[[descending node]] |
− | + | ;DNP:dynamic [[pressure]] | |
− | + | ;DNS:atmospheric density | |
− | + | ;DPS:'''D'''ata '''P'''rocessing '''S'''ystem. Term describing the general purpose computers and their interfaces onboard various manned spacecraft. | |
− | ;DNP:dynamic [[pressure]] | + | ;DST or Dst:distance (to target) |
− | |||
− | ;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: | ||
− | |||
− | |||
;DTe:time to [[ejection]], as seen on the [[transfer MFD]] | ;DTe:time to [[ejection]], as seen on the [[transfer MFD]] | ||
;DTi:time to intercept, as seen on the [[transfer MFD]] | ;DTi:time to intercept, as seen on the [[transfer MFD]] | ||
− | ;DTmin:time of | + | ;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]] | ;Dv:delta [[velocity]], as seen on the [[transfer MFD]], see also [[Delta-V]] | ||
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=E= | =E= | ||
− | ;Ecc:[[eccentricity | + | ;Ecc:[[eccentricity]] |
;ECL:plane of the [[ecliptic]] | ;ECL:plane of the [[ecliptic]] | ||
;ECLSS:'''E'''nvironmental '''c'''ontrol and '''l'''ife '''s'''upport '''s'''ystem | ;ECLSS:'''E'''nvironmental '''c'''ontrol and '''l'''ife '''s'''upport '''s'''ystem | ||
;ECSS:'''e'''uropean '''c'''ooperation for '''s'''pace '''s'''tandardization | ;ECSS:'''e'''uropean '''c'''ooperation for '''s'''pace '''s'''tandardization | ||
;EELV:Evolved Expendable Launch Vehicle | ;EELV:Evolved Expendable Launch Vehicle | ||
− | |||
− | |||
;EQU:plane of the [[equator]] | ;EQU:plane of the [[equator]] | ||
− | |||
− | |||
;ESA:[[European Space Agency]] | ;ESA:[[European Space Agency]] | ||
;ESAS:[[w:Exploration Systems Architecture Study|Exploration Systems Architecture Study]] | ;ESAS:[[w:Exploration Systems Architecture Study|Exploration Systems Architecture Study]] | ||
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;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. | ;FRF:'''F'''light '''R'''eadiness '''F'''iring, a launch countdown test of the Shuttle running all except SRB ignition and lift-off. | ||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=G= | =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]] | |
− | |||
;GET:'''G'''round '''E'''lapsed '''T'''ime [http://history.nasa.gov/SP-4029/Apollo_00c_Introduction.htm] | ;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 | ;GLOC:'''G'''ravity-induced '''L'''oss '''o'''f '''C'''onsciousness | ||
;GMT:Greenwich Mean Time.See [[w:Universal Time|Universal Time on Wikipedia]] | ;GMT:Greenwich Mean Time.See [[w:Universal Time|Universal Time on Wikipedia]] | ||
− | |||
;GPDS:[[GPDS|Generic Payload Description System]] | ;GPDS:[[GPDS|Generic Payload Description System]] | ||
;GPS:'''G'''lobal '''P'''ositioning '''S'''ystem | ;GPS:'''G'''lobal '''P'''ositioning '''S'''ystem | ||
− | ;GS: [[ | + | ;GS:[[ground speed]] |
− | |||
;GTO:[[GTO|'''g'''eostationary '''t'''ransfer '''o'''rbit]] | ;GTO:[[GTO|'''g'''eostationary '''t'''ransfer '''o'''rbit]] | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
− | |||
=H= | =H= | ||
;H:Horizon | ;H:Horizon | ||
;HAC:[[Heading Alignment Cone]] | ;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]] | ||
;HSI:[[horizontal situation indicator]] | ;HSI:[[horizontal situation indicator]] | ||
;HST:[[Hubble Space Telescope]] | ;HST:[[Hubble Space Telescope]] | ||
;HTO:[[hypothetical transfer orbit]], as seen on the [[transfer MFD]] | ;HTO:[[hypothetical transfer orbit]], as seen on the [[transfer MFD]] | ||
− | ;HUD:[[heads up display]] | + | ;HUD:[[heads up display]] |
[[#top|Back to top]] | [[#top|Back to top]] | ||
− | |||
=I= | =I= | ||
− | ;IAS:indicated air speed [ | + | ;IAS:indicated air speed [http://en.wikipedia.org/wiki/Indicated_air_speed] |
− | + | ;IDS:[[instrument docking system]] | |
− | ;IDS:[[ | ||
;ILS: | ;ILS: | ||
#[[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: | + | ;Inc:Inclination (http://en.wikipedia.org/wiki/Inclination) |
− | |||
;ISP:[[specific impulse]] | ;ISP:[[specific impulse]] | ||
;ISS:[[International Space Station]] | ;ISS:[[International Space Station]] | ||
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=J= | =J= | ||
;JD:[[Julian date]] | ;JD:[[Julian date]] | ||
+ | ;JWST:'''J'''ames '''W'''ebb '''S'''pace '''T'''elescope | ||
;JSC: Lyndon B. '''J'''ohnson '''S'''pace '''C'''enter | ;JSC: Lyndon B. '''J'''ohnson '''S'''pace '''C'''enter | ||
− | |||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
− | |||
=K= | =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] | ||
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[[#top|Back to top]] | [[#top|Back to top]] | ||
=L= | =L= | ||
− | ;LAN: | + | ;LAN:longitude of [[ascending node]] or local-area network |
− | |||
− | |||
;LCC: | ;LCC: | ||
#'''l'''aunch '''c'''ontrol '''c'''enter | #'''l'''aunch '''c'''ontrol '''c'''enter | ||
#'''l'''ife '''c'''ycle '''c'''ost | #'''l'''ife '''c'''ycle '''c'''ost | ||
;LDEF:[[Long Duration Exposure Facility]] | ;LDEF:[[Long Duration Exposure Facility]] | ||
− | |||
− | |||
;LEO:[[Low earth orbit]] | ;LEO:[[Low earth orbit]] | ||
;LH2:Liquid Hydrogen | ;LH2:Liquid Hydrogen | ||
;LOCV: Loss of crew and vehicle | ;LOCV: Loss of crew and vehicle | ||
;LOX:Liquid Oxygen | ;LOX:Liquid Oxygen | ||
− | ;LPe:longitude of [[periapsis]] | + | ;LPe:longitude of [[periapsis]] |
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=M= | =M= | ||
;m:metre | ;m:metre | ||
− | ;M: | + | ;M:Mega (SI prefix for 10<sup>6</sup>). Occasionally mass or [[mach]] number |
− | |||
− | |||
− | |||
− | |||
;MCC: | ;MCC: | ||
#'''m'''id '''c'''ourse '''c'''orrection | #'''m'''id '''c'''ourse '''c'''orrection | ||
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;MET:'''M'''ission '''E'''lapsed '''T'''ime. See [[w:Mission Elapsed Time|Mission Elapsed Time on Wikipedia]]. | ;MET:'''M'''ission '''E'''lapsed '''T'''ime. See [[w:Mission Elapsed Time|Mission Elapsed Time on Wikipedia]]. | ||
;MFD:'''M'''ulti'''f'''unctional '''D'''isplay, see [[MFD]] | ;MFD:'''M'''ulti'''f'''unctional '''D'''isplay, see [[MFD]] | ||
− | |||
;MJD:[[modified Julian date]] | ;MJD:[[modified Julian date]] | ||
;MLP:[[Mobile Launcher Platform]] | ;MLP:[[Mobile Launcher Platform]] | ||
;MMOD:'''M'''icro'''m'''eteorites and '''o'''rbital '''d'''ebris | ;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]] |
− | ;MnL:[[mean longitude | + | ;MnL:[[mean longitude]] |
− | ; | + | ;MSx:Mission Specialist x |
;m/s:meters per second, the SI base unit of [[velocity]] | ;m/s:meters per second, the SI base unit of [[velocity]] | ||
− | |||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
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=N= | =N= | ||
;NAV: | ;NAV: | ||
− | |||
− | |||
− | |||
− | |||
#navigation | #navigation | ||
#[[navigation aid]] | #[[navigation aid]] | ||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=O= | =O= | ||
− | ;OAT:outside air temperature | + | ;OAT:outside air temperature |
− | ;Ob: | + | ;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]] | ||
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;[[OMP]]:'''O'''rbiter '''M'''ultiplayer '''P'''roject, an ongoing program to create a multiplayer server in Orbiter. | ;[[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 | ;OMS:'''O'''rbital '''M'''aneuvering '''S'''ystem, the 'main engines' of the [[space shuttle]] orbiter | ||
− | ;OS:[[ | + | ;OS:[[orbital speed]] |
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
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;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 | ;PDRS:'''P'''ayload '''D'''eployment and '''R'''etrieval '''S'''ystem, the official name of the robot arm of the Space Shuttle | ||
− | ;PeA:[[periapsis]] altitude. Altitude of periapsis above the surface of the orbited body | + | ;PRR:'''p'''reliminary '''r'''equirements '''r'''eview |
+ | ;PeA:[[periapsis]] altitude. Altitude of periapsis above the surface of the orbited body | ||
;PeD:[[periapsis]] distance. See PeR. | ;PeD:[[periapsis]] distance. See PeR. | ||
− | ;PeR:[[periapsis]] radius. Distance of periapsis from the center of the orbited body | + | ;PeR:[[periapsis]] radius. Distance of periapsis from the center of the orbited body |
− | ;PeT:time to [[periapsis]] in seconds | + | ;PeT:time to [[periapsis]] in seconds. |
− | ;PG: | + | ;PG:[[prograde]] |
− | |||
− | |||
;PLT:Pilot | ;PLT:Pilot | ||
;PMI:'''P'''rincipal '''m'''oments of '''i'''nertia, see [[PMI]] | ;PMI:'''P'''rincipal '''m'''oments of '''i'''nertia, see [[PMI]] | ||
;Pos:position | ;Pos:position | ||
− | ;PRJ: | + | ;PRJ:[[projection]], as seen on the [[orbit MFD]] |
− | |||
;PSx:Payload Specialist x | ;PSx:Payload Specialist x | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
− | |||
=Q= | =Q= | ||
;QR: '''q'''ualification '''r'''eview | ;QR: '''q'''ualification '''r'''eview | ||
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#mean radius | #mean radius | ||
#specific gas constant | #specific gas constant | ||
− | |||
− | |||
− | |||
;r0:atmospheric density at sea level | ;r0:atmospheric density at sea level | ||
;Rad: | ;Rad: | ||
− | |||
#radial distance | #radial distance | ||
#angular unit ''radians'' | #angular unit ''radians'' | ||
− | ;RAnm:[[true anomaly]] of reference axis, | + | ;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 | ||
;RDT&E:'''r'''esearch, '''d'''evelopment, '''t'''esting and '''e'''valuation | ;RDT&E:'''r'''esearch, '''d'''evelopment, '''t'''esting and '''e'''valuation | ||
− | ;REF: '''Reference''' | + | ;REF: '''Reference''', used in Align MFD to select a reference body. |
− | + | ;RInc:[[relative inclination]], as seen on the [[align orbital plane MFD]] | |
− | + | ;RVel:relative [[velocity]] | |
;RG:[[retrograde]] | ;RG:[[retrograde]] | ||
− | |||
;RKA:Russian Space Agency | ;RKA:Russian Space Agency | ||
;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ||
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;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. | ;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. | ;RTLS:'''R'''eturn '''t'''o '''l'''aunch '''s'''ite, a [[Space Shuttle]] abort mode. | ||
− | |||
− | |||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
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#'''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]] | ;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]] | ||
+ | ;SDHLV:'''S'''huttle '''D'''erived '''H'''eavy '''L'''aunch '''V'''ehicle, see [[Ares V]] | ||
;SECO: | ;SECO: | ||
#'''S'''econdary '''E'''ngine '''C'''ut'''o'''ff | #'''S'''econdary '''E'''ngine '''C'''ut'''o'''ff | ||
#'''S'''ustainer '''E'''ngine '''C'''ut'''o'''ff | #'''S'''ustainer '''E'''ngine '''C'''ut'''o'''ff | ||
− | |||
− | |||
;Sim: | ;Sim: | ||
#simulation time (in seconds), as seen in the [[general information display]] | #simulation time (in seconds), as seen in the [[general information display]] | ||
#a common abbreviation for "simulator" | #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]] | ;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]] | ;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]] |
− | ;SMi:[[semi-minor 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] | ;SRB:'''S'''olid '''R'''ocket '''B'''ooster [http://en.wikipedia.org/wiki/Solid_rocket_booster] | ||
;SRTM:'''S'''huttle '''r'''adar '''t'''opography '''m'''ission, see [[SRTM]]. | ;SRTM:'''S'''huttle '''r'''adar '''t'''opography '''m'''ission, see [[SRTM]]. | ||
− | |||
;SSTO:[[Single_Stage_To_Orbit | Single Stage to Orbit]] | ;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. | ;STOVL:Short take-off, vertical landing. As performed by the DG on full fuel employing hover thrusters during takeoff. | ||
− | ;STP:static [[pressure]] | + | ;STP:static [[pressure]] |
− | |||
;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]] | ||
− | |||
[[#top|Back to top]] | [[#top|Back to top]] | ||
− | |||
=T= | =T= | ||
− | + | ;Tgt:target, esp. in [[docking]] mode | |
− | ;T:orbit period, measured in seconds | + | ;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] | ||
;TAEM:Terminal Area Energy Management | ;TAEM:Terminal Area Energy Management | ||
− | |||
− | |||
;TEI:'''T'''rans '''E'''arth '''I'''njection[http://en.wikipedia.org/wiki/Trans_Earth_Injection] | ;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. | ||
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;TLi:intercept longitude, as seen on the [[transfer MFD]] | ;TLi:intercept longitude, as seen on the [[transfer MFD]] | ||
;TLI:Trans Lunar Injection | ;TLI:Trans Lunar Injection | ||
− | ;Tn: | + | ;Tn:time to node, as seen on the [[align orbital plane MFD]] |
;TOFS:tangential offset [[docking MFD]] | ;TOFS:tangential offset [[docking MFD]] | ||
− | + | ;TrA:[[true anomaly]] | |
− | ;TrA:[[true anomaly | + | ;TRK:Track ship, as displayed by [[map MFD]] |
− | ;TRK:Track, | + | ;TrL:[[true longitude]] |
− | ;TrL:[[true longitude | ||
;TRL:'''t'''echnology '''r'''eadiness '''l'''evel | ;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]] |
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;TVEL:tangential [[velocity]] | ;TVEL:tangential [[velocity]] | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
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=U= | =U= | ||
;UMMU:'''U'''niversal '''m'''anned '''m'''aneuvering '''u'''nit, popular add-on, see [[Universal MMU]]. | ;UMMU:'''U'''niversal '''m'''anned '''m'''aneuvering '''u'''nit, popular add-on, see [[Universal MMU]]. | ||
;UNKS:unknown problems, you are aware of. | ;UNKS:unknown problems, you are aware of. | ||
;UNK-UNKS:unknown problems, you are not aware of. | ;UNK-UNKS:unknown problems, you are not aware of. | ||
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;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. | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=V= | =V= | ||
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;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: | ||
#virtual cockpit | #virtual cockpit | ||
#Visual C++, an IDE and C++ compiler by Microsoft. | #Visual C++, an IDE and C++ compiler by Microsoft. | ||
− | ;Vel:[[velocity | + | ;Vel:[[velocity]] |
− | ;VOR: | + | ;VOR:[[very high frequency omnidirectional radio]] |
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− | |||
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;VS:vertical speed | ;VS:vertical speed | ||
− | |||
;VSA: [[Virtual Space Agency]] | ;VSA: [[Virtual Space Agency]] | ||
− | |||
;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ;VTOL:'''V'''ertical '''T'''ake '''O'''ff and '''L'''anding | ||
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[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 457: | Line 353: | ||
;Wrp:time acceleration factor, seen in the [[general information display]] | ;Wrp:time acceleration factor, seen in the [[general information display]] | ||
=X= | =X= | ||
− | ;XPDR:[[transponder | + | ;XPDR:[[transponder]] |
=Y= | =Y= | ||
;YSC:Yokohama Science Center | ;YSC:Yokohama Science Center | ||
=Z= | =Z= | ||
− | ;ZM | + | ;ZM:zoom, as seen on the [[map MFD]] |
[[#top|Back to top]] | [[#top|Back to top]] |