Difference between revisions of "List of Acronyms and Abbreviations"
(→E: Alphabetized terms.) |
(Added terms.) |
||
(12 intermediate revisions by the same user not shown) | |||
Line 41: | Line 41: | ||
=A= | =A= | ||
− | ;AgP:[[Argument of periapsis]]:The angle in the orbit from the point of the ascending node to the point of periapsis, | + | ;ACC: Acceleration, used in [[Surface MFD]] to indicate increasing or decereasing horizontal speed of the ship in m/s<sup>2</sup> |
− | ;Alt:[[altitude]], distance from the body surface | + | ;ACT: Activate, command button in [[RCS attitude MFD]] in docking mode to activate the programmed orientation to the target dock |
− | ;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. | + | ;AgP:[[Argument of periapsis]]:The angle in the orbit from the point of the ascending node to the point of periapsis, displayed in [[Orbit MFD]] |
+ | ;ALT or Alt:[[altitude]], distance from the body surface | ||
+ | #Used in [[Orbit MFD]] when Alt mode is selected to indicate distance from the surface of the body | ||
+ | #Used in [[Surface MFD]] to indicate altitude in km from the body surface | ||
+ | ;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 [[Align MFD]] and [[Orbit MFD]] as a dotted vector line connecting to a solid square on the orbit. | ||
+ | ;AOA: Angle of attack, the difference between the ship's direction of travel and the pitch of its nose | ||
+ | #Used in [[Surface MFD]] to indicate the angle of attack | ||
;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 | + | ;AP: Used in [[Surface MFD]], a red rectangle with white "AP" in the altitude tape to indicate the altitude of the ship's apoapsis |
+ | ;ApA:[[apoapsis]] apoapsis altitude, the lowest altitude of an orbit, displayed in [[Orbit MFD]]. | ||
;ApD:[[apoapsis]] apoapsis distance | ;ApD:[[apoapsis]] apoapsis distance | ||
− | ;ApR:[[apoapsis]] apoapsis radius | + | ;ApR:[[apoapsis]] apoapsis radius, displayed in [[Orbit MFD]] |
− | ;ApT:time to [[apoapsis]] in seconds | + | ;ApT:time to [[apoapsis]] in seconds, displayed in [[Orbit MFD]] |
− | ;AR:'''a'''cceptance '''r'''eview | + | ;AR: |
+ | #'''A'''utomatic '''R'''eference, used in [[Align MFD]], [[Orbit MFD]] as a command button for Align to select a reference body automatically based on highest gravity | ||
+ | #'''A'''ltitude '''R'''ange, used to manually set the range in the altitude graph in [[Ascent profile MFD]] | ||
+ | #'''a'''cceptance '''r'''eview | ||
;atmo:[[atmosphere]] | ;atmo:[[atmosphere]] | ||
;ATV: | ;ATV: | ||
Line 55: | Line 65: | ||
#'''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]] | ||
+ | ;AX: '''Ax'''is, command button in [[RCS attitude MFD]] to change the selected axis beetween pitch/yaw/roll | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=B= | =B= | ||
+ | ;BAS: Basemode, command button to select programmed attitude (prograde, orbit normal, perpendicular in, radial down) in [[RCS attitude MFD]] | ||
;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) | ||
+ | ;BRG: '''B'''ea'''r'''in'''g''', used in the [[Horizontal Situation Indicator MFD]] to indicate the compass direction of the ILS or VOR transmitter | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 70: | Line 83: | ||
;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 | ||
+ | ;CFG: command button in [[RCS attitude MFD]] to switch to configuration page | ||
;CLV:'''C'''rew '''l'''aunch '''v'''ehicle, see [[Ares I]] | ;CLV:'''C'''rew '''l'''aunch '''v'''ehicle, see [[Ares I]] | ||
+ | ;CNC: Cancel, used in [[RCS attitude MFD]] in the docking mode to cancel the docking mode program | ||
;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 | ||
+ | ;CRS: '''C'''ou'''rs'''e, indicates the ship's course (heading) in the [[Horizontal Situation Indicator MFD]] | ||
;CTD:[[crash to desktop]] | ;CTD:[[crash to desktop]] | ||
;CTRL:Control | ;CTRL:Control | ||
Line 78: | Line 94: | ||
#'''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''' | ||
+ | ;CUR: Command button in [[RCS attitude MFD]] to set the programmed attitude to the current attitude | ||
;CVEL: | ;CVEL: | ||
#[[closing velocity]] | #[[closing velocity]] | ||
Line 84: | Line 101: | ||
[[#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]] |
+ | ;Da: Deviation, displayed in [[RCS attitude MFD]] to indicate how many degrees the ship has to go in Roll to reach programmed attitude | ||
+ | ;DCK: command button in [[RCS attitude MFD]] to set the MFD into Docking mode | ||
;DDT&E:'''d'''esign, '''d'''evelopment, '''t'''est and '''e'''valuation | ;DDT&E:'''d'''esign, '''d'''evelopment, '''t'''est and '''e'''valuation | ||
+ | ;DEV:'''Dev'''iation, in the [[Horizontal Situation Indicator MFD]], it indicates how far the OBS is adjusted left or right of the radial | ||
;DG:[[Delta-glider]] | ;DG:[[Delta-glider]] | ||
;DG4:Orbiter's stock '''DG''' | ;DG4:Orbiter's stock '''DG''' | ||
Line 95: | Line 115: | ||
;DIV:[[divergent]], i.e. [[yaw]] [[gimbal]] mode. | ;DIV:[[divergent]], i.e. [[yaw]] [[gimbal]] mode. | ||
;DLng:longitude difference, as seen on the [[synchronise orbit MFD]] | ;DLng:longitude difference, as seen on the [[synchronise orbit MFD]] | ||
− | ;DN:[[descending node]] | + | ;DN: |
+ | #'''Down''', used in [[Map MFD]] when Tracking mode is off and map zoomed in to scroll the map down so you can see farther South | ||
+ | # Command button in [[RCS attitude MFD]] to change the selected modification up so you can edit it | ||
+ | #[[descending node]] | ||
;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 | + | ;DPS:'''D'''ata '''P'''rocessing '''S'''ystem. Term describing the general purpose computers and their interfaces onboard various manned spacecraft |
− | ;DST or Dst: | + | ;Dr: Deviation, displayed in [[RCS attitude MFD]] to indicate how many degrees until the ship reaches pitch and yaw alignment with the programmed attitude |
+ | ;DSP: '''D'''i'''sp'''lay, used in [[Map MFD]] to switch between Ground Track Display and Orbital Plane Display | ||
+ | ;DST or Dst: | ||
+ | #Distance (to target), used in the [[Horizontal Situation Indicator MFD]] to indicate distance to the selected ILS or VOR transmitter | ||
+ | #Distance, used in [[Orbit MFD]] to select between Rad, ApR, PeR (distance from body center) and Alt, ApA, PeA (distance from body surface) | ||
;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]] | ||
Line 108: | Line 135: | ||
=E= | =E= | ||
− | ;Ecc:[[eccentricity]] | + | ;Ecc:[[eccentricity]] of orbit, displayed in [[Orbit MFD]] |
;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 | ||
+ | ;ELS: '''EL'''ements, custom '''S'''elect, used in [[Align MFD]] to select a custom orbital elements to which to align | ||
+ | ;END: command button in [[RCS attitude MFD]] to stop the programmed attitude mode | ||
;EQU:plane of the [[equator]] | ;EQU:plane of the [[equator]] | ||
;ESA:[[European Space Agency]] | ;ESA:[[European Space Agency]] | ||
Line 126: | Line 155: | ||
;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. | ||
+ | ;FRM: '''Fr'''a'''m'''e of reference, used in [[Orbit MFD]] to change the orbital display and parameters between Equatorial or Ecliptic | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=G= | =G= | ||
− | ;g: | + | ;G or g: |
+ | #used in [[Orbit MFD]], indicates what fraction of gravity is exerted on the ship by the reference body (0 to 1) | ||
+ | #unit of acceleration. 1g equals the gravity acceleration on earths surface, 9.81 m/s² | ||
+ | ;GET:'''G'''round '''E'''lapsed '''T'''ime [http://history.nasa.gov/SP-4029/Apollo_00c_Introduction.htm] | ||
;GL:Used often as vehicle name prefix for a [[Delta-glider]] | ;GL:Used often as vehicle name prefix for a [[Delta-glider]] | ||
− | |||
;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]] | ||
+ | ;GO: '''Go''', command button in [[RCS attitude MFD]], once the desired orientation and modifications are set, to activate the program | ||
;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: [[w:Ground speed|Ground speed]] |
+ | #Command button in [[Surface MFD]] to set the speed tape to GS | ||
;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 | ||
− | |||
;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]], used in [[Docking MFD]], [[Orbit MFD]], [[Surface MFD]] to copy the current parameters to the HUD |
[[#top|Back to top]] | [[#top|Back to top]] | ||
+ | |||
=I= | =I= | ||
− | ;IAS:indicated air speed [ | + | ;IAS:indicated air speed [[w:Indicated airspeed|Indicated airspeed]] |
− | ;IDS:[[instrument docking system]] | + | #Command button in [[Surface MFD]] to set the speed tape to IAS |
+ | ;IDS:[[IDS|instrument docking system]], used in [[Docking MFD]] | ||
;ILS: | ;ILS: | ||
#[[instrument landing system]] | #[[instrument landing system]] | ||
+ | #also used in [[Horizontal Situation Indicator MFD]] to indicate which runway at which Spaceport is selected by the NAV 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]], angular difference between one orbit with respect to another, usually the ecliptic, equatorial, body orbit, or target orbit, displayed in [[Align MFD]], [[Orbit MFD]] |
+ | ;INV: Inverse, command button in [[RCS attitude MFD]] to change the programmed attitude to the inverse (retrograde, orbit antinormal, perpendicular out, radial up) | ||
;ISP:[[specific impulse]] | ;ISP:[[specific impulse]] | ||
;ISS:[[International Space Station]] | ;ISS:[[International Space Station]] | ||
Line 164: | Line 202: | ||
=J= | =J= | ||
;JD:[[Julian date]] | ;JD:[[Julian date]] | ||
+ | ;JSC: Lyndon B. '''J'''ohnson '''S'''pace '''C'''enter | ||
;JWST:'''J'''ames '''W'''ebb '''S'''pace '''T'''elescope | ;JWST:'''J'''ames '''W'''ebb '''S'''pace '''T'''elescope | ||
− | + | ||
[[#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] | ||
Line 174: | Line 214: | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
=L= | =L= | ||
− | ;LAN: | + | ;LAN: |
+ | #Longitude of the [[ascending node]], used in [[Align MFD]], [[Orbit MFD]] | ||
+ | #local-area network | ||
;LCC: | ;LCC: | ||
#'''l'''aunch '''c'''ontrol '''c'''enter | #'''l'''aunch '''c'''ontrol '''c'''enter | ||
Line 183: | Line 225: | ||
;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]], displayed in [[Orbit MFD]] |
+ | ;L/R:'''L'''eft/'''R'''ight, used in [[Horizontal Situation Indicator MFD]] to switch MFD mode focus to the left or right graphic display | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 198: | Line 241: | ||
;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]] | ||
+ | ;MHz: '''M'''ega'''H'''er'''z''', same as the old term megacycles/second, radio and transponder frequency, used in [[COMNAV 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]], displayed in [[Orbit MFD]] |
− | ;MnL:[[mean longitude]] | + | ;MnL:[[mean longitude]], displayed in [[Orbit MFD]] |
+ | ;MOD: used in [[Orbit MFD]] to cycle the display between parameters only, orbital display only, or both | ||
+ | ;m/s:meters per second, the SI base unit of [[velocity]] | ||
;MSx:Mission Specialist x | ;MSx:Mission Specialist x | ||
− | + | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 211: | Line 257: | ||
=N= | =N= | ||
;NAV: | ;NAV: | ||
+ | #Navigatonal receiver, | ||
+ | ##in [[COMNAV MFD]] it is used to identify up to four receivers in the stack | ||
+ | ##in [[Horizontal Situation Indicator MFD]], it is used to select which receiver an HSI display is tuned to | ||
+ | ##in [[RCS attitude MFD]] command button in Docking mode to slave one of the Nav receivers to this MFD | ||
#navigation | #navigation | ||
#[[navigation aid]] | #[[navigation aid]] | ||
+ | ;NT: '''N'''o '''t'''arget, used in [[Orbit MFD]] to deselect the target | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 218: | Line 269: | ||
;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) | ||
+ | ;OB+ and OB-: '''O'''mni'''B'''earing, used to change the offset of the course arrow to left or right of the beam | ||
;OBS:[[omni bearing selector]] | ;OBS:[[omni bearing selector]] | ||
;OBT:[[orbit]], as seen on the [[orbit MFD]] | ;OBT:[[orbit]], as seen on the [[orbit MFD]] | ||
Line 223: | Line 275: | ||
;[[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:[[w:Orbital speed|Orbital speed]] |
+ | #Command button in [[Surface MFD]] to set the speed tape to OS | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 234: | Line 287: | ||
;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, used in [[Orbit MFD]] | |
− | ;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, used in [[Orbit MFD]] |
− | ;PeT:time to [[periapsis]] in seconds | + | ;PeT:time to [[periapsis]] in seconds, displayed in [[Orbit MFD]] |
− | ;PG:[[prograde]] | + | ;PG: |
+ | #Page, switching displayed pages in an MFD mode, used in [[Align MFD]] | ||
+ | #[[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, used in the [[Orbit MFD]] to switch orbital display between Ecliptic, Equatorial, Ship's orbit, Target orbit |
+ | ;PRR:'''p'''reliminary '''r'''equirements '''r'''eview | ||
;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 | ||
Line 255: | Line 311: | ||
#mean radius | #mean radius | ||
#specific gas constant | #specific gas constant | ||
+ | ;+R and -R: | ||
+ | #+R, command button in [[RCS attitude MFD]] to add a line (pitch, yaw, roll) to the programmed attitude | ||
+ | #-R, command button in [[RCS attitude MFD]] to remove the last line (pitch, yaw, roll) from the list of programmed attitude | ||
;r0:atmospheric density at sea level | ;r0:atmospheric density at sea level | ||
;Rad: | ;Rad: | ||
+ | #Displayed in [[Orbit MFD]] when Radius mode is selected to indicate distance from the center of the body in meters | ||
#radial distance | #radial distance | ||
#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]] | ||
+ | ;Rate: How fast the current orbital plane is changing, degrees per second, used in [[Align 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]], [[Map MFD]], [[Orbit MFD]] to select a reference body. | |
− | |||
;RG:[[retrograde]] | ;RG:[[retrograde]] | ||
+ | ;RInc:[[relative inclination]], relative inclination between the current and target orbits, used in [[Align MFD]] | ||
;RKA:Russian Space Agency | ;RKA:Russian Space Agency | ||
;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ;RMS:'''R'''emote '''M'''anipulator '''S'''ystem | ||
Line 273: | Line 334: | ||
;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. | ||
+ | ;RTN: Return, command button in [[RCS attitude MFD]] to return the display to the Active mode page | ||
+ | ;RVel:relative [[velocity]] | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 281: | Line 344: | ||
#'''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] | + | ;SC< and SC>:'''SC'''an frequency up or down in the currently selected receiver, used in [[COMNAV MFD]] |
+ | ;SDK:Software Development Kit [http://en.wikipedia.org/wiki/SDK] | ||
+ | ;SDHLV:'''S'''huttle '''D'''erived '''H'''eavy '''L'''aunch '''V'''ehicle, see [[Ares V]] | ||
;SDLV:'''S'''huttle '''D'''erived '''L'''aunch '''V'''ehicle, see [[Ares]] | ;SDLV:'''S'''huttle '''D'''erived '''L'''aunch '''V'''ehicle, see [[Ares]] | ||
− | |||
;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 | ||
+ | ;SET: Set, used in [[RCS attitude MFD]] to set the desired attitude | ||
+ | ;SHP: Ship, used in [[Map MFD]] to indicate your ship's name, position, altitude, course of your ship | ||
;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" | ||
− | |||
;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]] | ||
+ | ;SL+ and SL-: '''S'''e'''l'''ect, change which receiver to next or previous receiver to adjust frequency, used in [[COMNAV MFD]] | ||
;SLF:shuttle landing facility, see [[Cape Canaveral]] | ;SLF:shuttle landing facility, see [[Cape Canaveral]] | ||
− | ;SMa:[[semi-major axis]] | + | ;SMa: [[semi-major axis]], used in [[Orbit MFD]] |
− | + | ;SMi:[[semi-minor axis]], used in [[Orbit MFD]] | |
− | ;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]]. | ||
+ | ;SSME:Space Shuttle Main Engines [http://en.wikipedia.org/wiki/SSME_%28rocket_engine%29] | ||
;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]] | ||
+ | ;SUS: command button in [[RCS attitude MFD]] to suspend programmed attitude temporarily | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
+ | |||
=T= | =T= | ||
− | + | ||
− | + | ;T:orbit period, measured in seconds, displayed in [[Orbit MFD]] | |
− | ;T:orbit period, measured in seconds | ||
− | |||
;TAEM:Terminal Area Energy Management | ;TAEM:Terminal Area Energy Management | ||
+ | ;TAS:true air speed [[w:True airspeed|True airspeed]] | ||
+ | #Command button in [[Surface MFD]] to set the speed tape to TAS | ||
;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] | ||
+ | ;TGT:'''T'''ar'''G'''e'''T''' | ||
+ | #command button used in [[Align MFD]], [[Docking MFD]], [[Map MFD]], [[Orbit MFD]] to select a target | ||
+ | #used in the [[Map MFD]] display to indicate target name, position, altitude of the target | ||
+ | ;Tg-ToR:target [[time-on-reference]], as seen on the [[synchronise orbit MFD]] | ||
;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 318: | Line 390: | ||
;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:'''T'''ime to '''n'''ode, used in [[Align MFD]] |
;TOFS:tangential offset [[docking MFD]] | ;TOFS:tangential offset [[docking MFD]] | ||
− | ;TrA:[[true anomaly]] | + | ;TrA:[[true anomaly]], displayed in [[Orbit MFD]] |
− | ;TRK:Track | + | ;TRK:Track, used in [[map MFD]] to keep the ship centered in the map display |
− | ;TrL:[[true longitude]] | + | ;TrL:[[true longitude]], displayed in [[Orbit MFD]] |
;TRL:'''t'''echnology '''r'''eadiness '''l'''evel | ;TRL:'''t'''echnology '''r'''eadiness '''l'''evel | ||
;Ts:length of siderial day | ;Ts:length of siderial day | ||
− | ; | + | ;TthA: Estimated thrust time at the ascending node to align planes, used in [[Align MFD]] |
+ | ;TthD: Estimated thrust time at the descending node to align planes, used in [[Align MFD]] | ||
;TVEL:tangential [[velocity]] | ;TVEL:tangential [[velocity]] | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
+ | |||
=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. | ||
+ | ;UP: | ||
+ | #'''UP''', used in [[Map MFD]] when Track mode is off and map is zoomed in to scroll the map up to see farther North | ||
+ | #Command button in [[RCS attitude MFD]] to change the selected modification up so you can edit it | ||
;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= | ||
+ | ;+V and -V: Used in [[RCS attitude MFD]] to add or subtract one degree each click the programmed attitude mode | ||
;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]], displayed in [[Orbit MFD]] |
− | ;VOR:[[very high frequency omnidirectional radio]] | + | ;VOR: |
+ | #[[very high frequency omnidirectional radio]] | ||
+ | # used in the [[Horizontal Situation Indicator MFD]] to indicate which VOR transmitter is selected by a NAV radio, if it's selected to a VOR transmitter | ||
+ | ;VRR: '''V'''elocity '''R'''adial '''R'''ange, used to manually set the range in the Radial Velocity graph in [[Ascent profile MFD]] | ||
;VS:vertical speed | ;VS:vertical speed | ||
+ | #Used in [[Surface MFD]] to indicate rate of ascent or descent in meters per second | ||
;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 | ||
+ | ;VTR: '''V'''elocity '''T'''angential '''R'''ange, used to manually set the range in the Tangential Velocity Range graph in [[Ascent profile MFD]] | ||
[[#top|Back to top]] | [[#top|Back to top]] | ||
Line 353: | Line 436: | ||
;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]], used in [[Docking MFD]] |
=Y= | =Y= | ||
;YSC:Yokohama Science Center | ;YSC:Yokohama Science Center | ||
=Z= | =Z= | ||
− | ;ZM:zoom, | + | ;ZM+ and ZM-: zoom,used in [[Map MFD]] to zoom the map display in and out |
[[#top|Back to top]] | [[#top|Back to top]] |
Revision as of 14:23, 21 December 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
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
- ACC
- Acceleration, used in Surface MFD to indicate increasing or decereasing horizontal speed of the ship in m/s2
- ACT
- Activate, command button in RCS attitude MFD in docking mode to activate the programmed orientation to the target dock
- AgP
- Argument of periapsis:The angle in the orbit from the point of the ascending node to the point of periapsis, displayed in Orbit MFD
- ALT or Alt
- altitude, distance from the body surface
- Used in Orbit MFD when Alt mode is selected to indicate distance from the surface of the body
- Used in Surface MFD to indicate altitude in km from the body surface
- 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 Align MFD and Orbit MFD as a dotted vector line connecting to a solid square on the orbit.
- AOA
- Angle of attack, the difference between the ship's direction of travel and the pitch of its nose
- Used in Surface MFD to indicate the angle of attack
- AORP
- Autonomous Orbiter Rapid Prototype, a system to allow a shuttle orbiter to land without crew.
- AP
- Used in Surface MFD, a red rectangle with white "AP" in the altitude tape to indicate the altitude of the ship's apoapsis
- ApA
- apoapsis apoapsis altitude, the lowest altitude of an orbit, displayed in Orbit MFD.
- ApD
- apoapsis apoapsis distance
- ApR
- apoapsis apoapsis radius, displayed in Orbit MFD
- ApT
- time to apoapsis in seconds, displayed in Orbit MFD
- AR
- Automatic Reference, used in Align MFD, Orbit MFD as a command button for Align to select a reference body automatically based on highest gravity
- Altitude Range, used to manually set the range in the altitude graph in Ascent profile MFD
- acceptance review
- atmo
- atmosphere
- ATV
- AU
- astronomical unit
- AX
- Axis, command button in RCS attitude MFD to change the selected axis beetween pitch/yaw/roll
B
- BAS
- Basemode, command button to select programmed attitude (prograde, orbit normal, perpendicular in, radial down) in RCS attitude MFD
- BMW
- Bate, Mueller, White - authors of Fundamentals of Astrodynamics (1971)
- BRG
- Bearing, used in the Horizontal Situation Indicator MFD to indicate the compass direction of the ILS or VOR transmitter
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
- CFG
- command button in RCS attitude MFD to switch to configuration page
- CLV
- Crew launch vehicle, see Ares I
- CNC
- Cancel, used in RCS attitude MFD in the docking mode to cancel the docking mode program
- COAS
- Crew Optical Alignment Sight
- COM
- communication or communicator
- CRS
- Course, indicates the ship's course (heading) in the Horizontal Situation Indicator MFD
- CTD
- crash to desktop
- CTRL
- Control
- CTV
- Crew Transfer Vehicle, a manned spacecraft derived from the ATV, see CTV
- Compatibility Test Van, NASA
- CUR
- Command button in RCS attitude MFD to set the programmed attitude to the current attitude
- CVEL
- closing velocity
- Common Vessel Extensions Light, see CVEL
D
- D3D9
- refers to the advanced graphics client in Orbiter
- Da
- Deviation, displayed in RCS attitude MFD to indicate how many degrees the ship has to go in Roll to reach programmed attitude
- DCK
- command button in RCS attitude MFD to set the MFD into Docking mode
- DDT&E
- design, development, test and evaluation
- DEV
- Deviation, in the Horizontal Situation Indicator MFD, it indicates how far the OBS is adjusted left or right of the radial
- DG
- Delta-glider
- DG4
- Orbiter's stock DG
- DGIII
- DeltagliderIII, a famous enhanced version of the Delta-glider.
- DGIV
- DeltaGliderIV, an improved version of the DeltaGliderIII.
- DG-S
- Delta-glider equiped with two scramjets.
- Dir
- direction
- Dist
- distance
- DIV
- divergent, i.e. yaw gimbal mode.
- DLng
- longitude difference, as seen on the synchronise orbit MFD
- DN
- Down, used in Map MFD when Tracking mode is off and map zoomed in to scroll the map down so you can see farther South
- Command button in RCS attitude MFD to change the selected modification up so you can edit it
- descending node
- DNP
- dynamic pressure
- DNS
- atmospheric density
- DPS
- Data Processing System. Term describing the general purpose computers and their interfaces onboard various manned spacecraft
- Dr
- Deviation, displayed in RCS attitude MFD to indicate how many degrees until the ship reaches pitch and yaw alignment with the programmed attitude
- DSP
- Display, used in Map MFD to switch between Ground Track Display and Orbital Plane Display
- DST or Dst
- Distance (to target), used in the Horizontal Situation Indicator MFD to indicate distance to the selected ILS or VOR transmitter
- Distance, used in Orbit MFD to select between Rad, ApR, PeR (distance from body center) and Alt, ApA, PeA (distance from body surface)
- 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 of orbit, displayed in Orbit MFD
- ECL
- plane of the ecliptic
- ECLSS
- Environmental control and life support system
- ECSS
- european cooperation for space standardization
- EELV
- Evolved Expendable Launch Vehicle
- ELS
- ELements, custom Select, used in Align MFD to select a custom orbital elements to which to align
- END
- command button in RCS attitude MFD to stop the programmed attitude mode
- EQU
- plane of the equator
- ESA
- European Space Agency
- ESAS
- Exploration Systems Architecture Study
- ET
- external tank
- 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
- FRF
- Flight Readiness Firing, a launch countdown test of the Shuttle running all except SRB ignition and lift-off.
- FRM
- Frame of reference, used in Orbit MFD to change the orbital display and parameters between Equatorial or Ecliptic
G
- G or g
- used in Orbit MFD, indicates what fraction of gravity is exerted on the ship by the reference body (0 to 1)
- unit of acceleration. 1g equals the gravity acceleration on earths surface, 9.81 m/s²
- GET
- Ground Elapsed Time [2]
- GL
- Used often as vehicle name prefix for a Delta-glider
- GLOC
- Gravity-induced Loss of Consciousness
- GMT
- Greenwich Mean Time.See Universal Time on Wikipedia
- GO
- Go, command button in RCS attitude MFD, once the desired orientation and modifications are set, to activate the program
- GPDS
- Generic Payload Description System
- GPS
- Global Positioning System
- GS
- Ground speed
- Command button in Surface MFD to set the speed tape to GS
H
- H
- Horizon
- HAC
- Heading Alignment Cone
- HLLV
- heavy lift launch vehicle
- HSI
- horizontal situation indicator
- HST
- Hubble Space Telescope
- HTO
- hypothetical transfer orbit, as seen on the transfer MFD
- HUD
- heads up display, used in Docking MFD, Orbit MFD, Surface MFD to copy the current parameters to the HUD
I
- IAS
- indicated air speed Indicated airspeed
- Command button in Surface MFD to set the speed tape to IAS
- IDS
- instrument docking system, used in Docking MFD
- ILS
- instrument landing system
- also used in Horizontal Situation Indicator MFD to indicate which runway at which Spaceport is selected by the NAV system
- International launch services, a US-russian joint venture marketing Atlas and Proton launches
- Inc
- Inclination, angular difference between one orbit with respect to another, usually the ecliptic, equatorial, body orbit, or target orbit, displayed in Align MFD, Orbit MFD
- INV
- Inverse, command button in RCS attitude MFD to change the programmed attitude to the inverse (retrograde, orbit antinormal, perpendicular out, radial up)
- ISP
- specific impulse
- ISS
- International Space Station
J
- JD
- Julian date
- JSC
- Lyndon B. Johnson Space Center
- JWST
- James Webb Space Telescope
K
- KISS
- "Keep it simple, stupid!" Famous engineering dogma.[3]
- KSC
- Kennedy Space Center
L
- LAN
- Longitude of the ascending node, used in Align MFD, Orbit MFD
- 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, displayed in Orbit MFD
- L/R
- Left/Right, used in Horizontal Situation Indicator MFD to switch MFD mode focus to the left or right graphic display
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
- MET
- Mission Elapsed Time. See Mission Elapsed Time on Wikipedia.
- MFD
- Multifunctional Display, see MFD
- MHz
- MegaHerz, same as the old term megacycles/second, radio and transponder frequency, used in COMNAV MFD
- MJD
- modified Julian date
- MLP
- Mobile Launcher Platform
- MMOD
- Micrometeorites and orbital debris
- MMU
- manned maneuvering unit, see MMU
- MnA
- mean anomaly, displayed in Orbit MFD
- MnL
- mean longitude, displayed in Orbit MFD
- MOD
- used in Orbit MFD to cycle the display between parameters only, orbital display only, or both
- m/s
- meters per second, the SI base unit of velocity
- MSx
- Mission Specialist x
N
- NAV
- Navigatonal receiver,
- in COMNAV MFD it is used to identify up to four receivers in the stack
- in Horizontal Situation Indicator MFD, it is used to select which receiver an HSI display is tuned to
- in RCS attitude MFD command button in Docking mode to slave one of the Nav receivers to this MFD
- navigation
- navigation aid
- NT
- No target, used in Orbit MFD to deselect the target
O
- OAT
- outside air temperature
- Ob
- obliquity of ecliptic (tilt of axis of rotation against plane of ecliptic)
- OB+ and OB-
- OmniBearing, used to change the offset of the course arrow to left or right of the beam
- 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
- Command button in Surface MFD to set the speed tape to OS
P
- 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
- PeA
- periapsis altitude. Altitude of periapsis above the surface of the orbited body, used in Orbit MFD
- PeD
- periapsis distance. See PeR.
- PeR
- periapsis radius. Distance of periapsis from the center of the orbited body, used in Orbit MFD
- PeT
- time to periapsis in seconds, displayed in Orbit MFD
- PG
- PLT
- Pilot
- PMI
- Principal moments of inertia, see PMI
- Pos
- position
- PRJ
- Projection, used in the Orbit MFD to switch orbital display between Ecliptic, Equatorial, Ship's orbit, Target orbit
- PRR
- preliminary requirements review
- PSx
- Payload Specialist x
Q
- QR
- qualification review
R
- R
- mean radius
- specific gas constant
- +R and -R
- +R, command button in RCS attitude MFD to add a line (pitch, yaw, roll) to the programmed attitude
- -R, command button in RCS attitude MFD to remove the last line (pitch, yaw, roll) from the list of programmed attitude
- r0
- atmospheric density at sea level
- Rad
- Displayed in Orbit MFD when Radius mode is selected to indicate distance from the center of the body in meters
- radial distance
- angular unit radians
- RAnm
- true anomaly of reference axis, as seen on the synchronise orbit MFD
- Rate
- How fast the current orbital plane is changing, degrees per second, used in Align MFD
- RCS
- reaction control system, spacebourne orientation rocket system.
- R&D
- research and development
- RDT&E
- research, development, testing and evaluation
- REF
- Reference
- RG
- retrograde
- RInc
- relative inclination, relative inclination between the current and target orbits, used in Align MFD
- 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.
- RTN
- Return, command button in RCS attitude MFD to return the display to the Active mode page
- RVel
- relative velocity
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
- SC< and SC>
- SCan frequency up or down in the currently selected receiver, used in COMNAV MFD
- SDK
- Software Development Kit [4]
- SDHLV
- Shuttle Derived Heavy Launch Vehicle, see Ares V
- SDLV
- Shuttle Derived Launch Vehicle, see Ares
- SECO
- Secondary Engine Cutoff
- Sustainer Engine Cutoff
- SET
- Set, used in RCS attitude MFD to set the desired attitude
- SHP
- Ship, used in Map MFD to indicate your ship's name, position, altitude, course of your ship
- Sim
- simulation time (in seconds), as seen in the general information display
- a common abbreviation for "simulator"
- 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
- SL+ and SL-
- Select, change which receiver to next or previous receiver to adjust frequency, used in COMNAV MFD
- SLF
- shuttle landing facility, see Cape Canaveral
- SMa
- semi-major axis, used in Orbit MFD
- SMi
- semi-minor axis, used in Orbit MFD
- SRB
- Solid Rocket Booster [5]
- SRTM
- Shuttle radar topography mission, see SRTM.
- SSME
- Space Shuttle Main Engines [6]
- 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
- SUS
- command button in RCS attitude MFD to suspend programmed attitude temporarily
T
- T
- orbit period, measured in seconds, displayed in Orbit MFD
- TAEM
- Terminal Area Energy Management
- TAS
- true air speed True airspeed
- Command button in Surface MFD to set the speed tape to TAS
- TEI
- Trans Earth Injection[7]
- TGT
- TarGeT
- command button used in Align MFD, Docking MFD, Map MFD, Orbit MFD to select a target
- used in the Map MFD display to indicate target name, position, altitude of the target
- Tg-ToR
- target time-on-reference, as seen on the synchronise orbit MFD
- 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, used in Align MFD
- TOFS
- tangential offset docking MFD
- TrA
- true anomaly, displayed in Orbit MFD
- TRK
- Track, used in map MFD to keep the ship centered in the map display
- TrL
- true longitude, displayed in Orbit MFD
- TRL
- technology readiness level
- Ts
- length of siderial day
- TthA
- Estimated thrust time at the ascending node to align planes, used in Align MFD
- TthD
- Estimated thrust time at the descending node to align planes, used in Align MFD
- TVEL
- tangential velocity
U
- 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.
- UP
- UP, used in Map MFD when Track mode is off and map is zoomed in to scroll the map up to see farther North
- Command button in RCS attitude MFD to change the selected modification up so you can edit it
- 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
- +V and -V
- Used in RCS attitude MFD to add or subtract one degree each click the programmed attitude mode
- 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.
- very high frequency omnidirectional radio
- used in the Horizontal Situation Indicator MFD to indicate which VOR transmitter is selected by a NAV radio, if it's selected to a VOR transmitter
- VRR
- Velocity Radial Range, used to manually set the range in the Radial Velocity graph in Ascent profile MFD
- VS
- vertical speed
- Used in Surface MFD to indicate rate of ascent or descent in meters per second
- VSA
- Virtual Space Agency
- VTOL
- Vertical Take Off and Landing
- VTR
- Velocity Tangential Range, used to manually set the range in the Tangential Velocity Range graph in Ascent profile MFD
W
- WBS
- work breakdown structure
- WPD
- work package description
- Wrp
- time acceleration factor, seen in the general information display
X
- XPDR
- transponder, used in Docking MFD
Y
- YSC
- Yokohama Science Center
Z
- ZM+ and ZM-
- zoom,used in Map MFD to zoom the map display in and out
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