|
gptkbp:instanceOf
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rocket component
|
|
gptkbp:diameter
|
about 3.7 meters (Space Shuttle SRB)
|
|
gptkbp:function
|
provide thrust during launch
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|
https://www.w3.org/2000/01/rdf-schema#label
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Solid rocket boosters
|
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gptkbp:ignition
|
cannot be shut down after ignition
|
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gptkbp:length
|
about 45 meters (Space Shuttle SRB)
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
gptkb:Thiokol
|
|
gptkbp:material
|
steel casing
|
|
gptkbp:propulsion
|
solid propellant
|
|
gptkbp:reusable
|
sometimes reusable
|
|
gptkbp:separationStage
|
jettisoned after burnout
|
|
gptkbp:thrust
|
about 12.5 MN (Space Shuttle SRB)
|
|
gptkbp:usedIn
|
gptkb:Long_March_7A
gptkb:Antares_rocket
gptkb:Minotaur_rocket
gptkb:Ariane_5
gptkb:Epsilon_rocket
gptkb:GSLV_(Geosynchronous_Satellite_Launch_Vehicle)
gptkb:PSLV_(Polar_Satellite_Launch_Vehicle)
gptkb:SLS_(Space_Launch_System)
gptkb:Space_Shuttle
gptkb:Ares_I
gptkb:Ares_V
gptkb:Atlas_III_(as_SRBs)
gptkb:Atlas_V_(as_SRBs)
gptkb:Delta_III_(as_SRBs)
gptkb:Delta_II_(as_SRBs)
gptkb:Delta_IV_(as_SRBs)
gptkb:Delta_IV_Heavy_(as_SRBs)
gptkb:Delta_I_(as_SRBs)
gptkb:Electron_rocket_(Kick_Stage_as_solid_motor)
gptkb:H-IIA_(as_SRBs)
gptkb:H-IIB_(as_SRBs)
gptkb:LVM3_(GSLV_Mk_III)
gptkb:Long_March_6A
gptkb:Soyuz-2.1v_(optional_boosters)
gptkb:Ariane_6
gptkb:Titan_III
gptkb:Titan_IV
gptkb:Long_March_11
gptkb:Long_March_8
gptkb:Vega_C
gptkb:Vega_E
gptkb:Vega_rocket
gptkb:Vulcan_Centaur
Atlas V 401 (as SRBs)
Atlas V 411 (as SRBs)
Atlas V 421 (as SRBs)
Atlas V 431 (as SRBs)
Atlas V 501 (as SRBs)
Atlas V 511 (as SRBs)
Atlas V 521 (as SRBs)
Atlas V 531 (as SRBs)
Atlas V 541 (as SRBs)
Atlas V 551 (as SRBs)
|
|
gptkbp:bfsParent
|
gptkb:SLS
|
|
gptkbp:bfsLayer
|
6
|