|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:associatedWith
|
gptkb:International_Space_Station
|
|
gptkbp:collaboratedWith
|
international space agencies
|
|
gptkbp:composedOf
|
two engines
|
|
gptkbp:contributedTo
|
scientific research
|
|
gptkbp:controls
|
digital
|
|
gptkbp:crewCapacity
|
7
|
|
gptkbp:decommissioned
|
2011
|
|
gptkbp:designedBy
|
gptkb:Rockwell_International
|
|
gptkbp:designedFor
|
Space Shuttle
|
|
gptkbp:developedBy
|
NASA
|
|
gptkbp:enables
|
satellite deployment
|
|
gptkbp:engine
|
2
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:facilitates
|
space station construction
|
|
gptkbp:firstFlight
|
1981
2011
|
|
gptkbp:firstHeld
|
gptkb:STS-1
STS-135
|
|
gptkbp:fuelType
|
hypergolic propellants
|
|
gptkbp:hasAuthorityOver
|
pitch, yaw, roll
|
|
gptkbp:height
|
1.5 m
|
|
gptkbp:historicalSignificance
|
pioneered reusable spacecraft technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Shuttle Orbital Maneuvering System
|
|
gptkbp:influencedBy
|
gptkb:Apollo_program
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
2,000 kg
100,000 kg
|
|
gptkbp:launchVehicle
|
Space Shuttle
|
|
gptkbp:legacy
|
influenced future spacecraft designs
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:missileSystem
|
1,000 kg
|
|
gptkbp:mission
|
crew missions
|
|
gptkbp:missions
|
up to 14 days
|
|
gptkbp:numberOfFigures
|
135
|
|
gptkbp:operatedBy
|
NASA
|
|
gptkbp:operationalArea
|
spacecraft maneuvering
|
|
gptkbp:operationalStatus
|
retired
1981-2011
up to 600 km
low_Earth_orbit
|
|
gptkbp:payloadCapacity
|
24,000 kg
|
|
gptkbp:primaryFunction
|
deorbit
orbit insertion
|
|
gptkbp:propulsion
|
1.2
1800 lbf
|
|
gptkbp:provides
|
inertial navigation
crew transport
|
|
gptkbp:replacedBy
|
gptkb:Space_Launch_System
|
|
gptkbp:safetyFeatures
|
high
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:supported
|
Hubble_Space_Telescope_missions
|
|
gptkbp:usedFor
|
orbital maneuvers
|
|
gptkbp:usedIn
|
gptkb:STS_missions
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:width
|
1.5 m
|