gptkbp:instanceOf
|
spacecraft stage
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
gptkbp:diameter
|
1.52 meters
|
gptkbp:engineType
|
gptkb:Bell_8096_engine
|
gptkbp:firstFlight
|
1962
|
gptkbp:guidanceSystem
|
inertial guidance
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agena D
|
gptkbp:length
|
6.3 meters
|
gptkbp:manufacturer
|
gptkb:Lockheed
|
gptkbp:mass
|
7,000 kg
|
gptkbp:notableMission
|
gptkb:Gemini_12
gptkb:Gemini_11
gptkb:Gemini_8
|
gptkbp:predecessor
|
gptkb:Agena_B
|
gptkbp:propulsion
|
inhibited red fuming nitric acid
unsymmetrical dimethylhydrazine
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:satellite
|
gptkbp:thrust
|
71 kN
|
gptkbp:usedAs
|
target vehicle
upper stage
|
gptkbp:usedFor
|
gptkb:satellite
gptkb:Titan_II_rocket
gptkb:Thor_rocket
satellite deployment
orbital rendezvous
|
gptkbp:usedIn
|
gptkb:KH-7_Gambit_reconnaissance_satellites
gptkb:Gemini_program
gptkb:Corona_reconnaissance_satellites
gptkb:KH-9_Hexagon_reconnaissance_satellites
gptkb:KH-8_Gambit_reconnaissance_satellites
|
gptkbp:bfsParent
|
gptkb:Thor-Agena_D
gptkb:Titan_IIIB
gptkb:Thor_Agena_D
gptkb:Titan_IIIB-Agena_D
gptkb:Agena_B
|
gptkbp:bfsLayer
|
7
|