Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:diameter |
0.99 m
|
| gptkbp:firstFlight |
1958
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| gptkbp:length |
1.7 m
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:specificImpulseVacuum |
319 s
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
43.4 kN
|
| gptkbp:usedIn |
gptkb:Delta_IV
gptkb:Apollo_Service_Module gptkb:European_Service_Module gptkb:Apollo_CSM gptkb:Delta_III gptkb:Delta_II_second_stage gptkb:Orion_spacecraft gptkb:Saturn_I gptkb:Vanguard_rocket gptkb:Delta_II gptkb:Delta_III_second_stage gptkb:Delta_IV_second_stage gptkb:Space_Shuttle_OMS gptkb:Space_Shuttle_Orbital_Maneuvering_System Saturn I second stage Vanguard second stage |
| gptkbp:weight |
124 kg
|
| gptkbp:bfsParent |
gptkb:Orion_MPCV
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Aerojet Rocketdyne AJ10
|