Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| https://www.w3.org/2000/01/rdf-schema#label |
AJ10-137
|
| gptkbp:length |
1.56 m
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:specificImpulseVacuum |
314 s
|
| gptkbp:status |
retired
|
| gptkbp:thrustVacuum |
91 kN
|
| gptkbp:usedIn |
gptkb:Apollo_Service_Module
gptkb:Apollo_spacecraft Apollo CSM Service Propulsion System |
| gptkbp:weight |
131 kg
|
| gptkbp:bfsParent |
gptkb:Apollo_Service_Module
|
| gptkbp:bfsLayer |
6
|