Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:diameter |
0.99 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| https://www.w3.org/2000/01/rdf-schema#label |
AJ10-190
|
| gptkbp:length |
1.56 m
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:status |
retired
|
| gptkbp:thrustVacuum |
91 kN
|
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:Apollo_12 gptkb:Apollo_Service_Module gptkb:Apollo_10 gptkb:Apollo_16 gptkb:Apollo_13 gptkb:Apollo_17 gptkb:Apollo_7 gptkb:Apollo_8 gptkb:Apollo_14 gptkb:Apollo_15 gptkb:Apollo_9 Apollo Lunar Module Ascent Stage |
| gptkbp:bfsParent |
gptkb:Orion_spacecraft_service_module_(planned)
gptkb:Orbital_Maneuvering_System |
| gptkbp:bfsLayer |
7
|