Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:culturalHeritage |
derived from AJ10 family
|
| 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 |
AJ10-118K engine
|
| gptkbp:length |
1.56 m
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:restartable |
yes
|
| gptkbp:specificImpulseVacuum |
319 seconds
|
| gptkbp:thrustVacuum |
43.4 kN
|
| gptkbp:usedBy |
gptkb:NASA
|
| gptkbp:usedFor |
gptkb:satellite
|
| gptkbp:usedIn |
gptkb:Apollo_Service_Module
gptkb:Apollo_spacecraft |
| gptkbp:weight |
281 kg
|
| gptkbp:bfsParent |
gptkb:Delta_II_7925-9.5
gptkb:Delta_II_7425-10 |
| gptkbp:bfsLayer |
6
|