Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
two
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
anhydrous ammonia
|
| https://www.w3.org/2000/01/rdf-schema#label |
XLR-25
|
| gptkbp:manufacturer |
gptkb:Reaction_Motors,_Inc.
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
liquid-propellant
|
| gptkbp:thrust |
57,000 lbf
|
| gptkbp:usedBy |
gptkb:NASA
gptkb:US_Air_Force |
| gptkbp:usedIn |
gptkb:X-15_rocket_plane
|
| gptkbp:bfsParent |
gptkb:Aerojet_Rocketdyne_engines
|
| gptkbp:bfsLayer |
7
|