Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
anhydrous ammonia
|
| gptkbp:manufacturer |
Reaction Motors Inc.
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
57,000 lbf
|
| gptkbp:usedIn |
gptkb:North_American_X-15
gptkb:X-15_rocket_plane |
| gptkbp:bfsParent |
gptkb:Reaction_Motors
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
XLR30 rocket engine
|