Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:combustor_type |
gas-generator cycle
|
| gptkbp:development |
1950s
|
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_type |
liquid oxygen and RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
XLR99-RM-1
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:propulsion |
57,000 lbf
|
| gptkbp:specific_impulse |
290 seconds
|
| gptkbp:used_in |
gptkb:X-15_rocket_plane
|
| gptkbp:weight |
1,500 lb
|
| gptkbp:bfsParent |
gptkb:XLR99_rocket_engine
|
| gptkbp:bfsLayer |
6
|