Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:burnTime |
280 seconds
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
0.25 m
|
| gptkbp:firstFlight |
1957
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:length |
1.2 m
|
| gptkbp:manufacturer |
gptkb:Reaction_Motors
|
| gptkbp:numberBuilt |
over 500
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:purpose |
vernier engine
|
| gptkbp:status |
retired
|
| gptkbp:thrustVacuum |
3.4 kN
|
| gptkbp:usedFor |
fine trajectory adjustments
roll control thrust vector control |
| gptkbp:usedIn |
gptkb:satellite
gptkb:Titan_rocket |
| gptkbp:bfsParent |
gptkb:Rocketdyne
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
LR101 rocket engine
|