Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:derivedFrom |
gptkb:H-1_rocket_engine
|
| gptkbp:diameter |
1.07 m
|
| gptkbp:firstFlight |
1974
|
| gptkbp:fuelType |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
RS-27
|
| gptkbp:length |
3.86 m
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
255 s
302 s |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:RS-27A
|
| gptkbp:thrustSeaLevel |
890 kN
|
| gptkbp:thrustVacuum |
971 kN
|
| gptkbp:usedIn |
gptkb:Delta_2000_series
gptkb:Delta_3000_series gptkb:Delta_5000_series |
| gptkbp:weight |
1,010 kg
|
| gptkbp:bfsParent |
gptkb:Delta_II
|
| gptkbp:bfsLayer |
5
|