Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
oxidizer-rich staged combustion
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:firstFlight |
1966
|
| gptkbp:fuelType |
UDMH
|
| gptkbp:gimbalRange |
7 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-264
|
| gptkbp:length |
2.4 m
|
| gptkbp:manufacturer |
gptkb:Energomash
|
| gptkbp:numberOfRooms |
4
|
| gptkbp:oxidizer |
N2O4
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
285 s
301 s |
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
1,040 kN
|
| gptkbp:thrustVacuum |
1,040 kN
|
| gptkbp:usedIn |
gptkb:R-36_ICBM
gptkb:Dnepr_launch_vehicle |
| gptkbp:weight |
1,120 kg
|
| gptkbp:bfsParent |
gptkb:Dnepr_launch_vehicle
|
| gptkbp:bfsLayer |
7
|