Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:firstFlight |
1988
|
| gptkbp:fuelType |
UDMH
|
| gptkbp:gimbalRange |
±55°
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-869
|
| gptkbp:manufacturer |
gptkb:Yuzhnoye_Design_Bureau
|
| gptkbp:oxidizer |
N2O4
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
315 s
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
40 kN
|
| gptkbp:usedIn |
R-36M2 missile
|
| gptkbp:bfsParent |
gptkb:Dnepr_launch_vehicle
|
| gptkbp:bfsLayer |
7
|