Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
240 s
|
| gptkbp:chamber |
1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
1.58 m
|
| gptkbp:firstFlight |
1963
|
| gptkbp:fuelType |
unsymmetrical dimethylhydrazine
|
| gptkbp:gimbalRange |
±3°
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-0110
|
| gptkbp:length |
2.4 m
|
| gptkbp:manufacturer |
KBKhA
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
326 s
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
297 kN
|
| gptkbp:usedFor |
upper stage
|
| gptkbp:usedIn |
gptkb:Soyuz-FG
gptkb:Soyuz_rocket gptkb:Molniya_rocket gptkb:Soyuz-2.1a gptkb:Soyuz-U gptkb:Vostok-2M gptkb:Voskhod_rocket |
| gptkbp:weight |
408 kg
|
| gptkbp:bfsParent |
gptkb:Molniya_8K78
|
| gptkbp:bfsLayer |
7
|