Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:chamber |
4
|
| gptkbp:combustionChamberArrangement |
clustered
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:culturalHeritage |
gptkb:RD-107
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:diameter |
1.58 m
|
| gptkbp:firstFlight |
1957
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:gimbalRange |
±6°
|
| gptkbp:length |
2.8 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:primaryUse |
first stage booster
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
256 s
313 s |
| gptkbp:status |
in service
|
| gptkbp:thrustSeaLevel |
838 kN
|
| gptkbp:thrustVacuum |
1020 kN
|
| gptkbp:usedIn |
gptkb:Soyuz_rocket
gptkb:Molniya_rocket gptkb:R-7_family_rockets gptkb:Soyuz-2.1a_rocket gptkb:Soyuz-2.1b_rocket gptkb:Soyuz-FG_rocket gptkb:Soyuz-U_rocket gptkb:Voskhod_rocket gptkb:Vostok_rocket |
| gptkbp:weight |
1120 kg
|
| gptkbp:bfsParent |
gptkb:RD-107_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-107A
|