Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:chamber |
1
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:cycle |
oxidizer-rich staged combustion
|
| gptkbp:diameter |
1.45 m
|
| gptkbp:firstFlight |
2013
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:gimbalRange |
+/-6 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-0124A
|
| gptkbp:length |
2.4 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:nozzleExpansionRatio |
55
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
359 s
|
| gptkbp:status |
in service
|
| gptkbp:thrustVacuum |
294 kN
|
| gptkbp:usedIn |
gptkb:Angara_rocket
gptkb:Soyuz-2.1v |
| gptkbp:weight |
480 kg
|
| gptkbp:bfsParent |
gptkb:Angara
gptkb:Angara_rocket gptkb:Angara-A5 |
| gptkbp:bfsLayer |
6
|