Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:culturalHeritage |
derived from RD-191
|
| gptkbp:diameter |
2.1 m
|
| gptkbp:engineCycle |
oxidizer-rich staged combustion
|
| gptkbp:exportedTo |
gptkb:United_States
|
| gptkbp:firstFlight |
2016
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
+/- 5 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-181
|
| gptkbp:length |
3.56 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:notableClient |
gptkb:Northrop_Grumman
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:predecessor |
gptkb:AJ26
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
338 s
311.3 s |
| gptkbp:status |
in production
|
| gptkbp:thrustSeaLevel |
1860 kN
|
| gptkbp:thrustVacuum |
1920 kN
|
| gptkbp:usedFor |
first stage
|
| gptkbp:usedIn |
gptkb:Antares_rocket
|
| gptkbp:weight |
2340 kg
|
| gptkbp:bfsParent |
gptkb:Antares_rocket
gptkb:Antares_230 gptkb:Antares_230+ |
| gptkbp:bfsLayer |
6
|