Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:basedOn |
gptkb:NK-33
|
| gptkbp:cycle |
oxidizer-rich staged combustion
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:fault |
2014 Antares launch failure
|
| gptkbp:firstFlight |
2013
|
| https://www.w3.org/2000/01/rdf-schema#label |
AJ26
|
| gptkbp:length |
3.7 m
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:modificationBy |
gptkb:Aerojet
|
| gptkbp:numberOfEnginesUsed |
2 (on Antares first stage)
|
| gptkbp:origin |
gptkb:United_States
|
| gptkbp:originalDesign |
Soviet NK-33
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,630 kN
|
| gptkbp:usedBy |
gptkb:Orbital_Sciences_Corporation
|
| gptkbp:usedIn |
gptkb:Antares_rocket
|
| gptkbp:weight |
1,250 kg
|
| gptkbp:bfsParent |
gptkb:Antares_120
|
| gptkbp:bfsLayer |
6
|