Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
3
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
309,000 lbf
|
| gptkbp:thrustVacuum |
367,000 lbf
|
| gptkbp:usedIn |
gptkb:Atlas_D_missile
gptkb:Mercury-Atlas_launches gptkb:Atlas_LV-3B |
| gptkbp:bfsParent |
gptkb:Atlas_LV-3B
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rocketdyne MA-2
|