Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:engineType |
nuclear thermal rocket
|
| https://www.w3.org/2000/01/rdf-schema#label |
ISUS 90-15
|
| gptkbp:manufacturer |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:propulsion |
gptkb:uranium
hydrogen |
| gptkbp:specificImpulseVacuum |
900 s
|
| gptkbp:status |
experimental
|
| gptkbp:thrust |
15 kN
|
| gptkbp:bfsParent |
gptkb:Type_214_submarine
|
| gptkbp:bfsLayer |
5
|