Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
20
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developmentType |
cancelled
|
| gptkbp:diameter |
2.4 m
|
| gptkbp:engineCycle |
gas-generator
|
| gptkbp:engineType |
liquid-fueled
linear aerospike |
| gptkbp:firstFlight |
never flown
|
| gptkbp:intendedUse |
gptkb:Lockheed_Martin_X-33
|
| gptkbp:length |
7.5 m
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:relatedTo |
aerospike engine technology
|
| gptkbp:specificImpulseVacuum |
455 s
347 s |
| gptkbp:status |
cancelled
|
| gptkbp:thrustVacuum |
220,000 lbf
|
| gptkbp:usedIn |
gptkb:X-33_program
|
| gptkbp:bfsParent |
gptkb:X-33_(VentureStar_demonstrator)
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
RS-2200 Linear Aerospike
|