Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:experimental_spacecraft
|
| gptkbp:cancellationDate |
2001
technical difficulties with composite hydrogen tank |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Lockheed_Martin
gptkb:NASA |
| gptkbp:firstFlight |
late 1990s
|
| gptkbp:fundedBy |
gptkb:NASA
|
| gptkbp:height |
7.6 m
|
| gptkbp:intendedToLeadTo |
gptkb:VentureStar
|
| gptkbp:intendedUse |
gptkb:technology
|
| gptkbp:length |
21.9 m
|
| gptkbp:missionType |
gptkb:reusable_launch_vehicle
|
| gptkbp:plannedLandingSite |
gptkb:Edwards_Air_Force_Base
|
| gptkbp:plannedToDemonstrate |
single-stage-to-orbit technology
aerospike engine performance rapid turnaround operations |
| gptkbp:propulsion |
aerospike engine
|
| gptkbp:status |
cancelled
|
| gptkbp:wingspan |
22.9 m
|
| gptkbp:bfsParent |
gptkb:RL10_rocket_engine
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
X-33 (planned)
|