Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:cancellationDate |
technical difficulties with composite fuel tank
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:fundedBy |
gptkb:NASA
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lockheed Martin VentureStar
|
| gptkbp:intendedCrewCapacity |
7
|
| gptkbp:intendedLaunchSite |
gptkb:Kennedy_Space_Center
|
| gptkbp:intendedUse |
reusable launch vehicle
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:notableFeature |
composite cryogenic hydrogen tank
lifting body design single-stage-to-orbit design |
| gptkbp:payloadToLEO |
20,000 kg
|
| gptkbp:predecessor |
gptkb:Rockwell_X-33
|
| gptkbp:propulsion |
hydrogen-oxygen rocket engines
|
| gptkbp:relatedTo |
gptkb:Space_Shuttle
gptkb:X-33 |
| gptkbp:startYear |
1996
2001 |
| gptkbp:status |
cancelled
|
| gptkbp:successor |
none
|
| gptkbp:bfsParent |
gptkb:Douglas_X-33
|
| gptkbp:bfsLayer |
6
|