Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
experimental spacecraft
|
| gptkbp:cancellationDate |
2001
technical difficulties with composite hydrogen tank |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:NASA
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:height |
7.6 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
X-33 VentureStar
|
| gptkbp:intendedCrew |
uncrewed
|
| gptkbp:intendedToBe |
single-stage-to-orbit vehicle
|
| gptkbp:intendedUse |
gptkb:technology
prototype for VentureStar |
| gptkbp:launchSite |
gptkb:Edwards_Air_Force_Base
|
| gptkbp:length |
21.9 meters
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:mass |
57,153 kg
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:projectCost |
~$1.3 billion
|
| gptkbp:propulsion |
aerospike engine
|
| gptkbp:relatedTo |
gptkb:Space_Shuttle_program
gptkb:Reusable_Launch_Vehicle_program |
| gptkbp:startYear |
1996
|
| gptkbp:status |
cancelled
|
| gptkbp:successor |
VentureStar (never built)
|
| gptkbp:wingspan |
22.9 meters
|
| gptkbp:bfsParent |
gptkb:aircraft
|
| gptkbp:bfsLayer |
4
|