Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:announced |
2004
|
| gptkbp:application |
horizontal landing
single-stage-to-orbit |
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:engineType |
air-breathing rocket engine
|
| gptkbp:fuelType |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
Skylon spaceplane
|
| gptkbp:intendedUse |
orbital launch
|
| gptkbp:length |
82 meters
|
| gptkbp:manufacturer |
gptkb:Reaction_Engines_Limited
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:payloadBayDiameter |
4.8 meters
|
| gptkbp:payloadBayLength |
13 meters
|
| gptkbp:payloadToLEO |
15,000 kg
|
| gptkbp:projectedCostPerLaunch |
low compared to conventional rockets
|
| gptkbp:propulsion |
gptkb:SABRE_engine
|
| gptkbp:reusable |
fully reusable
|
| gptkbp:seatingCapacity |
uncrewed
|
| gptkbp:status |
concept
|
| gptkbp:takeoffMethod |
horizontal takeoff
|
| gptkbp:website |
https://www.reactionengines.co.uk/skylon/
|
| gptkbp:wingspan |
25 meters
|
| gptkbp:bfsParent |
gptkb:Reaction_Engines_Limited
|
| gptkbp:bfsLayer |
7
|