Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:engineer
|
| gptkbp:aimsTo |
orbital launch capability
horizontal takeoff and landing |
| gptkbp:beganIn |
1989
|
| gptkbp:developedBy |
gptkb:Reaction_Engines_Limited
|
| gptkbp:features |
pre-cooler technology
modular payload bay integrated engine-airframe design |
| gptkbp:focusesOn |
single-stage-to-orbit vehicle design
|
| gptkbp:involves |
thermal protection systems
aerodynamic optimization SABRE engine development lightweight airframe materials reusable spacecraft technology |
| gptkbp:relatedTo |
Skylon (spaceplane)
|
| gptkbp:target |
commercial spaceflight
satellite deployment space station resupply |
| gptkbp:uses |
liquid oxygen
hydrogen fuel |
| gptkbp:bfsParent |
gptkb:Frank_Newby
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Engineering of the Skylon
|