Hotol - Where next?
Abstract
The design of Hotol 'a fully reusable single-stage-to-orbit spaceplane' is examined. The possible incorporation of Hotol into the ESA space program is discussed. Hotol's airbreathing cryogenic engine, which is capable of air-breathing propulsion through the atmosphere and rocket propulsion at Mach 5 and 7, is analyzed. The specifications and wing configuration of the spaceplane are described. The horizontal take-off and landing of the vehicle under microwave radar control is studied. Hotol, which can carry a payload mass of 7-11 tons, is to be utilized for the launching of satellites into geosynchronous orbit and low-earth orbit, and the retrieving of satellites and space station hardware; the spaceplane is designed to perform unmanned and manned operations.
- Publication:
-
Flight International (ISSN 0015-3710
- Pub Date:
- March 1986
- Bibcode:
- 1986FlInt.129...38M
- Keywords:
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- Aerospace Planes;
- Launch Vehicles;
- Space Transportation;
- Cost Estimates;
- Payloads;
- Space Commercialization;
- Spacecraft Launching;
- Takeoff;
- Launch Vehicles and Space Vehicles