Reaction Engines RB545
| Country of origin | United Kingdom |
|---|---|
| Designer | Rolls-Royce |
| Application | Single-stage-to-orbit |
| Associated L/V | HOTOL |
| Predecessor | SATAN |
| Status | Cancelled |
| Liquid-fuel engine | |
| Propellant | Air and LO2 / liquid hydrogen |
| Cycle | Combined cycle precooled jet engine and closed cycle rocket engine |
| Configuration | |
| Nozzle ratio | 100:1 |
| Performance | |
| Thrust (vac.) | Approx. 735 kN (165,000 lbf) |
| Thrust (SL) | Approx. 340 kN (76,000 lbf) |
| Thrust-to-weight ratio | Up to 14 (atmospheric) |
| Isp (vac.) | 4,500 N‑s/kg (460 s) |
| Isp (SL) | 14,780 N‑s/kg (1,507 s) |
| Dimensions | |
| Dry weight | 2,500 kilograms (5,500 lb) (excluding intake and spill) |
| References | |
| References | |
HOTOL, for Horizontal Take-Off and Landing, was a 1980s British design for a single-stage-to-orbit (SSTO) spaceplane that was to be powered by an airbreathing jet engine. Development was being conducted by a consortium led by Rolls-Royce and British Aerospace (BAe).
Designed as a single-stage-to-orbit (SSTO) reusable winged launch vehicle, HOTOL was to be fitted with a unique air-breathing engine, the RB545 or Swallow, that was under development by British engine manufacturer Rolls-Royce. The propellant for the engine technically consisted of a combination of liquid hydrogen/liquid oxygen; however, it was to employ a new means of dramatically reducing the amount of oxidizer needed to be carried on board by utilising atmospheric oxygen as the spacecraft climbed through the lower atmosphere. Since propellant typically represents the majority of the takeoff weight of a rocket, HOTOL was to be considerably smaller than normal pure-rocket designs, roughly the size of a medium-haul airliner such as the McDonnell Douglas DC-9/MD-80.
While HOTOL's proof-of-concept design study was being carried out, attempts were made by both industry and the British government to establish international cooperation to develop, produce, and deploy the spacecraft. In spite of American interest in the programme, there was little appetite amongst the members of the European Space Agency (ESA), and the British government was not prepared to depart from ESA cooperation. Additionally, technical issues were encountered, and there were allegations that comparisons with alternative launch systems such as conventional rocket vehicle using similar construction techniques failed to show much advantage to HOTOL. In 1989, funding for the project ended. The termination of development work on HOTOL led to the formation of Reaction Engines Limited (REL) to develop and produce Skylon, a proposed spacecraft based on HOTOL technologies, including its engine.
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