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astronautix.com Interim HOTOL
Hotol 2
Hotol 2 - Hotol 2 is launched from the back of an Antonov 225

Credit: British Aerospace. 25,186 bytes. 408 x 257 pixels.

Gross Mass: 250,000 kg. Empty Mass: 33,100 kg. Thrust (vac): 800,000 kgf. Isp: 455 sec. Burn time: 122 sec. Propellants: Lox/LH2 Isp(sl): 352 sec. Diameter: 10.0 m. Span: 21.6 m. Length: 36.5 m. Country: UK/USSR. No Engines: 4. RD-0120 Status: Study. Other designations: Interim HOTOL.
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Last update 12 March 2001.
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© Mark Wade, 2001 .