| HOTOL |
home
topic index |
||
Model: HOTOL. Gross Mass: 250,000 kg (550,000 lb). Empty Mass: 50,000 kg (110,000 lb). Thrust (vac): 1,103.200 kN (248,009 lbf). Isp: 700 sec. Burn time: 730 sec. Propellants: Liquid Air/Lox/LH2. Isp(sl): 2,000 sec. Diameter: 7.00 m (22.90 ft). Span: 28.30 m (92.80 ft). Length: 62.80 m (206.00 ft). Country: UK. No Engines: 3. Motor: RB545. Status: Development ended 1985. Cost $ : 10.000 million. First Flight: 1998. Other designations: Horizontal Takeoff and Landing.
Model: Interim HOTOL. Gross Mass: 250,000 kg (550,000 lb). Empty Mass: 33,100 kg (72,900 lb). Thrust (vac): 7,840.000 kN (1,762,500 lbf). Isp: 455 sec. Burn time: 122 sec. Propellants: Lox/LH2. Isp(sl): 352 sec. Diameter: 10.00 m (32.00 ft). Span: 21.60 m (70.80 ft). Length: 36.45 m (119.58 ft). Country: UK. No Engines: 4. Motor: RD-0120. Status: Study 1990. Cost $ : 10.000 million. First Flight: 1991. Last Flight: 1991. No Launched: 1. Other designations: Interim HOTOL.
Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |
