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Interim HOTOL stage
Part of HOTOL Family
LOx/LH2 propellant rocket stage. .

AKA: Interim HOTOL. Status: Study 1990. Thrust: 7,840.00 kN (1,762,500 lbf). Gross mass: 250,000 kg (550,000 lb). Unfuelled mass: 33,100 kg (72,900 lb). Specific impulse: 455 s. Specific impulse sea level: 352 s. Burn time: 122 s. Height: 36.45 m (119.58 ft). Diameter: 10.00 m (32.00 ft). Span: 21.60 m (70.80 ft).

Cost $ : 10.000 million. No Engines: 4.



Country: UK. Engines: RD-0120. Launch Vehicles: Interim HOTOL. Propellants: Lox/LH2.

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