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McDonnell-Douglas ILRV stage
LOx/LH2 propellant rocket stage. High-pressure Lox/Lh2 engine.

AKA: McDonnell-Douglas ILRV. Status: Study. Thrust: 16,242.82 kN (3,651,532 lbf). Gross mass: 215,000 kg (473,000 lb). Unfuelled mass: 95,254 kg (209,999 lb). Height: 53.00 m (173.00 ft).

No Engines: 4.



Country: USA. Propellants: Lox/LH2.

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