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MB-35
Part of LE-5 engine
Rocketdyne LOx/LH2 rocket engine. Design 2004. Mitsubishi / Boeing joint project for an engine for Delta IV cryogenic upper stages. Expander bleed, pump-fed.

Status: Design 2004. Date: 1999. Thrust: 156.00 kN (35,070 lbf). Unfuelled mass: 345 kg (760 lb). Specific impulse: 467 s. Height: 2.21 m (7.25 ft).

Boeing's Rocketdyne Division (USA) and Mitsubishi Heavy Industries (Japan) had announced on 14 February 2000 their agreement to jointly design and develop the MB-XX family of high-power cryogenic upper-stage engines for Boeing's Delta-4 and Japan's H-2A launch vehicles.

Engine: 345 kg (760 lb).



Country: Japan. Propellants: Lox/LH2. Agency: Rocketdyne.

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