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MB-45

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Status: Design 2004. Date: 1999. Thrust: 200.00 kN (44,960 lbf). Specific impulse: 467 s.

MHI (Mitsubishi Japan)/Boeing joint project for an engine for Delta IV cryogenic upper stages. Expander bleed, pump-fed. 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.