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Mu-3
Part of Mu
The Japanese Mu launcher series provided a flexible all-solid propellant launch vehicle for access to space.

Status: Out of production. Payload: 770 kg (1,690 lb). Thrust: 1,740.00 kN (391,160 lbf). Gross mass: 62,610 kg (138,030 lb). Height: 28.00 m (91.00 ft). Diameter: 1.50 m (4.90 ft). Apogee: 185 km (114 mi).

LEO Payload: 770 kg (1,690 lb) to a 185 km orbit. Payload: 520 kg (1,140 lb) to a GTO. Launch Price $: 30.000 million in 1994 dollars.

Stage Data - Mu-3



Family: all-solid, orbital launch vehicle. Country: Japan. Spacecraft: SS, Tansei, Corsa A, EXOS, Astro, Hagoromo, Hiten, Solar (Japanese satellite), Express 1. Agency: Nissan.

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