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Mu-4S
Part of Mu
Japanese all-solid orbital launch vehicle. Five stage vehicle consisting of 8 x SB-310 + 1 x M-10 + 1 x M-20 + 1 x M-30 + 1 x M-40

Status: Retired 1972. First Launch: 1970-09-25. Last Launch: 1972-08-19. Number: 4 . Payload: 180 kg (390 lb). Thrust: 1,932.00 kN (434,330 lbf). Gross mass: 43,600 kg (96,100 lb). Height: 23.60 m (77.40 ft). Diameter: 1.41 m (4.62 ft). Apogee: 6,500 km (4,000 mi).

LEO Payload: 180 kg (390 lb).


More at: Mu-4S.

Family: all-solid, orbital launch vehicle. Country: Japan. Spacecraft: SS, Tansei. Launch Sites: Kagoshima, Kagoshima M. Stages: M-20, SB-310, M-10, M-30, M-40. Agency: Nissan.

1970 September 25 - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-4S. FAILURE: Fourth stage failed to ignite.. Failed Stage: 4.
1971 February 16 - . 04:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-4S.
1971 September 28 - . 04:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-4S.
1972 August 19 - . 02:40 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-4S.

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