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Mu-3S
Part of Mu
Mu-3C
Mu-3C
Mu-3C - COSPAR 1975-014
Japanese all-solid orbital launch vehicle. Four stage vehicle consisting of 8 x SB-310 + 1 x M-13TVC + 1 x M-22TVC + 1 x M-3A

Status: Retired 1984. First Launch: 1980-02-17. Last Launch: 1984-02-14. Number: 4 . Payload: 300 kg (660 lb). Thrust: 2,150.00 kN (483,330 lbf). Gross mass: 49,300 kg (108,600 lb). Height: 23.80 m (78.00 ft). Diameter: 1.41 m (4.62 ft). Apogee: 1,000 km (600 mi).

LEO Payload: 300 kg (660 lb).


More at: Mu-3S.

Family: all-solid, orbital launch vehicle. Country: Japan. Spacecraft: Tansei, EXOS, Astro. Launch Sites: Kagoshima, Kagoshima M. Stages: M-22, M-3A, SB-310, M-13, M-23-Mu, SB-735 engine, M-3B-Mu. Agency: Nissan.

1980 February 17 - . 00:40 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-3S.
1981 February 21 - . 00:30 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-3S.
1983 February 20 - . 05:10 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. Launch Pad: M1. LV Family: Mu. Launch Vehicle: Mu-3S.
1984 February 14 - . 08:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. Launch Pad: M1. LV Family: Mu. Launch Vehicle: Mu-3S.

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