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Space · launch vehicle

Mu-4S

ISAS RETIRED
At a glance
Launches
4
Success rate
75%
3 ok · 1 failed
Payload to LEO
180 kg
Payload to GTO
—
Status
Retired
First flight
25 Sept 1970
Reusable
No
Height
23.6 m
Diameter
1.41 m
Launch mass
43 t
Liftoff thrust
1,932 kN
Stages
5
Launch cost
—
Booster landings
—
About

The Mu, also known as M, was a series of Japanese solid-fuelled carrier rockets, which were launched from Uchinoura between 1966 and 2006. Originally developed by Japan's Institute of Space and Astronautical Science, Mu rockets were later operated by Japan Aerospace Exploration Agency following ISAS becoming part of it.