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The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in 1990 at a cost of 15 billion yen. It has three stages and is 30.7 meters (101 ft) high, 2.5 meters (8 ft 2 in) in diameter and weighs about 140 tonnes (310,000 pounds).
Missions
7
Success Rate
85.7%
Successes
6
Failures
1
Success Streak
4
Partial Failures
0
Active 2003 to 2006
Rocket
Height: 30.7m
Payload to Orbit
LEO: 1,800 kg
Liftoff Thrust
3,780 Kilonewtons
Stages
4
Active 1997 to 2000
Rocket
Height: 30.7m
Payload to Orbit
LEO: 1,800 kg
Liftoff Thrust
3,780 Kilonewtons
Stages
4