M-V
Mu familyIHI CorporationRetired
The M-V rocket also called Mu-5 was a Japanese solid-fuel rocket designed to launch scientific satellites.
Specifications
- Thrust
- 3,780 kN
- Height
- 30.8 m
- Diameter
- 2.5 m
- Launch mass
- 137 t
- Stages
- 4
- LEO capacity
- 1,800 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
7flightswith a definitive outcome
85.7%success rate6 of 7
4success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.