Mu-3S-II
Mu-3S-II is a 4-stage Mu rocket built by Institute of Space and Astronautical Science.
Specifications
- Height
- 27.8 m
- Diameter
- 1.41 m
- Mass
- 61000 kg
- Stages
- 4
- Thrust
- 1930 kN
- LEO payload
- 800 kg
- First flight
- Jan 7, 1985
Manufacturer & operator
- Family
- Mu
- Variant
- S-II
- Manufacturer
- Institute of Space and Astronautical Science
- Operator
- β
- Country
- Japan
Launch sites
- Uchinoura Space Center, Japan (8 launches)
Launch history
8 launches to date.