Family:
Configuration: V
The M-V rocket also called Mu-5 was a Japanese solid-fuel rocket designed to launch scientific satellites.
Specifications
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Minimum Stage
3
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Max Stage
4
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Length
30.8 m
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Diameter
2.5 m
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Fairing Diameter
2.5 m
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Launch Mass
137.0 T
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Thrust
3780.0 kN
Family
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Name
M-V
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Family
―
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Variant
V
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Alias
―
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Full Name
M-V
Payload Capacity
-
Launch Cost
―
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Low Earth Orbit
1800.0 kg
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Geostationary Transfer
Orbit
―
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Direct Geostationary
―
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Sun-Synchronous Capacity
―