IHI Corporation

M-V

V

Retired

Overview

/01

The M-V rocket also called Mu-5 was a Japanese solid-fuel rocket designed to launch scientific satellites.

Manufacturer

IHI Corporation

Variant

V

Alias

N/A

Maiden Flight

February 12, 1997

Technical Specifications

/02

30.8 m

Length

2.5 m

Diameter

0 t

Launch Mass

3780 kN

Liftoff Thrust

1800 kg

LEO Capacity

—

GTO Capacity

Launch Record

/03

7

Total Launches

6

Successful

1

Failed

85.7%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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