Hayabusa

Overview

Destination: Asteroid
Mission: Astrophysics

Asteroid M-V Pad Uchinoura Space Center, Japan

MUSES-C (renamed Hayabusa after launch) is a sample return mission to the asteroid. Its primary goal is to acquire and verify technology which is necessary to retrieve samples from a small body in the solar system and to bring back them to the earth.

M-V

Family: Mu
Configuration: V

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

Specifications
  • Minimum Stage
    3
  • Max Stage
    4
  • Length
    30.8 m
  • Diameter
    2.5 m
  • Fairing Diameter
    2.5 m
  • Launch Mass
    137 T
  • Thrust
    3780 kN
Family
  • Name
    M-V
  • Family
    Mu
  • Variant
    V
  • Alias
  • Full Name
    M-V
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    1800 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

IHI Corporation

IHI Corporation

(IHI)

Successes: 0 Failures: 0 Pending: 0

Agency Type: Commercial

INFO WIKI

Uchinoura Space Center, Japan

M-V Pad


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Success
2 weeks, 1 day ago
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