Tansei-3

Overview

Destination: Elliptical Orbit
Mission: Astrophysics

Elliptical Orbit Mu Center Uchinoura Space Center, Japan

Japanese satellite used to test the new Mu-3H launch vehicle, experiment magnetic stabilization and ovserve UV radiation

Mu-3H

Family: Mu
Configuration: H

The Mu, also known as M, was a series of Japanese solid-fuelled carrier rockets, which were launched from Uchinoura between 1966 and 2006. Originally developed by Japan's Institute of Space and Astronautical Science, Mu rockets were later operated by Japan Aerospace Exploration Agency following ISAS becoming part of it.

Specifications
  • Stages
    5
  • Length
    23.8 m
  • Diameter
    1.41 m
  • Fairing Diameter
    1.41 m
  • Launch Mass
    44 T
  • Thrust
    2150 kN
Family
  • Name
    Mu-3H
  • Family
    Mu
  • Variant
    H
  • Alias
  • Full Name
    Mu-3H
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    300 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Institute of Space and Astronautical Science

Institute of Space and Astronautical Science

(ISAS)

Successes: 24 Failures: 8 Pending: 0

Agency Type: Government

ISAS is a Japanese national research organization of astrophysics using rockets, astronomical satellites and interplanetary probes which played a major role in Japan's space development.

INFO WIKI

Uchinoura Space Center, Japan

Mu Center


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