The Mu, also known as M, was a series of Japanese

solid-fueled Solid fuel refers to various forms of solid material that can be burnt to release energy, providing heat and light through the process of combustion. Solid fuels can be contrasted with liquid fuels and gaseous fuels. Common examples of solid fuel ...

carrier rocket A launch vehicle or carrier rocket is a rocket designed to carry a payload (spacecraft or satellites) from the Earth's surface to outer space. Most launch vehicles operate from a launch pad, launch pads, supported by a missile launch contro ...

s, which were launched from Uchinoura between 1966 and 2006. Originally developed by Japan's

Institute of Space and Astronautical Science (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. Since 2003, it is a division of Japan Aerospace E ...

, Mu rockets were later operated by

Japan Aerospace Exploration Agency The is the Japanese national air and space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and launch of satellites into orb ...

following ISAS becoming part of it.

Early Japanese carrier rockets

The first Mu rocket, the Mu-1 made a single,

sub-orbital A sub-orbital spaceflight is a spaceflight in which the spacecraft reaches outer space, but its trajectory intersects the atmosphere or surface of the gravitating body from which it was launched, so that it will not complete one orbital re ...

, test flight, on 31 October 1966. Subsequently, a series of rockets were produced, designated

Mu-3 The Mu, also known as M, was a series of Japanese solid-fueled 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 ...

and

Mu-4 The Mu, also known as M, was a series of Japanese solid-fueled 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 ...

. In 1969 a suborbital test launch of the Mu-3D was conducted. The first orbital launch attempt for the Mu family, using a Mu-4S, was conducted on 25 September 1970, however the fourth stage did not ignite, and the rocket failed to reach orbit. On 16 February 1971, Tansei 1 was launched by another Mu-4S rocket. Two further Mu-4S launches took place during 1971 and 1972. The Mu-4S was replaced by the Mu-3C, was launched four times between 1974 and 1979, with three successes and one failure, and the Mu-3H, which was launched three times in 1977 and 1978. The Mu-3S was used between 1980 and 1984, making four launches. The final member of the Mu-3 family was the Mu-3SII, which was launched eight times between 1985 and 1995. The Mu-3 was replaced in service by the

M-V The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in ...

M-V

The

, or Mu-5, was introduced in 1997 and retired in 2006. Seven launches, six of which were successful, were conducted. Typically, the M-V flew in a three-stage configuration, however a four-stage configuration, designated M-V KM was used 3 times, with the MUSES-B (HALCA) satellite in 1997, Nozomi (PLANET-B) spacecraft in 1998, and the

Hayabusa was a robotic spacecraft developed by the Japan Aerospace Exploration Agency (JAXA) to return a sample of material from a small near-Earth asteroid named 25143 Itokawa to Earth for further analysis. ''Hayabusa'', formerly known as MUSES-C ...

(MUSES-C) spacecraft in 2003. The three-stage configuration had a maximum payload of for an orbit with altitude of and

inclination Orbital inclination measures the tilt of an object's orbit around a celestial body. It is expressed as the angle between a Plane of reference, reference plane and the orbital plane or Axis of rotation, axis of direction of the orbiting object ...

of 30°, and to a polar orbit (90° inclination), with an altitude of . The M-V KM could launch to an orbit with 30° inclination and altitude. The three stage M-V had a total launch mass of , whilst the total mass of a four-stage M-V KM was .

List of launches

All launches are from the Mu Launch Pad at the

Uchinoura Space Center The is a space launch facility in the Japanese town of Kimotsuki, Kagoshima Prefecture. Before the establishment of the JAXA space agency in 2003, it was simply called the (KSC). All of Japan's scientific satellites were launched from Uchino ...

. Two sub-orbital launches of the Mu family were performed prior to its first orbital flight: the 1.5 stage Mu-1 flew on October 31, 1966, at 05:04 UTC and the 3.5 stage Mu-3D flew on August 17, 1969, at 06:00 UTC.

References

External links

Mu series in Encyclopedia AstronauticaISAS Satellite Launch Vehicles
{{Japanese launch systems Solid-fuel rockets Space launch vehicles of Japan Rocket families Japanese inventions

Early Japanese carrier rockets

M-V

List of launches

See also

References

External links