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 1990 at a cost of 15 billion yen. It has three stages and is 30.7 m (101 ft) high, 2.5 m in diameter, and weighs about 140,000 kg (310,000 lb). It was capable of launching a satellite weighing 1,800 kg (4,000 lb) into an orbit as high as 250 km (160 mi).

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Wikimedia, Wikidata
M-5; Mu-5
height 30.7 metre, diameter 2.5 metre, 
Mu, Nissan, Japan, 
Persia, Republic of Haiti, Mu, Ekran, Dong Fang Hong 2, Hayabusa, Tarshish, Sweden, Sikh Confederacy, Ashkenaz, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Japan, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,

Frameless

M-V 2nd nozzle

M-V Fairing cutaway model P4037829

Type	Subtype	Date	Description	Notes	Source
commons	image		M-V 2nd nozzle		Commons
commons	image		M-V Fairing cutaway model P4037829		Commons