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

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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