Minotaur II

Minotaur II rockets consist of the M55A1 first stage and SR19AJ1 second stage of a decommissioned Minuteman missile. The third stage varies depending on the configuration required for the payload: a Minuteman II M57A1 stage is used on the baseline configuration, whilst the Minotaur II+ uses an SR-73-AJ. The Minotaur II Lite is a two-stage configuration, without a third stage. A heavy configuration is also available, with an Orion 50XL third stage, as used on the Minotaur I. The baseline configuration can propel a 400 kilograms (880 lb) payload 4,000 kilometres (2,500 mi) downrange, whilst the heavy configuration can place 1,400 kilograms (3,100 lb) onto an 8,000-kilometre (5,000 mi) trajectory.

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2000  Wikimedia, Wikidata
height 17.6 metre, diameter 1.68 metre, mass 33100 kilogram, 
Minotaur, Orbital Sciences Corporation, United States, 
Sikh Confederacy, Republic of Haiti, 2000, Minotaur, launch vehicle, Ekran, Dong Fang Hong 2, Tarshish, Sweden, United States, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz, 

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Minotaur-2 1

Type	Subtype	Date	Description	Notes	Source
commons	image		Minotaur-2 1		Commons