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Launch Vehicle

Minotaur

United States Private Company

A family of small American launch vehicles built partly from decommissioned Minuteman and Peacekeeper ballistic missile stages under a U.S. Air Force program, flown for government-sponsored small satellites at low cost using surplus military hardware.

Facts
Vehicle Class
Light-lift solid-fuel expendable launch vehicle 1
Manufacturer
Northrop Grumman 1
First Flight Date
2000-01-26 1
Status
Operational, flown periodically for U.S. government small-satellite missions. 1
Connections

Has Vehicle Class

Source Minotaur (rocket family) (Wikipedia)

Operated By

Source Encyclopedia Astronautica
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Also in Business Atlas: the manufacturer of this subject.

Sources
1. Encyclopedia Astronautica
  • http://astronautix.com/m/minotaur.html
    Minotaur was developed for the US Air Force's Orbital/Suborbital Program (OSP) as a low-cost, four-stage Space Launch Vehicle (SLV) using a combination of government-supplied surplus Minuteman II ICBM motors and proven Orbital space launch technologies.
  • Operated By: Northrop Grumman
Minotaur (rocket family) (Wikipedia)
  • In Group: Commercial American Launch Vehicles, Lead sentence
    The Minotaur is a family of United States solid-fuel launch vehicles derived from retired Minuteman and Peacekeeper intercontinental ballistic missiles (ICBM).
  • Has Vehicle Class: Small-Lift Launch Vehicle, Lead sentence
    The Minotaur family consists of four primary variants: the Minotaur I, used for launching small satellites into low Earth orbit; the Minotaur II, used primarily as a suborbital target vehicle; the Minotaur IV, a small-lift orbital launch vehicle; and the Minotaur V and Minotaur VI, capable of higher-energy missions including geostationary transfer orbit and trans-lunar trajectories.
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