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Minotaur (rocket)

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Image:Minotaur-1 1.jpg The Minotaur I Rocket is an American solid fuel rocket designed to launch small satellites. It is built by Orbital Sciences Corporation and uses a Minuteman stage, combined with Pegasus upper stages. It is capable of putting up to 1280 lbm (580 kg) into LEO (100 nmi/185 km, 28.5 deg inclination).

The fourth launch of Minotaur I in September 2005 was a spectaular sunset launch, delivering a fast-growing cloud of colors, visible across the whole southern west coast of the United States. Local authorities reported being flooded with calls inquiring about the phenomenon.

[edit] Minotaur flights

Date (UTC) Flight Payload Result
January 27 2000 03:03:06 1 JAWSAT (P98-1) Success
FalconSat1 / ASUSat1 / OCSE / OPAL
July 19 2000 20:09:00 2 Mightysat 2.1 (Sindri, P99-1) / MEMS 2A / MEMS 2B Success
April 11 2005 13:35:00 3 XSS 11 Success
September 23 2005 02:24:00 4 Streak (STP-R1) Success
April 15 2006 01:40:00 5 COSMIC (FORMOSAT 3) Success

[edit] Minotaur IV

Orbital Sciences Corporation is currently developing the much more powerful Minotaur IV, which combines the government-furnished solid rocket motors from decommissioned Peacekeeper ICBMs with technologies shared with other Orbital-built launch vehicles, including the Minotaur I, Pegasus, and Taurus.

A Minotaur V five-stage version is also conceived with an additional upper stage for GTO and interplanetary missions.

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