Orbital Sciences Corporation

Minotaur I

Minotaur I
Active

Overview

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The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.

Manufacturer

Orbital Sciences Corporation

Variant

N/A

Alias

Minotaur OSP-SLV

Maiden Flight

January 27, 2000

Technical Specifications

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19.21 m

Length

1.67 m

Diameter

0 t

Launch Mass

935 kN

Liftoff Thrust

580 kg

LEO Capacity

GTO Capacity

Launch Record

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12

Total Launches

12

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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