Orbital Sciences Corporation

Minotaur-C 3110

3110

Active

Overview

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American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.

Manufacturer

Orbital Sciences Corporation

Variant

3110

Alias

N/A

Maiden Flight

February 24, 2009

Technical Specifications

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31.6 m

Length

2.35 m

Diameter

0 t

Launch Mass

1380 kN

Liftoff Thrust

—

LEO Capacity

—

GTO Capacity

Launch Record

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1

Total Launches

0

Successful

1

Failed

0.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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