Orbital Sciences Corporation

Minotaur-C 2110

2110

Active

Overview

/01

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

2110

Alias

N/A

Maiden Flight

September 21, 2001

Technical Specifications

/02
27.9 m

Length

2.35 m

Diameter

0 t

Launch Mass

1380 kN

Liftoff Thrust

1380 kg

LEO Capacity

—

GTO Capacity

Launch Record

/03
2

Total Launches

1

Successful

1

Failed

50.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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