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Minotaur·Orbital ATK

Minotaur-C 2210

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Specifications

Status
active
Height
29.7 m
Diameter
2.35 m
Mass
73,000 kg
Stages
4
Thrust
1,380 kN
Payload to LEO
1,380 kg
First flight
1998-02-10
Total launches
1
Success / Fail
1 / 0

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.

Payloads it launched

4 loaded
ORBCOMM FM03
OrbComm · LEO
GFO
LEO
ORBCOMM FM04
OrbComm · LEO
CELESTIS-02 & TAURUS R/B
LEO