Space · launch vehicle
Minotaur-C 2210
OSC
ACTIVE
At a glance
Launches
1
Success rate
100%
1 ok · 0 failed
Payload to LEO
1,380 kg
Payload to GTO
—
Manufacturer
Orbital Sciences CorporationStatus
ActiveFirst flight
10 Feb 1998Reusable
NoHeight
29.7 mDiameter
2.35 mLaunch mass
73 tLiftoff thrust
1,380 kNStages
4Launch cost
—Booster landings
—Links
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About
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
