Minotaur-C 2210 Vehicle Overview
A complete overview of the Minotaur-C 2210 launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Minotaur-C 2210
Family
Minotaur-C
Manufacturer
First Launch
10 Feb 1998
Successful Launches
1
Failed Launches
0
Rocket Info
Status
Active
Stages
4
Length
29.7 m
Diameter
2.35 m
Launch Mass
73 tons
Thrust
1,380 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
1,380 kg
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.
Launch Sites used by Minotaur-C 2210
Vandenberg SFB
U.S. Space Force facility in California for spacecraft launches and missile testing.
📍 CA, United States
🚀 797 Launches