Minotaur-C 2210 Vehicle Overview

A complete overview of the Minotaur-C 2210 launch vehicle, including launch stats, vehicle info and launch locations.

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Basic Info

Name

Minotaur-C 2210

Family

Minotaur-C

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

Vandenberg SFB launch site

U.S. Space Force facility in California for spacecraft launches and missile testing.

📍 CA, United States
🚀 796 Launches

Upcoming Launches