Space · launch vehicle

Minotaur-C 3210

OSC ACTIVE

At a glance

Launches

Success rate

100%

1 ok · 0 failed

Payload to LEO

—

Payload to GTO

—

Manufacturer

Orbital Sciences Corporation

Status

Active

First flight

20 May 2004

Reusable

Height

31.6 m

Diameter

2.35 m

Launch mass

73 t

Liftoff thrust

1,380 kN

Stages

Launch cost

—

Booster landings

—

Links

Wikipedia

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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

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