Minotaur-C 2210

Active

Orbital Sciences Corporation (OSC)

Feb. 10, 1998

Description

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.

Specifications

Stages
4
Length
29.7 m
Diameter
2.35 m
Fairing Diameter
2.35 m
Launch Mass
73.0 T
Thrust
1380.0 kN

Family

Name
Minotaur-C 2210
Family
―
Variant
2210
Alias
―
Full Name
Minotaur-C 2210

Payload Capacity

Launch Cost
―
Low Earth Orbit
1380.0 kg
Geostationary Transfer Orbit
―
Direct Geostationary
―
Sun-Synchronous Capacity
―

Orbital Sciences Corporation

Commercial

None

OSC

None

Flight Record

No spaceflights found for .

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