Minotaur-C 2210
ActiveOrbital 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
OSCFlight Record
No spaceflights found for .
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Space Launch System (SLS)
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Meridian-M No.21L
43/3 (43L) - Plesetsk Cosmodrome, Russian FederationNote: Payload identity uncertain. Meridian is a series of communications satellite for military and civilian use.
