Minotaur-C 3110
ActiveOrbital Sciences Corporation (OSC)
Feb. 24, 2009
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
31.6 m -
Diameter
2.35 m -
Fairing Diameter
2.35 m -
Launch Mass
73.0 T -
Thrust
1380.0 kN
Family
-
Name
Minotaur-C 3110 -
Family
― -
Variant
3110 -
Alias
― -
Full Name
Minotaur-C 3110
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
― -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Orbital Sciences Corporation
Commercial
None
OSCNone
Taurus 3110 | OCO
Orbital Sciences Corporation | United States of AmericaVandenberg SFB, CA, USA
Feb. 24, 2009, 9:55 a.m.
LVM-3 (GSLV Mk III)
CMS-03 (GSAT-7R)
Satish Dhawan Space Centre Second Launch Pad - Satish Dhawan Space Centre, IndiaCommunications Satellite for the Indian Navy, replacing GSAT-7 for secure real-time links between Indian warships, submarines, aircraft, and shore-ba…
Falcon 9
Bandwagon 4 (Dedicated Mid-Inclination Rideshare)
Space Launch Complex 40 - Cape Canaveral SFS, FL, USADedicated rideshare flight to a mid-inclination orbit with dozens of small microsatellites and nanosatellites for commercial and government customers.
Falcon 9
Starlink Group 11-23
Space Launch Complex 4E - Vandenberg SFB, CA, USAA batch of 28 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
Long March 2
Shenzhou 21
Launch Area 4 (SLS-1 / 921) - Jiuquan Satellite Launch Center, People's Republic of ChinaTenth crewed flight to the Chinese space station.
Falcon 9
Starlink Group 10-37
Space Launch Complex 40 - Cape Canaveral SFS, FL, USAA batch of 29 satellites for the Starlink mega-constellation - SpaceX's project for space-based Internet communication system.
