Minotaur V
Description
The Minotaur V is an American expendable launch system derived from the Minotaur IV, itself a derivative of the LGM-118 Peacekeeper ICBM. It was developed by Orbital Sciences Corporation, (now absorbed into Northrop Grumman Innovation Systems).
Missions
1
Success Rate
100.0%
Successes
1
Failures
0
Success Streak
1
Partial Failures
0
Previous
September 7, 2013
LADEE
Minotaur V | Northrop
Wallops Flight Facility, Virginia, USA
Configurations
Active
Minotaur V
Active Since 2013
Price
$55.00 million
Rocket
Height: 24.56m
Payload to Orbit
GTO: 532 kg
Liftoff Thrust
2,224 Kilonewtons
Fairing
Diameter: 2.34m
Height: 6.4m
Stages
5