NEXT SPACEFLIGHT

Minotaur V

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
Successes: 1
Partial Failures: 0
Failures: 0
Success Streak: 1
Success Rate: 100%
Wiki

Configurations

Minotaur V
Image Credit: Northrop Grumman
Northrop
Status: Active
Price: $55.0 million
Liftoff Thrust: 2,224 kN
Payload to GTO: 532 kg
Stages: 5
Strap-ons: 0
Rocket Height: 24.56 m
Fairing Diameter: 2.34 m
Fairing Height: 6.4 m

Launch Sites

LP-0B, Wallops Flight Facility, Virginia, USA

Launches

Northrop
Minotaur V | LADEE
Sat Sep 07, 2013 03:27 UTC
LP-0B, Wallops Flight Facility, Virginia, USA