Padside

Minotaur-C 3110

Minotaur family · Orbital Sciences Corporation · Active

Wikipedia ↗Compare with… →

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

Thrust
1,380 kN
Height
31.6 m
Diameter
2.35 m
Launch mass
73 t
Stages
4
Launch cost
LEO capacity
GTO capacity
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
1
Launches with a definitive outcome
Success rate
0%
0 of 1
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Launches