Padside

Minotaur-C 2210

Minotaur family · Orbital Sciences Corporation · Active

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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
29.7 m
Diameter
2.35 m
Launch mass
73 t
Stages
4
Launch cost
LEO capacity
1,380 kg
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Vehicle specifications from Launch Library; blanks are unpublished figures.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
100%
1 of 1
Current success streak
1
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