Minotaur-C 3210
Minotaur familyOrbital Sciences CorporationActive
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
- LEO capacity
- 1,275 kg
- SSO capacity
- 880 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
1flightwith a definitive outcome
100%success rate1 of 1
1success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.