Minotaur-C 2110
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
- 27.9 m
- Diameter
- 2.35 m
- Launch mass
- 73 t
- Stages
- 4
- LEO capacity
- 1,380 kg
- GTO capacity
- 375 kg
- SSO capacity
- 900 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
2flightswith a definitive outcome
50%success rate1 of 2
1failureincluding partial failures
0success streakcurrent
First flight December 21, 1999 · latest September 21, 2001
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Minotaur-C 2110 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1999 | 1 | 0 | 1 |
| 2000 | 0 | 0 | 0 |
| 2001 | 0 | 1 | 1 |