Minotaur IV+
Minotaur familyOrbital Sciences CorporationActive
The Minotaur IV+ launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. It is similar to the Minotaur IV, but uses a larger Star-48V upper stage in place of the Orion-38 used on the baseline Minotaur IV.
Specifications
- Thrust
- 2,200 kN
- Height
- 23.9 m
- Diameter
- 2.35 m
- Launch mass
- 86 t
- Stages
- 4
- LEO capacity
- 1,950 kg
- GTO capacity
- 0 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.