Minotaur C
Minotaur familyOrbital ATKRetired
Specifications
- Thrust
- 1,607 kN
- Height
- 27.9 m
- Diameter
- 2.35 m
- Launch mass
- 73 t
- Stages
- 4
- LEO capacity
- 1,458 kg
- SSO capacity
- 1,054 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
4flightswith a definitive outcome
75%success rate3 of 4
1failureincluding partial failures
1success streakcurrent
First flight March 13, 1994 · latest October 31, 2017
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Minotaur flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1994 | 1 | 0 | 1 |
| 1995 | 0 | 0 | 0 |
| 1996 | 0 | 0 | 0 |
| 1997 | 0 | 0 | 0 |
| 1998 | 1 | 0 | 1 |
| 1999 | 0 | 0 | 0 |
| 2000 | 0 | 0 | 0 |
| 2001 | 0 | 0 | 0 |
| 2002 | 0 | 0 | 0 |
| 2003 | 0 | 0 | 0 |
| 2004 | 0 | 0 | 0 |
| 2005 | 0 | 0 | 0 |
| 2006 | 0 | 0 | 0 |
| 2007 | 0 | 0 | 0 |
| 2008 | 0 | 0 | 0 |
| 2009 | 0 | 0 | 0 |
| 2010 | 0 | 0 | 0 |
| 2011 | 0 | 1 | 1 |
| 2012 | 0 | 0 | 0 |
| 2013 | 0 | 0 | 0 |
| 2014 | 0 | 0 | 0 |
| 2015 | 0 | 0 | 0 |
| 2016 | 0 | 0 | 0 |
| 2017 | 1 | 0 | 1 |