Titan 401A Centaur
Titan familyLockheed MartinRetired
Titan IV was a family of heavy-lift space launch vehicles developed by Martin Marietta and operated by the United States Air Force from 1989 to 2005.
Specifications
- Thrust
- 14,200 kN
- Height
- 63.1 m
- Diameter
- 3.05 m
- Launch mass
- 868 t
- Stages
- 3
- LEO capacity
- 21,680 kg
- GTO capacity
- 9,000 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
9flightswith a definitive outcome
88.9%success rate8 of 9
1failureincluding partial failures
0success streakcurrent
First flight February 7, 1994 · latest August 12, 1998
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Titan 401A Centaur flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1994 | 3 | 0 | 3 |
| 1995 | 3 | 0 | 3 |
| 1996 | 1 | 0 | 1 |
| 1997 | 1 | 0 | 1 |
| 1998 | 0 | 1 | 1 |