Titan 402A IUS
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
- 54 m
- Diameter
- 3.05 m
- Launch mass
- 910 t
- Stages
- 3
- Launch cost
- $432M
- LEO capacity
- 21,680 kg
- GEO capacity
- 2,380 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
100%success rate3 of 3
0failuresincluding partial failures
3success streakcurrent
First flight June 14, 1989 · latest December 22, 1994
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Titan 402A IUS flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1989 | 1 | 0 | 1 |
| 1990 | 1 | 0 | 1 |
| 1991 | 0 | 0 | 0 |
| 1992 | 0 | 0 | 0 |
| 1993 | 0 | 0 | 0 |
| 1994 | 1 | 0 | 1 |