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
- 15,000 kN
- Height
- 54 m
- Diameter
- 3.05 m
- Launch mass
- 925 t
- Stages
- 3
- Launch cost
- —
- LEO capacity
- 21,680 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
5
Launches with a definitive outcome
Success rate
80%
4 of 5
Current success streak
3
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Titan 402B IUS | DSP 22 — Success
- Titan 402B IUS | DSP 21 — Success
- Titan 402B IUS | DSP 20 — Success
- Titan 402B IUS | DSP 19 — Failure
- Titan 402B IUS | DSP 18 — Success