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
- 906 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 14,500 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
1
Launches with a definitive outcome
Success rate
100%
1 of 1
Current success streak
1
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 405B | NROL-16 — Success