The Titan 34D was a United States expendable launch vehicle used to launch a number of satellites for military applications.
Specifications
- Thrust
- 11,280 kN
- Height
- 50 m
- Diameter
- 3.05 m
- Launch mass
- 720 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- —
- GTO capacity
- 5,000 kg
- GEO capacity
- 1,900 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
7
Launches with a definitive outcome
Success rate
100%
7 of 7
Current success streak
7
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 34D Transtage | DSCS-2 15 — Success
- Titan 34D Transtage | Mercury 13 — Success
- Titan 34D Transtage | Mercury 12 — Success
- Titan 34D Transtage | DSP F13 — Success
- Titan 34D Transtage | DSP F12 — Success