Titan 34D Transtage
Titan familyLockheed MartinRetired
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
- GTO capacity
- 5,000 kg
- GEO capacity
- 1,900 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
7flightswith a definitive outcome
100%success rate7 of 7
0failuresincluding partial failures
7success streakcurrent
First flight January 31, 1984 · latest September 4, 1989
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Titan 34D Transtage flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1984 | 3 | 0 | 3 |
| 1985 | 0 | 0 | 0 |
| 1986 | 0 | 0 | 0 |
| 1987 | 1 | 0 | 1 |
| 1988 | 1 | 0 | 1 |
| 1989 | 2 | 0 | 2 |