Titan II SLV
Titan familyLockheed MartinRetired
The Titan 23G, Titan II(23)G, Titan 2(23)G or Titan II SLV was an American expendable launch system derived from the LGM-25C Titan II intercontinental ballistic missile. Retired Titan II missiles were converted by Martin Marietta, into which the Glenn L. Martin Company, which built the original Titan II, had merged. It was used to carry payloads for the United States Air Force, NASA and NOAA. Thirteen were launched from Space Launch Complex 4W at the Vandenberg Air Force Base between 1988 and 2003.
Specifications
- Thrust
- 1,900 kN
- Height
- 31.4 m
- Diameter
- 3.05 m
- Launch mass
- 117 t
- Stages
- 3
- LEO capacity
- 3,600 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
First flight September 5, 1988 · latest October 18, 2003
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Titan II SLV flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1988 | 1 | 0 | 1 |
| 1989 | 1 | 0 | 1 |
| 1990 | 0 | 0 | 0 |
| 1991 | 0 | 0 | 0 |
| 1992 | 1 | 0 | 1 |
| 1993 | 0 | 1 | 1 |
| 1994 | 1 | 0 | 1 |
| 1995 | 0 | 0 | 0 |
| 1996 | 0 | 0 | 0 |
| 1997 | 1 | 0 | 1 |
| 1998 | 1 | 0 | 1 |
| 1999 | 2 | 0 | 2 |
| 2000 | 1 | 0 | 1 |
| 2001 | 0 | 0 | 0 |
| 2002 | 1 | 0 | 1 |
| 2003 | 2 | 0 | 2 |