Titan 2B
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
American intercontinental ballistic orbital launch vehicle. Space launch version of Titan 2 ICBM, obtained through minimal modification of ICBM (new wiring and avionics only, and use of existing ICBM re-entry vehicle shroud). Proposed in the late 1980's but never developed.
LEO Payload: 3,175 kg (6,999 lb) to a 185 km orbit at 28.60 degrees.
Related
- Family
- ICBM, orbital launch vehicle
- Country
- USA
- Agency
- Martin