Titan 23C
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
American orbital launch vehicle. Post-MOL standardization of Titan 3C, with man-rated systems removed, upgraded first stage engines, digital avionics, blowdown solid rocket motor thrust vector control in place of pressure-regulated system, simplified Transtage attitude control system.
LEO Payload: 13,100 kg (28,800 lb) to a 185 km orbit. Payload: 3,000 kg (6,600 lb) to a GTO.
Related
- Family
- orbital launch vehicle
- Country
- USA
- Stages
- Titan 3A-1, Titan 3A-2, Titan Transtage, UA1205
- Agency
- Martin