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Titan 23C

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Titan 23C Part of Titan 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. AKA: SLV-5C. Status: Out of production. Payload: 13,100 kg (28,800 lb). Thrust: 10,586.80 kN (2,380,007 lbf). Gross mass: 626,190 kg (1,380,510 lb). Height: 42.00 m (137.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi). LEO Payload: 13,100 kg (28,800 lb) to a 185 km orbit. Payload: 3,000 kg (6,600 lb) to a GTO. Family: orbital launch vehicle. Country: USA. Stages: Titan 3A-1, Titan 3A-2, Titan Transtage, UA1205. Agency: Martin. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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