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 3BAS2
Part of Titan
Titan 3BAS
Titan 3BAS
Credit: © Mark Wade
American orbital launch vehicle. Configuration of Titan 3B proposed by Martin in mid-1960's. Titan 3B for deep space missions with Centaur upper stage, Algol strapons for liftoff thrust augmentation. Never flown.

Status: Study 1965. Payload: 6,600 kg (14,500 lb). Thrust: 3,024.00 kN (679,822 lbf). Gross mass: 225,650 kg (497,470 lb). Height: 52.00 m (170.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 6,600 kg (14,500 lb) to a 185 km orbit. Payload: 1,900 kg (4,100 lb) to a GTO. Launch Price $: 14.000 million in 1965 dollars.

Stage Data - Titan 3BAS2



Family: orbital launch vehicle. Country: USA. Engines: RL-10A-3, LR87-11, LR91-11. Stages: Algol 2, Titan 3B-1, Titan 3B-2, Centaur D/E, Star 37. Agency: Martin.

1960 - . LV Family: Titan. Launch Vehicle: Titan 3BAS2.

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