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 2-2
Part of Titan LR91 stage series
N2O4/Aerozine-50 propellant rocket stage. .

Status: Study 1961. Thrust: 444.82 kN (99,999 lbf). Gross mass: 28,939 kg (63,799 lb). Unfuelled mass: 2,404 kg (5,299 lb). Specific impulse: 316 s. Specific impulse sea level: 160 s. Burn time: 180 s. Height: 7.86 m (25.78 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 4.640 million.



Country: USA. Engines: LR91-7. Launch Vehicles: Titan II, Soltan, Titan II GLV, Titan 2B, Titan II SLV. Propellants: N2O4/Aerozine-50.

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