Titan 1-2 (original) (raw)

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 1-2

Part of Titan LR91 stage series

LOx/Kerosene propellant rocket stage. .

Status: Study 1958. Thrust: 355.86 kN (80,001 lbf). Gross mass: 28,939 kg (63,799 lb). Unfuelled mass: 1,725 kg (3,802 lb). Specific impulse: 308 s. Specific impulse sea level: 210 s. Burn time: 225 s. Height: 9.80 m (32.10 ft). Diameter: 2.26 m (7.41 ft). Span: 2.26 m (7.41 ft).

Cost $ : 4.000 million.

Country: USA. Engines: LR91-3. Launch Vehicles: Titan I, Super-Jupiter, Juno V-A. Propellants: Lox/Kerosene.

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