Titan C-2

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 C-2

LOx/LH2 propellant rocket stage. Engine developed 1958-1960, but launch vehicle cancelled 1961.

AKA: Titan C. Status: Development ended 1961. Thrust: 666.00 kN (149,722 lbf). Gross mass: 57,400 kg (126,500 lb). Unfuelled mass: 6,000 kg (13,200 lb). Specific impulse: 403 s. Specific impulse sea level: 350 s. Burn time: 300 s. Height: 19.50 m (63.90 ft). Diameter: 4.07 m (13.35 ft). Span: 4.07 m (13.35 ft).

Country: USA. Engines: LR87 LH2. Launch Vehicles: Titan C. Propellants: Lox/LH2.

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