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 LDC-1
Part of Titan LR87 stage series Family
N2O4/Aerozine-50 propellant rocket stage. 15 foot diameter core Titan proposed in 1960's for space station logistics. Masses estimated.

Status: Study 1965. Thrust: 4,344.46 kN (976,674 lbf). Gross mass: 350,000 kg (770,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 296 s. Specific impulse sea level: 258 s. Burn time: 210 s. Height: 29.90 m (98.00 ft). Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft).

Cost $ : 11.600 million. No Engines: 4.



Country: USA. Engines: LR87-7. Launch Vehicles: Titan 3L2, Titan 3L4. Propellants: N2O4/Aerozine-50.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use