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 3L4
Part of Titan
Titan 3L4 Credit: © Mark Wade |
American orbital launch vehicle. Variant of Titan with 15 foot Large Diameter Core, 4 x 7 segment strap-ons. Man rated, optimized for delivery of 40,000 pound manned payloads into 250 nm / 50 deg space station orbit.
Status: Study 1965. Payload: 45,000 kg (99,000 lb). Thrust: 25,642.10 kN (5,764,573 lbf). Gross mass: 1,747,580 kg (3,852,750 lb). Height: 63.00 m (206.00 ft). Diameter: 4.57 m (14.99 ft). Apogee: 185 km (114 mi).
LEO Payload: 45,000 kg (99,000 lb) to a 185 km orbit. Payload: 16,000 kg (35,000 lb) to a GTO. Launch Price $: 38.000 million in 1965 dollars.
Stage Data - Titan 3L4
- Stage 0. 4 x Titan UA1207. Gross Mass: 319,330 kg (704,000 lb). Empty Mass: 51,230 kg (112,940 lb). Thrust (vac): 7,116.999 kN (1,599,965 lbf). Isp: 272 sec. Burn time: 120 sec. Isp(sl): 245 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 34.14 m (112.00 ft). Propellants: Solid. No Engines: 1. Engine: UA1207. Status: In Production.
- Stage 1. 1 x Titan LDC-1. Gross Mass: 350,000 kg (770,000 lb). Empty Mass: 20,000 kg (44,000 lb). Thrust (vac): 4,344.463 kN (976,674 lbf). Isp: 296 sec. Burn time: 210 sec. Isp(sl): 258 sec. Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft). Length: 29.90 m (98.00 ft). Propellants: N2O4/Aerozine-50. No Engines: 4. Engine: LR-87-7. Status: Study 1965. Comments: 15 foot diameter core Titan proposed in 1960's for space station logistics. Masses estimated.
- Stage 2. 1 x Titan LDC-2. Gross Mass: 50,000 kg (110,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 444.819 kN (99,999 lbf). Isp: 316 sec. Burn time: 320 sec. Isp(sl): 160 sec. Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft). Length: 13.40 m (43.90 ft). Propellants: N2O4/Aerozine-50. No Engines: 1. Engine: LR-91-7. Status: Study 1965. Comments: 15 foot diameter core Titan proposed in 1960's for space station logistics. Masses estimated.
- Stage 3. 1 x Centaur D/E. Gross Mass: 16,258 kg (35,842 lb). Empty Mass: 2,631 kg (5,800 lb). Thrust (vac): 131.222 kN (29,500 lbf). Isp: 444 sec. Burn time: 470 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 9.60 m (31.40 ft). Propellants: Lox/LH2. No Engines: 2. Engine: RL-10A-3. Status: Out of Production.
Family:
orbital launch vehicle.
Country:
USA.
Engines:
LR87-7,
LR91-7,
RL-10A-3.
Stages:
Titan LDC-1,
Titan LDC-2,
Centaur D/E,
UA1207.
Agency:
Martin.
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