Titan 34D

Tip : Don't hit AG8!

American orbital launch vehicle. Stretched Titan core designed for use with 5 1/2 segment solid rocket motors. IUS (Interim/Inertial Upper Stage) solid upper stages, Transtage, or used without upper stages.
Status: Retired 1988. First Launch: 1983-06-20. Last Launch: 1988-11-06. Number: 7 . Payload: 14,515 kg (32,000 lb). Thrust: 11,279.10 kN (2,535,643 lbf). Gross mass: 723,490 kg (1,595,020 lb). Height: 50.00 m (164.00 ft). Diameter: 3.05 m (10.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 14,515 kg (32,000 lb) to a 185 km orbit. Payload: 5,000 kg (11,000 lb) to a GTO. Launch Price $: 150.000 million in 1985 dollars.

Stage Data - Titan 34D

Stage 0. 2 x Titan UA1206. Gross Mass: 251,427 kg (554,301 lb). Empty Mass: 40,827 kg (90,008 lb). Thrust (vac): 6,226.997 kN (1,399,885 lbf). Isp: 265 sec. Burn time: 114 sec. Isp(sl): 240 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 27.56 m (90.41 ft). Propellants: Solid. No Engines: 1. Engine: UA1206. Status: Out of Production.
Stage 1. 1 x Titan 3B-1. Gross Mass: 139,935 kg (308,503 lb). Empty Mass: 7,000 kg (15,400 lb). Thrust (vac): 2,413.191 kN (542,507 lbf). Isp: 302 sec. Burn time: 161 sec. Isp(sl): 250 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 23.99 m (78.70 ft). Propellants: N2O4/Aerozine-50. No Engines: 2. Engine: LR-87-11. Status: In Production.
Stage 2. 1 x Titan 3B-2. Gross Mass: 37,560 kg (82,800 lb). Empty Mass: 2,900 kg (6,300 lb). Thrust (vac): 460.314 kN (103,483 lbf). Isp: 316 sec. Burn time: 230 sec. Isp(sl): 145 sec. Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft). Length: 8.60 m (28.20 ft). Propellants: N2O4/Aerozine-50. No Engines: 1. Engine: LR-91-11. Status: In Production.
Stage 3. 1 x TOS. Gross Mass: 10,960 kg (24,160 lb). Empty Mass: 1,130 kg (2,490 lb). Thrust (vac): 185.100 kN (41,612 lbf). Isp: 296 sec. Burn time: 144 sec. Isp(sl): 115 sec. Diameter: 2.34 m (7.67 ft). Span: 2.34 m (7.67 ft). Length: 3.29 m (10.79 ft). Propellants: Solid. No Engines: 1. Engine: SRM-1. Other designations: Transfer Orbit Stage. Status: In Production. Comments: IUS-2 stage with simplified electronics.
Stage 3. 1 x IUS-1. Gross Mass: 10,841 kg (23,900 lb). Empty Mass: 1,134 kg (2,500 lb). Thrust (vac): 181.501 kN (40,803 lbf). Isp: 296 sec. Burn time: 152 sec. Isp(sl): 220 sec. Diameter: 2.34 m (7.67 ft). Span: 2.34 m (7.67 ft). Length: 3.52 m (11.54 ft). Propellants: Solid. No Engines: 1. Engine: SRM-1. Other designations: Orbus 21D. Status: In Production.
Stage 4. 1 x IUS-2. Gross Mass: 3,919 kg (8,639 lb). Empty Mass: 1,170 kg (2,570 lb). Thrust (vac): 78.413 kN (17,628 lbf). Isp: 304 sec. Burn time: 103 sec. Isp(sl): 200 sec. Diameter: 1.61 m (5.28 ft). Span: 1.61 m (5.28 ft). Length: 2.08 m (6.82 ft). Propellants: Solid. No Engines: 1. Engine: SRM-2. Other designations: TOS. Status: In Production.

From : Astronautix