American orbital launch vehicle. Version of Titan 34D with IUS upper stages.
LEO Payload: 5,000 kg (11,000 lb). Payload: 5,000 kg (11,000 lb) to a GTO.
Gross mass: 725,000 kg (1,598,000 lb).
More... - Chronology...
Payload: 5,000 kg (11,000 lb).
Height: 52.40 m (171.90 ft).
Diameter: 3.05 m (10.00 ft).
Thrust: 11,280.00 kN (2,535,840 lbf).
Apogee: 40,000 km (24,000 mi).
First Launch: 1982.10.30.
Number: 1 .
DSCS II American military communications satellite. 15 launches, 1971.11.03 (DSCS II-01) to 1982.10.30 (DSCS II-15). DSCS provided secure voice and data communications for the US military. More...
DSCS III American military communications satellite. 15 launches, 1982.10.30 (DSCS III-01) to 2003.08.29 (USA 170). DSCS satellites provided secure voice and data communications for the US military. More...
Titan The Titan launch vehicle family was developed by the United States Air Force to meet its medium lift requirements in the 1960's. The designs finally put into production were derived from the Titan II ICBM. Titan outlived the competing NASA Saturn I launch vehicle and the Space Shuttle for military launches. It was finally replaced by the USAF's EELV boosters, the Atlas V and Delta IV. Although conceived as a low-cost, quick-reaction system, Titan was not successful as a commercial launch vehicle. Air Force requirements growth over the years drove its costs up - the Ariane using similar technology provided lower-cost access to space. More...
Associated Manufacturers and Agencies
Martin American manufacturer of rockets, spacecraft, and rocket engines. Martin Marietta Astronautics Group (1956), Denver, CO, USA. More...
Associated Launch Sites
Cape Canaveral America's largest launch center, used for all manned launches. Today only six of the 40 launch complexes built here remain in use. Located at or near Cape Canaveral are the Kennedy Space Center on Merritt Island, used by NASA for Saturn V and Space Shuttle launches; Patrick AFB on Cape Canaveral itself, operated the US Department of Defense and handling most other launches; the commercial Spaceport Florida; the air-launched launch vehicle and missile Drop Zone off Mayport, Florida, located at 29.00 N 79.00 W, and an offshore submarine-launched ballistic missile launch area. All of these take advantage of the extensive down-range tracking facilities that once extended from the Cape, through the Caribbean, South Atlantic, and to South Africa and the Indian Ocean. More...
Cape Canaveral LC40 Titan launch complex. Constructed as part of the Titan Integrate-Transfer-Launch (ITL) facility at the north end of Cape Canaveral in the early 1960s. Supported a wide variety of military space missions involving Titan IIIC, Titan 34D and Titan IV vehicles. More...
IUS-2 Solid propellant rocket stage. Loaded/empty mass 3,919/1,170 kg. Thrust 78.41 kN. Vacuum specific impulse 304 seconds. More...
Titan 3A-1 N2O4/Aerozine-50 propellant rocket stage. Loaded/empty mass 116,573/5,443 kg. Thrust 2,339.76 kN. Vacuum specific impulse 302 seconds. More...
Titan 3A-2 N2O4/Aerozine-50 propellant rocket stage. Loaded/empty mass 29,188/2,653 kg. Thrust 453.71 kN. Vacuum specific impulse 316 seconds. More...
Titan UA1206 Solid propellant rocket stage. Loaded/empty mass 251,427/40,827 kg. Thrust 6,227.00 kN. Vacuum specific impulse 265 seconds. More...
TOS Solid propellant rocket stage. Loaded/empty mass 10,960/1,130 kg. Thrust 185.10 kN. Vacuum specific impulse 296 seconds. IUS-2 stage with simplified electronics. More...
Titan 34D/IUS Chronology
1982 October 30 -
04:05 GMT - .
: Cape Canaveral
. Launch Complex
: Cape Canaveral LC40
. LV Family
. Launch Vehicle
: Titan 34D/IUS
. LV Configuration
: Titan 34D/IUS 34D-1 (04D-5?).
- DSCS II-15 - .
Payload: DSCS II F-15. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS II. Completed Operations Date: 1997-05-23 . USAF Sat Cat: 13636 . COSPAR: 1982-106A. Apogee: 37,332 km (23,196 mi). Perigee: 37,277 km (23,162 mi). Inclination: 11.3000 deg. Period: 1,514.40 min. Positioned in geosynchronous orbit at 15 deg W in 1983-1987; 66 deg E in 1987; 60 deg E in 1987-1994; 65 deg E in 1994-1997 As of 5 September 2001 located at 114.00 deg W drifting at 18.661 deg W per day. As of 2007 Mar 9 located at 172.94E drifting at 18.658W degrees per day. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).
- DSCS III-01 - .
Payload: DSCS III F-1. Nation: USA. Agency: USAF. Program: DSCS. Class: Communications. Type: Military communications satellite. Spacecraft: DSCS III. USAF Sat Cat: 13637 . COSPAR: 1982-106B. Apogee: 36,171 km (22,475 mi). Perigee: 36,132 km (22,451 mi). Inclination: 8.8000 deg. Period: 1,454.80 min. Summary: Positioned in geosynchronous orbit at 105 deg W in 1982-1983; 135 deg W in 1983-1989; 130 deg W in 1989-1999. As of 2006 Sep 9 located at 94.39E drifting at 5.469W degrees per day..
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