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Titan 34D/IUS

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Status: Retired 1982. First Launch: 1982-10-30. Last Launch: 1982-10-30. Number: 1 . Payload: 5,000 kg (11,000 lb). Thrust: 11,280.00 kN (2,535,840 lbf). Gross mass: 725,000 kg (1,598,000 lb). Height: 52.40 m (171.90 ft). Diameter: 3.05 m (10.00 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 5,000 kg (11,000 lb). Payload: 5,000 kg (11,000 lb) to a GTO.

• Interim Upper Stage to be used with the Titan III - .

  A joint DOD/NASA study was carried out on the consolidation of expendable launch vehicles during transition to the space shuttle. The study recommended that the Interim Upper Stage, being developed for the space shuttle, be used with the Titan III during the transition period.

• DSCS II-15 - . Payload: DSCS II F-15. Mass: 562 kg (1,238 lb). 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: 11.30 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. Mass: 2,613 kg (5,760 lb). 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: 8.80 deg. Period: 1,454.80 min. 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..