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Delta II A Delta II launch vehicle launches from Cape Canaveral carrying the Dawn spacecraft. Function Launch vehicle Manufacturer United Launch Alliance Country of origin United States Cost per launch US$51 million in 1987 (7920-10 model) US$137 million in 2018 before retirement Size Height 38.9 m (128 ft) Diameter 2.44 m (8 ft 0 in) Mass 152,000–286,000 kg (335,000–631,000 lb) Stages 2 ...
Delta II was an expendable launch system, originally designed and built by McDonnell Douglas, and sometimes known as the Thorad Delta 1. Delta II was part of the Delta rocket family, derived directly from the Delta 3000 , and entered service in 1989.
The Delta rocket family was a versatile range of American rocket-powered expendable launch systems that provided space launch capability in the United States from 1960 to 2024. Japan also launched license-built derivatives ( N-I , N-II , and H-I ) from 1975 to 1992.
This is a list of launches made by the PGM-17 Thor IRBM, and its derivatives, including the Delta family and the Japanese N-I, N-II and H-I rockets which were based on license-produced components. Due to the number of launches, it has been split by decade: List of Thor and Delta launches (1957–1959) List of Thor and Delta launches (1960–1969)
Delta II 7920-10C VAFB SLC-2 MS-1 LEO: Iridium: Success Five Iridium satellites 243 May 20, 1997 22:39 Delta II 7925-9.5 CCAFS LC-17A Telenor Thor II: 1,467 kg GTO: Telenor: Success Hughes HS 376 satellite 244 July 9, 1997 13:04 Delta II 7920-10C VAFB SLC-2W MS-2 LEO: Iridium: Success Five Iridium satellites 245 July 23, 1997 03:43 Delta II ...
The US Air Force transferred Launch Complex 17A to NASA (SLC-17A) in 1965, but the site was returned to the US Air Force in 1988 to support the Delta II program. As Delta II launches continued over the next decades, Pad 17B was modified in 1997 to support a new, more powerful launch vehicle, the Delta III, which made its maiden flight from the ...
First Delta II launch 1989-03-24 21:50 Delta 3920-8 183 CCAFS LC-17B: Delta Star (USA-36) Experimental on-orbit ASAT test satellite LEO: Success 1989-06-10 22:30 Delta II 6925 185 CCAFS LC-17A: NAVSTAR II-2: GPS Block II navigation satellite MEO: Success 1989-08-18 05:58 Delta II 6925 186 CCAFS LC-17A: NAVSTAR II-3: GPS Block II navigation ...
GPS IIR-1 or GPS SVN-42 was the first Block IIR GPS satellite to be launched. It was to have been operated as part of the United States Air Force Global Positioning System.It was launched on 17 January 1997, and was destroyed 13 seconds into its flight due to a malfunction of the Delta II launch vehicle that was carrying it. [2]