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  2. Delta II - Wikipedia

    en.wikipedia.org/wiki/Delta_II

    On 14 December 2006, with the launch of USA-193, was the first launch of the Delta II operated by United Launch Alliance. [15] The last GPS launch aboard a Delta II and the final launch from SLC-17A at Cape Canaveral occurred in 2009. The GRAIL Launch in 2011 marked the last Delta II Heavy launch and the last from Florida.

  3. List of Delta II launches - Wikipedia

    en.wikipedia.org/wiki/List_of_Delta_II_launches

    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 ...

  4. Delta (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Delta_(rocket_family)

    A Delta 2310 was the vehicle for the first three-satellite launch of NOAA-4, Intasat, and AMSAT-OSCAR 7 on 15 November 1974. [citation needed] Delta 2910 boosters were used to launch both Landsat 2 in 1975 and Landsat 3 in 1978. On 7 April 1978, a Delta 2914 launched "Yuri 1", the first Japanese BSE Broadcasting Satellite. [12]

  5. GPS IIR-1 - Wikipedia

    en.wikipedia.org/wiki/GPS_IIR-1

    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]

  6. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Vehicle Origin Manufacturer Height Maximum payload mass (kg) Reusable / Expendable Orbital launches including failures [a] Launch site(s) Dates of flight LEO GTO Other First Latest Angara A5 / Briz-M Russia: Khrunichev: 48.7 m 24,500 [1] 5,200 [1] 2,800 to GEO [1] Expendable: 2 [1] Plesetsk, Vostochny: 2014 2020 Angara-1.2 Russia: Khrunichev ...

  7. Vulcan Centaur - Wikipedia

    en.wikipedia.org/wiki/Vulcan_Centaur

    Two of the 2,400-kilonewton (550,000 lbf)-thrust BE-4 engines were to be used on a new launch vehicle booster. [35] [36] [34] A month later, ULA restructured company processes and its workforce to reduce costs. The company said that the successor to Atlas V would blend existing Atlas V and Delta IV with a goal of halving the cost of the Atlas V ...

  8. Comparison of orbital launcher families - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Cost: Price for a launch at this time, in millions of US$ Launches reaching... Total: Flights which lift-off, or where the vehicle is destroyed during the terminal count Note: only includes orbital launches (flights launched with the intention of reaching orbit). Suborbital tests launches are not included in this listing.

  9. Delta IV - Wikipedia

    en.wikipedia.org/wiki/Delta_IV

    The Delta IV Medium+ (5,2) (Delta 9250) was similar to the Medium+ (4,2), but had a 5-m–diameter DCSS and payload fairing for larger payloads. Because of the extra weight of the larger payload fairing and second stage, the Medium+ (5,2) could launch 5,072 kg to GTO. [7]