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  2. Northrop Grumman Pegasus - Wikipedia

    en.wikipedia.org/wiki/Northrop_Grumman_Pegasus

    As of 2015, the most recent Pegasus XL to be purchased — a planned June 2017 launch of NASA's Ionospheric Connection Explorer (ICON) mission — had a total cost of US$56.3 million, which NASA notes includes "firm-fixed launch service costs, spacecraft processing, payload integration, tracking, data and telemetry and other launch support ...

  3. List of Launch Services Program launches - Wikipedia

    en.wikipedia.org/wiki/List_of_Launch_Services...

    Launch Date Mission Vehicle Launch Site Total Launch Cost* (million) 1998 [3] 1998.10.24 Deep Space 1: Delta II 7326-9.5 Cape Canaveral Air Force Station Space Launch Complex 17 (CCAFS SLC 17A) 1998.12.06 Submillimeter Wave Astronomy Satellite (SWAS) Pegasus XL: Vandenberg Air Force Base (VAFB) 1998.12.11 Mars Climate Orbiter: Delta II 7425

  4. NASA Launch Services Program - Wikipedia

    en.wikipedia.org/wiki/NASA_Launch_Services_Program

    Expendable launch vehicles can accommodate all types of orbit inclinations and altitudes and are ideal vehicles for launching Earth-orbit and interplanetary missions. The Launch Services Program was established at Kennedy Space Center for NASA's acquisition and program management of expendable launch vehicle missions.

  5. Stargazer (aircraft) - Wikipedia

    en.wikipedia.org/wiki/Stargazer_(aircraft)

    The first Pegasus launch to use Stargazer was conducted on June 27, 1994, as the maiden flight of the Pegasus-XL. Previous launches used the NASA-operated Boeing B-52 nicknamed "Balls 8," which was also used for four subsequent launches, as the original Pegasus could not be launched from Stargazer due to clearance issues.

  6. Submillimeter Wave Astronomy Satellite - Wikipedia

    en.wikipedia.org/wiki/Submillimeter_Wave...

    It was launched on 6 December 1998, at 00:57:54 UTC, from Vandenberg Air Force Base aboard a Pegasus XL launch vehicle. [1] The telescope was designed by the Smithsonian Astrophysical Observatory (SAO) and integrated by Ball Aerospace, while the spacecraft was built by NASA's Goddard Space Flight Center (GSFC). [2]

  7. Pegasus II (rocket) - Wikipedia

    en.wikipedia.org/wiki/Pegasus_II_(rocket)

    The launch system would consist of three primary components: a carrier aircraft, contracted to Scaled Composites; a launch vehicle, originally contracted to SpaceX as a derivative of the Falcon 9 [8] —later contracted to Orbital Sciences as the Pegasus II; and a mating and integration system to enable the aircraft to safely interface with ...

  8. Comparison of solid-fuelled orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_solid...

    Pegasus: 3 United States: Orbital Sciences: 16.9 1.27 18.5 375 1990 10/11 ? Pegasus XL: 3 ... Comparison of space station cargo vehicles; List of space launch system ...

  9. Comparison of orbital launch systems - Wikipedia

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

    All launch vehicle propulsion systems employed to date have been chemical rockets falling into one of three main categories: Solid-propellant rockets or solid-fuel rockets have a motor that uses solid propellants , typically a mix of powdered fuel and oxidizer held together by a polymer binder and molded into the shape of a hollow cylinder.