When.com Web Search

Search results

  1. Results From The WOW.Com Content Network
  2. Terrier Oriole - Wikipedia

    en.wikipedia.org/wiki/Terrier_Oriole

    Terrier Oriole is an unguided two-stage rocket system which is primarily used by the Goddard Space Flight Center out of the Wallops Flight Facility as a sounding rocket.The system uses a Terrier first-stage booster attached to an Oriole second-stage rocket. [3]

  3. SpaceX Merlin - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Merlin

    SpaceX’s Merlin 2 LOX/RP-1-fueled engine on a gas-generator cycle, capable of a projected 7,600 kN (1,700,000 lbf) of thrust at sea level and 8,500 kN (1,920,000 lbf) in a vacuum and would provide the power for conceptual super-heavy-lift launch vehicles from SpaceX, which Markusic dubbed Falcon X and Falcon XX.

  4. Guizhou WS-19 - Wikipedia

    en.wikipedia.org/wiki/Guizhou_WS-19

    The Guizhou WS-19 (Chinese: 涡扇-19), code name Huangshan, is an afterburner turbofan engine designed by the Guizhou Aeroengine Design Institute. It has a reported thrust-to-weight ratio of 10 and a thrust of 10 metric tons or 22,000 lbs. [1] [2]

  5. Aerojet 260 - Wikipedia

    en.wikipedia.org/wiki/Aerojet_260

    The SL-3 motor was also test-fired using improvements based on the two previous firings. It resulted in the largest single motor ever fired on Earth at 5.6 million pounds (26.2 meganewtons) of thrust. Since SL-3 used the same casing design and materials as the previous boosters, the change in thrust was obtained from adding a nozzle to the end.

  6. SGI Onyx2 - Wikipedia

    en.wikipedia.org/wiki/SGI_Onyx2

    The Onyx2, code name Kego, is a family of visualization systems developed and manufactured by SGI, introduced in 1996 to succeed the Onyx. The Onyx2's basic system architecture is based on the Origin 2000 servers, but with the inclusion of graphics hardware. In 2000, the Onyx2 was succeeded by the Onyx 3000, and

  7. General Electric XA102 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_XA102

    The three-stream adaptive cycle design can direct air to the bypass third stream for increased fuel efficiency and cooling or to the core and fan streams for additional thrust and performance. The engine thrust has not been disclosed, although it is speculated by aviation reporters to be in the 35,000–40,000 lbf (156–178 kN) thrust class. [2]

  8. Falcon 9 v1.0 - Wikipedia

    en.wikipedia.org/wiki/Falcon_9_v1.0

    The Falcon 9 v1.0 first stage was used on the first five Falcon 9 launches, and powered by nine SpaceX Merlin 1C rocket engines arranged in a 3x3 pattern. Each of these engines had a sea-level thrust of 556 kN (125,000 pounds-force) for a total thrust on liftoff of about 5,000 kN (1,100,000 pounds-force).

  9. SpaceX Super Heavy - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Super_Heavy

    Super Heavy is the reusable first stage of the SpaceX Starship super heavy-lift launch vehicle, which it composes in combination with the Starship second stage.As a part of SpaceX's Mars colonization program, the booster evolved into its current design over a decade.