enow.com Web Search

  1. Ad

    related to: 30 pound thrust to horsepower transfer system for small engine repair class
    • About Us

      Learn More About Us And How We Can

      Assist Your Industrial Needs

    • Contact Us

      Contact Us To Learn More About Our

      Industrial Products

Search results

  1. Results from the WOW.Com Content Network
  2. Model rocket motor classification - Wikipedia

    en.wikipedia.org/wiki/Model_rocket_motor...

    Where is the burn time in seconds, is the instantaneous thrust in newtons, is average thrust in newtons, and is the total impulse in newton seconds. Class A is from 1.26 newton-seconds (conversion factor 4.448 N per lb. force) to 2.5 N·s, and each class is then double the total impulse of the preceding class, with Class B being 2.51 to 5.00 N·s.

  3. Williams FJ33 - Wikipedia

    en.wikipedia.org/wiki/Williams_FJ33

    The FJ33 has a dry weight of less than 300 lb (140 kg), overall diameter of 18.36 in (466 mm), 38.43 in (976 mm) overall length, and produces between 1,000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust.

  4. General Electric CJ610 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CJ610

    The General Electric CJ610 is a non-afterburning turbojet engine derived from the military J85, and is used on a number of civilian business jets.The model has logged over 16.5 million hours of operation.

  5. Pratt & Whitney Canada PW600 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW600

    The 2,500 lbf (11 kN) thrust PW625F demonstrator engine was first run on 31 October 2001. [1] It flew in late 2002. [2] In 2002, the PW610F was selected for the Eclipse 500 twinjet, replacing the EJ22 as Williams was unable to reach sufficient reliability. The 950 lbf (4.2 kN) thrust engine was certified by Transport Canada on 27 July 2006. [3]

  6. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN).

  7. Teledyne CAE J402 - Wikipedia

    en.wikipedia.org/wiki/Teledyne_CAE_J402

    The Teledyne CAE J402 is an American small turbojet engine. Several variants have been developed to power unmanned air vehicles such as missiles and target drones. Developed in the 1970s for the Harpoon anti-ship missile, the J402 was the first jet engine to be designed as a "wooden round", meaning that the engine had to be able to sit for long periods without maintenance or inspection and ...

  8. Williams F107 - Wikipedia

    en.wikipedia.org/wiki/Williams_F107

    The Williams F107 (company designation WR19) is a small turbofan engine made by Williams International.The F107 was designed to propel cruise missiles.It has been used as the powerplant for the AGM-86 ALCM, and BGM-109 Tomahawk, as well as the experimental Kaman KSA-100 SAVER and Williams X-Jet flying platform.

  9. Pratt & Whitney Canada PW300 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW300

    The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...

  1. Ad

    related to: 30 pound thrust to horsepower transfer system for small engine repair class