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  2. Trolling motor - Wikipedia

    en.wikipedia.org/wiki/Trolling_motor

    A trolling motor is a self-contained marine propulsion unit that includes an electric motor, propeller and control system, and is affixed to an angler's boat, either at the bow or stern. A gasoline-powered outboard used in trolling , if it is not the vessel's primary source of propulsion, may also be referred to as a trolling motor.

  3. Microturbo TRS 18 - Wikipedia

    en.wikipedia.org/wiki/Microturbo_TRS_18

    Includes an engine driven alternator and fuel and oil lubrication pumps. Dry weight as 18-046. Take-off thrust increased to 1.15 kN (260 lb st) and maximum continuous thrust to 1.10 kN (247 lb st). TRS 18-076 Intended for the Meteor-Mirach 100. Includes an engine driven alternator and fuel and oil lubrication pumps. Dry weight as 18-046.

  4. MS400 turbofan engine - Wikipedia

    en.wikipedia.org/wiki/MS400_turbofan_engine

    The MS400 (Ukrainian: MC-400) is a turbofan engine developed by the Ukrainian aircraft engine manufacturer Motor Sich. [ 1 ] [ 2 ] The engine is used for subsonic unmanned air vehicles. Specification

  5. Pratt & Whitney PW1000G - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_PW1000G

    The PW1400G has a cruise Thrust-specific fuel consumption of 0.51 lb/lbf/h (14.4 g/kN/s). [ 48 ] The 30,000-horsepower (22,000-kilowatt) gearbox is designed as a lifetime item with no scheduled maintenance other than changing oil. [ 42 ]

  6. Model rocket motor classification - Wikipedia

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

    The designation for a specific motor looks like C6-3.In this example, the letter (C) represents the total impulse range of the motor, the number (6) before the dash represents the average thrust in newtons, and the number (3) after the dash represents the delay in seconds from propelling charge burnout to the firing of the ejection charge (a gas generator composition, usually black powder ...

  7. Saturn AL-31 - Wikipedia

    en.wikipedia.org/wiki/Saturn_AL-31

    The design of the AL-31 turbofan began in the 1970s under the designation izdeliye 99 [N 1] by the Lyulka design bureau, also known as Lyulka-Saturn. With an emphasis on greater fuel efficiency over turbojets for longer range, the 12.5 tonnes-force (122.6 kN; 27,560 lbf) class turbofan engine was intended to power the heavy PFI (Russian: ПФИ, short for: перспективного ...