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  2. Yakovlev Yak-25 - Wikipedia

    en.wikipedia.org/wiki/Yakovlev_Yak-25

    The aircraft's fixed windshield included a 105-millimeter (4.1 in)-thick bulletproof glass panel, while the rest of the aircraft was protected by 10-millimeter (0.39 in) all-round armor plates. [2] The aircraft was armed with two 37 mm NL-37L cannon, mounted low on the sides of the center fuselage. A supply of 50 rounds per gun was typically ...

  3. Sukhoi Su-25 - Wikipedia

    en.wikipedia.org/wiki/Sukhoi_Su-25

    After testing, the aircraft went into series production in 1978 in Tbilisi in the Georgian Soviet Socialist Republic. Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-towing, and the Su-25K for export customers. Some aircraft were upgraded to the Su-25SM standard in 2012.

  4. Kamov Ka-25 - Wikipedia

    en.wikipedia.org/wiki/Kamov_Ka-25

    Kamov Ka-25K in Aeroflot markings at the 1967 Paris Air Show Ka-25K Civilian flying crane helicopter with a gondola under the lengthened nose for controlling slung loads up to 2,000 kilograms (4,400 lb). Fitted with electrically de-iced rotor blades and optional seats for 12 passengers. A single prototype (SSSR-21110) flown in 1966. Ka-25PS

  5. List of Sukhoi Su-25 operators - Wikipedia

    en.wikipedia.org/wiki/List_of_Sukhoi_Su-25_operators

    [15] 5 Su-25K and 1 Su-25UBK in service as of 2024. [16] Chad. The Chadian Air Force took delivery of six aircraft (four Su-25s and two Su-25UBs) from Ukraine between 2008 and 2010. Four additional aircraft were delivered from Ukraine in 2013. [17] Democratic Republic of the Congo. Air Force of the Democratic Republic of the Congo.

  6. 463L master pallet - Wikipedia

    en.wikipedia.org/wiki/463L_master_pallet

    The "SS-463L" project was developed by a U.S. Air Force committee in 1957 and awarded to the Douglas Aircraft Company in 1959. The "SS-463L Pallet Cargo Handling System" specifications for aircraft (aka "463L") included a "Master Pallet" design to meet a component of the material handling specifications of this system.

  7. Wing loading - Wikipedia

    en.wikipedia.org/wiki/Wing_loading

    Wing loading is a useful measure of the stalling speed of an aircraft. Wings generate lift owing to the motion of air around the wing. Larger wings move more air, so an aircraft with a large wing area relative to its mass (i.e., low wing loading) will have a lower stalling speed.

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