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  2. Focke-Wulf Fw 56 Stösser - Wikipedia

    en.wikipedia.org/wiki/Focke-Wulf_Fw_56_Stösser

    The Focke-Wulf Fw 56 Stösser (German : goshawk) was a single-engine parasol wing monoplane advanced trainer designed and built by the German aircraft manufacturer Focke-Wulf. It was the company's first aircraft to be designed from the onset by the aeronautical engineer Kurt Tank , who also named the type.

  3. .56-56 Spencer - Wikipedia

    en.wikipedia.org/wiki/.56-56_Spencer

    The first 56 is the diameter of the case at the base .56 inches (14.2 mm), measured just past the rim, and the second 56 is the diameter at the case mouth, also 0.56 inches (14 mm). Later versions of the cartridge included the .56-52, .56-50, and .56-46, which had varying degrees of taper in the cases, to accommodate smaller diameter bullets.

  4. Fieseler Fi 156 Storch - Wikipedia

    en.wikipedia.org/wiki/Fieseler_Fi_156_Storch

    The Fieseler Fi 156 Storch (, "stork") is a liaison aircraft designed and produced by the German aircraft manufacturer Fieseler.Its nickname of Storch was derived from the lengthy legs of its main landing gear, which gave the aircraft a similar appearance to that of the long-legged, big-winged bird.

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    Get AOL Mail for FREE! Manage your email like never before with travel, photo & document views. Personalize your inbox with themes & tabs. You've Got Mail!

  6. CFM International CFM56 - Wikipedia

    en.wikipedia.org/wiki/CFM_International_CFM56

    Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.

  7. Allison T56 variants - Wikipedia

    en.wikipedia.org/wiki/Allison_T56_variants

    A T56 on a mobile test unit at MCAS Futenma, 1982 T56-A-1 (Series I) A 1,600 lb weight (730 kg) engine delivering 3,460 shp (2,580 kW) and 725 lbf (329 kgf; 3.22 kN) residual jet thrust, which is equal to 3,750 equivalent shp (2,800 kW); single-shaft 14-stage axial flow compressor, cannular combustion chamber with 6-cylindrical through-flow combustion liners, 4-stage axial flow turbine; 13,800 ...

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