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  2. Aérospatiale SA 315B Lama - Wikipedia

    en.wikipedia.org/wiki/Aérospatiale_SA_315B_Lama

    Along with the Alouette III, the Cheetah was a key product for HAL; experience from manufacturing the type aided in the later development of more advanced indigenous helicopters such as the HAL Dhruv. [5] During the 1990s, HAL developed an armed light attack helicopter based upon the Cheetah, which was given the name Lancer. [6] [7]

  3. Boeing X-50 Dragonfly - Wikipedia

    en.wikipedia.org/wiki/Boeing_X-50_Dragonfly

    The Boeing X-50A Dragonfly, formerly known as the Canard Rotor/Wing Demonstrator, was a VTOL rotor wing experimental unmanned aerial vehicle that was developed by Boeing and DARPA to demonstrate the principle that a helicopter's rotor could be stopped in flight and act as a fixed wing, enabling it to transition between fixed-wing and rotary-wing flight.

  4. Plane mirror - Wikipedia

    en.wikipedia.org/wiki/Plane_mirror

    A plane mirror is a mirror with a flat reflective surface. [ 1 ] [ 2 ] For light rays striking a plane mirror, the angle of reflection equals the angle of incidence. [ 3 ] The angle of the incidence is the angle between the incident ray and the surface normal (an imaginary line perpendicular to the surface).

  5. Optical landing system - Wikipedia

    en.wikipedia.org/wiki/Optical_landing_system

    The mirror landing aid was a gyroscopically controlled concave mirror on the port side of the flight deck. On either side of the mirror was a line of green coloured "datum lights". A bright orange "source" light was shone into the mirror creating the "ball" (or "meatball" in later USN parlance) which could be seen by the aviator who was about ...

  6. Lancair 235 - Wikipedia

    en.wikipedia.org/wiki/Lancair_235

    Model first flown in 1984, powered by a 100 hp (75 kW) Continental O-200 engine. Overall length is 19.75 ft (6.02 m). [3] Lancair 235 Model introduced in 1985, powered by a 100 to 115 hp (75 to 86 kW) Lycoming O-235 engine. Overall length is 20.00 ft (6.10 m), slightly longer than the 200, due to the engine and mount dimensions. [3] [2]

  7. Lockheed XH-51 - Wikipedia

    en.wikipedia.org/wiki/Lockheed_XH-51

    The Lockheed XH-51 (Model 186) is an American single-engine experimental helicopter designed by Lockheed Aircraft, utilizing a rigid rotor and retractable skid landing gear. The XH-51 was selected as the test vehicle for a joint research program conducted by the United States Army and United States Navy to explore rigid rotor technology.

  8. Transverse-rotor aircraft - Wikipedia

    en.wikipedia.org/wiki/Transverse-rotor_aircraft

    A transverse-rotor aircraft is an aircraft with two large horizontal rotor assemblies mounted side by side. Single-rotor helicopters (unicopters) need an additional tail rotor or tail exhaust to neutralize the reactional angular momentum produced by the main rotor. Transverse rotor helicopters, however, use counter-rotating rotors, with each ...

  9. Lockheed CL-1200 Lancer - Wikipedia

    en.wikipedia.org/wiki/Lockheed_CL-1200_Lancer

    Since the Northrop F-5 was named the winner in November 1970, the primary market for the Lancer was lost, and the project was terminated with no aircraft completed. The X-27 was an experimental designation assigned by the USAF [1] to a proposed high-performance research aircraft derived from the CL-1200 Lancer project. The X-27 was to have ...