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Carl Goldberg Models manufactures radio-controlled (RC) aircraft and components. This company was purchased by Great Planes Model Manufacturing on August 24, 2007. The model shown on the right was in production during negotiations and is considered to be either the last model produced under the previous owner or the first under the new one; it ...
Dynon Avioncs D1 portable EFIS. Dynon Avionics is an American aircraft avionics manufacturer that specializes in non-certified electronic avionics.. Most of Dynon's instruments are not certified under FAA TSO specifications, and are developed for Experimental aircraft, Homebuilt aircraft, and Light Sport aircraft that include the avionics as part of their approved equipment during LSA ...
While primarily designed for jet aircraft, the Epic cockpit is also used on the AgustaWestland AW139 medium helicopter, which is certified for single-pilot IFR operations. [ 2 ] Dassault 's Enhanced Avionics System (EASy) was jointly developed with Honeywell and is based on the Primus Epic .
The Velocity Model 173 SE (Standard Elite) is an entry-level canard pusher aircraft from Velocity Aircraft. [ 1 ] [ 2 ] [ 3 ] The four seat, rear engine aircraft may be powered by a 160 hp (120 kW) Lycoming IO-320 or a 200 hp (150 kW) Lycoming IO-360 engine.
The IBM AP-101B CPU and I/O processor (right) and AP-101S (left) The IBM System/4 Pi is a family of avionics computers used, in various versions, on the F-15 Eagle fighter, E-3 Sentry AWACS, Harpoon Missile, NASA's Skylab, MOL, and the Space Shuttle, as well as other aircraft.
The system's purpose was to ensure that an aircraft's payload of nuclear weapons would detonate in the event of the crew becoming debilitated by enemy defences such as missiles. [1] Once armed, the system would ensure that the onboard nuclear weapons detonated if the aircraft dropped below a predetermined altitude.
The QTR was installed on all production models starting in June 1967 and offered as a kit for previously built aircraft. 1989 Model 269C 269C "Model 300C" The 300C was powered by a 190 hp (141 kW) Lycoming HIO-360-D1A and had a larger diameter main rotor - 26 ft 10 in (8.18 m) compared to 25 ft 4 in (7.72 m).
Gear retraction of a Velocity on takeoff. The Velocity XL is 12 in (310 mm) longer and has a 20 in (510 mm) greater span than the SE. [3] The standard XL has a cruising range of 875 nautical miles (1,620 km; 1,007 mi) and a 75% power cruising speed of 185 knots (213 mph; 343 km/h) air speed.