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Crossbow Technology was founded in August, 1995. [4] The company's initial vision was to leverage microelectromechanical systems-based sensor technology for motion-based input devices which are now used in video game systems such as the Nintendo Wii.
The Pro-Composites Vision is an American amateur-built aircraft, designed by Steve Rahm and produced by Pro-Composites of Buffalo Grove, Illinois. The aircraft is supplied in the form of plans for amateur construction, with some pre-formed parts made available to speed construction.
The 175 was designed to fill a niche between the Cessna 172 and the slightly heavier, larger and faster Cessna 182. The engine of the 175, a reduction drive or geared version of the O-300 (Continental GO-300) used in the 172, is rated at 175 hp (130 kW), or 30 hp (22 kW) more than the engine offered in the contemporary 172. Between 1958 and ...
The AN/PVS-14 Monocular Night Vision Device (MNVD) is in widespread use by the United States Armed Forces as well as NATO allies around the world. [3] It uses a third generation image intensifier tube, and is primarily manufactured by Litton Industries (Now L-3 Warrior Systems) and Elbit Systems of America (formerly Harris Night Vision, formerly Exelis, formerly ITT [4]). [5]
The 175 mm (6.9 in) diesel engine driven T235 self-propelled gun and 203 mm (8.0 in) T236 self-propelled howitzer, aside from the different armament, were essentially the same vehicle. They were introduced into U.S. Army service as the M107 and M110 in 1962 and 1963, respectively.
A 1951 USAF resolution test chart is a microscopic optical resolution test device originally defined by the U.S. Air Force MIL-STD-150A standard of 1951. The design provides numerous small target shapes exhibiting a stepped assortment of precise spatial frequency specimens.
The Franklin O-175 (company designation 4AC-176) was an American air-cooled aircraft engine of the 1940s. The engine was of horizontally-opposed four-cylinder and displaced 175 cu in (2.9 L). The power output was nominally 80 hp (60 kW). A later variant was designated O-180, despite sharing the same displacement.
Data from EASA Type certificate and Airbus Helicopters website General characteristics Crew: 2 Capacity: 12-18 pax Length: 18.06 m (59 ft 3 in) rotors running 15.68 m (51 ft) nose to tail rotor disc Height: 5.34 m (17 ft 6 in) to tail rotor tip Empty weight: 4,603 kg (10,148 lb) Gross weight: 7,500 kg (16,535 lb) Max takeoff weight: 7,800 kg (17,196 lb) Fuel capacity: 2,710 L (720 US gal; 600 ...