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The Samson Mite is a 75% scale version of the original Wolf Samson replica and was originally powered by a 150 hp (110 kW) Rotec R3600 engine driving a 86 in (220 cm) Whirl Wind propeller. [ 7 ] [ 8 ] The aircraft has a wing area of 110 sq ft (10 m 2 ) and features ailerons on the bottom wings. [ 7 ]
MH-139 Grey Wolf: Italy utility: MH-139: 79 aircraft (maximum number of aircraft planned for deployment) Of these, 4 are deployed and the remaining 75 are on order. [4] UH-1N Iroquois: United States utility 63 63 UH-1N total force as of September 2023 (USAF Almanac). [1] 64 UH-1N operational (WAF 2025). [2] V-22 Osprey: United States CSAR CV ...
Common rifle cartridges, from the largest .50 BMG to the smallest .22 Long Rifle with a $1 United States dollar bill in the background as a reference point.. This is a table of selected pistol/submachine gun and rifle/machine gun cartridges by common name.
The Boeing MH-139A Grey Wolf is a twin-engine helicopter operated by the United States Air Force (USAF) for security and support missions. Developed by Boeing , the Grey Wolf is a variant of the Leonardo AW139 , an Italian-built multi-role helicopter.
The Land Rover Wolf is a light military vehicle manufactured by Land Rover in the United Kingdom (UK), based on the Land Rover Defender, introduced in 1994.The Ministry of Defence (MoD) designates the Wolf 90 (short wheelbase) as Truck Utility Light (TUL) HS, and the Wolf 110 (long wheelbase) as Truck Utility Medium (TUM) HS, where HS stands for 'High Specification'.
Data from Recreational Power Engineering General characteristics Type: Twin cylinder, two-stroke, in-line, aircraft engine Bore: 76 mm (3.0 in) Stroke: 69 mm (2.7 in) Displacement: 625 cc (38.1 cu in) Length: 377 mm (14.8 in) Width: 450 mm (17.7 in) Height: 383 mm (15.1 in) Dry weight: 73 lb (33.1 kg) with free air cooling, 79 lb (35.8 kg) with fan cooling, including recoil starter and exhaust ...
Data from Kitplanes, Cliche and Purdy General characteristics Crew: one Capacity: one passenger Length: 22 ft 6 in (6.86 m) Wingspan: 30 ft 0 in (9.14 m) Height: 6 ft 2 in (1.88 m) Wing area: 160 sq ft (15 m 2) Empty weight: 450 lb (204 kg) Gross weight: 1,000 lb (454 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 twin cylinder, two-stroke aircraft engine, 64 hp (48 kW ...
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.