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Original file (Ogg multiplexed audio/video file, Theora/Vorbis, length 1 min 2 s, 1,280 × 720 pixels, 4.51 Mbps overall, file size: 33.54 MB) This is a file from the Wikimedia Commons . Information from its description page there is shown below.
The operational requirements of the ISV were nine passengers, a payload of 3,200 pounds (1,500 kg), transportable by external sling load by a Sikorksy UH-60 Black Hawk helicopter, internal load/external lift by Boeing CH-47 Chinook helicopter, low-velocity air drop by Lockheed C-130 Hercules or Boeing C-17 Globemaster III transport aircraft and ...
The Sling 4 is an all-metal, low-wing, fixed tricycle gear kit aircraft, developed in 2011. The canopy was modified to include gull-wing doors. The aircraft has flaps with 40 degrees of travel. [2] [3] It has been estimated that building a Sling 4 requires 900-1,200 man-hours of work. The aircraft can be supplied as a kit, or built by the ...
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The M-1956 load-carrying equipment (LCE), also known as the individual load-carrying equipment (ILCE), was developed by the U.S. Army and first issued in the early 1960s. [1] The M-1956 LCE was designed to replace the M-1945 Combat Pack , the M-1923 cartridge belt, the M-1936 pistol belt and the M-1937 BAR magazine belt.
A Boeing CH-47 Chinook at Campbell Army Airfield on 7 August 2012 delivering two Humvees by sling load On 6 August 2011, a Chinook crashed near Kabul, killing all of the 38 aboard. The Chinook was reportedly shot down with a rocket-propelled grenade by the Taliban while attempting to assist a group of U.S. Navy SEALs.
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As stalling is due to wing loading and maximum lift coefficient at a given altitude and speed, this limits the turning radius due to maximum load factor. At Mach 0.85 and 0.7 lift coefficient, a wing loading of 50 lb/sq ft (240 kg/m 2 ) can reach a structural limit of 7.33 g up to 15,000 feet (4,600 m) and then decreases to 2.3 g at 40,000 feet ...