Ov10a Aircraft - The OV-10A is a short takeoff and landing twin turboprop aircraft designed by the United States Marine Corps and developed under the Tri-Service program of the United States Air Force, Navy, and Marine Corps. The first serial OV-10A was ordered in 1966, and the first flew in August 1967.
Bronco missions include surveillance, forward air control (FAC), helicopter escort, armed reconnaissance, gunnery reconnaissance, assistance and limited ground attack. However, the USAF acquired the Bronco primarily as a FAC aircraft. Adding to its versatility is an aft hull compartment with a capacity of 3,200 pounds of cargo, five combat-equipped hulls or two stretcher patients and a paramedic.
Ov10a Aircraft
The US Air Force's first operational OV-10As arrived in Vietnam in July 1968. A total of 157 OV-10As were delivered to the USAF before production ended in April 1969.
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The aircraft on display were delivered to the US Air Force in October 1968 and shipped directly to the 504
Tactical Air Support Team at Ben Ho Air Force Base, Vietnam. It remained in Southeast Asia until assigned to the 507 in June 1974
December 1988 at Shaw Air Force Base. He later became a ground instructor at Shepard Air Force Base, Texas, and was transferred to the museum in 2008. The North American Rockwell OV-10 Mustang is an American twin-turboprop light attack and surveillance aircraft. It was developed in the 1960s as a special aircraft for counterinsurgency (COIN) operations, and one of its main missions was as a forward air control (FAC) aircraft. It can carry up to 3,200 lb (1,450 kg) of external munitions and internal cargo, such as parachutes or stretchers, and can roam three or more.
The aircraft was originally introduced in the early 1960s through W.H. Beckett and Colonel K.P. Rice, US Marines, who met at China Lake Air Force Base in California, where they were also fortunate enough to live. The original concept was a robust, simple aircraft for close air support combined with ground combat. At the time, the US military was still experimenting with gunships and the US Air Force was not interested in close air support.
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The concept aircraft is operated from a fast-forward airbase that uses roads as runways. Velocities range from very slow to moderately subsonic, with much longer residence times than pure jets. An efficient turboprop engine will provide better performance than a piston engine. The weapon will be mounted on the tail for effective long range targeting. Inventors favored marksmanship weapons, such as the self-loading recoilless rifle, which fired aimed explosive shells with less recoil than a cannon and weighed less per shot than a rocket. The hull is designed to avoid blowing out the back.
Beckett and Rice developed a basic platform that met these requirements and attempted to build a fiberglass prototype in their garage. The effort produced a cult following and an informal pamphlet describing the concept. W.H. Beckett, retired from the Marine Corps, went to work for North American Airlines selling airplanes.
The military definition of STOL (obstacles 500 feet to 50 feet) permits takeoff and landing in most areas where limited warfare is likely. In addition, the aircraft is designed to use roads, so it can fly in jungle areas where clearance is low and distances are long. Wingspan was therefore limited to 20 feet, and heavy-duty trailing arm landing gear with 6.5 feet of tread was provided for road operation. Float work is feasible...[2] ...it is very feasible to design the various components so that they can be easily disassembled and stored along with the equipment needed for reassembly in the field in a suitable 6×6 in a truck bed box. Therefore, it can be transported by amphibious transport, but also lifted by a 6x6 truck-helicopter or pulled to shore. [3] Lightly armed reconnaissance aircraft[edit]
The US Navy, Air Force and Army approved a "tri-service" specification for a Lightly Armed Reconnaissance Aircraft (LARA), which was released in late 1963. The LARA request was based on a perceived need for a new "Jungle Combat" multi-role light attack and observation aircraft. Existing military aircraft used for observation missions, such as the Cessna O-1 Bird Dog and the Cessna O-2 Skymaster, are considered outdated, too slow and too small a payload for such flexible tasks.
Aircraft Photo Of N429df
The specification requires that the two-engine, two-person aircraft can carry at least 2,400 pounds (1,100 kilograms) of cargo, six parachutes or stretchers, and withstand +8 and -3 g thrusts (basic aerobatic capability). It must also be able to operate on an aircraft carrier, fly at a speed of at least 350 mph (560 km/h), take off at an altitude of 800 feet (240 m) and convert to an amphibious vehicle. It must carry various armaments, including four 7.62 mm (0.300 in) machine guns and 2,000 rounds of ammunition, as well as external armament, including a gun bay with a 20 mm (0.79 in) M197 electric gun and an AIM-9 Sidewinder air - missile air.
Submitted Elev proposals including: Grumman Model 134R two-seat version of the US Army's fielded OV-1 Mohawk (the US Marine Corps dropped the Mohawk program in 1958), Goodyear GA 39, Beechcraft PD-183, Douglas D-855, Convair Model Charger, Helio 1320, Lockheed CL-760, Martin Design and North American Airlines/Rockwell NA-300.
In August 1964, the NA-300 was selected. The contract for the SEV prototype was awarded in October 1964. Convair protested the decision and built a small wing prototype Model 48 Charger, which first flew on November 29, 1964. It is also a wide spread biplane similar to the OV-10. Although the Charger was able to outperform the OV-10 in some respects, it crashed on October 19, 1965 after 196 test flights. Conwell then withdrew from the race.
The Bronco began flying halfway through the Charger test program on July 16, 1965, and became one of the premier counter-insurgency (COIN) aircraft for the next 30 years. It did not implement Rice's L2 VMA concept because the DoD insisted on a 40-foot (12-meter) wingspan, making it dependent on air bases. Rice concluded:
North American Ov 10a Bronco Aircraft Report 9/9/2022g
The original concept of a small, simple craft that could operate near supported troops was almost completely eliminated by the "system". Road-running capability (20-foot span and 6.5 treads) was neglected, and performance was compromised by a short 30-foot span, an extra 1,000 lbs for rugged off-road landing gear, and another 1,000 lbs of electronics. The "light, simple" aircraft also have full instrumentation, ejection seats and substantial external storage stations. The concept of using ground ammunition and bomb bays was neglected, although it had provisions for four M60 [medium] machine guns. Despite this growth (almost double the size and weight of the houses we build), the YOV-10 still has a lot of potential. It will not achieve the benefits of integration with ground maneuvering schemes, but it has the ability to remain valuable and unique at low d speed performance. [4]
The Mustang performs surveillance, forward air control, helicopter escort, armed reconnaissance, practical light airlift and limited ground attack. The Bronco also performed aerial radiological reconnaissance, tactical aerial surveillance, artillery and naval fire reconnaissance, air control over tactical air support operations, and frontline low-altitude aerial photography. A prototype designed in Vietnam for smoking cigarettes was so successful that evaluators used it for several months, it was barely released for sale, but was not bought due to lack of purpose.
The OV-10 has a central nacelle that houses the pilot and cargo, and twin arms that contain twin turboprops. The visual characteristic of the aircraft is a combination of twin arms and a horizontal stabilizer connecting them.
The aircraft is designed to support efficient operations from forward bases. The OV-10 can perform short takeoffs and landings, including on aircraft carriers and large-deck amphibious assault ships
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No need for catapults or arresting wires. In addition, the OV-10 is designed to take off and land in unimproved locations. It can be repaired with common tools. No ground equipment is required to start the engine. If necessary, the engine can run on high-octane automatic fuel with only a small loss of power.
The cockpit provided excellent visibility for the tandem pilot and co-pilot, provided by a "greenhouse" envelope wider than the fuselage. North American Rockwell custom ejection seats are standard,
With the second seat removed, it can carry 3,200 pounds (1,500 kilograms) of cargo, five paratroopers or two small aircraft and an escort. Curb weight is 6,969 pounds (3,161 kilograms). Normal operating fuel weight for a crew of two is 9,908 lb (4,494 kg). Maximum take-off weight is 14,446 lb (6,553 kg).
The lower part of the fuselage is equipped with side wings, or "short wings", which improve flight performance by reducing air resistance under the fuselage. Horizontal windows were placed on the prototype. Testing led to these being redesigned for production aircraft; downward angles for ties in production
Ov 10a Bronco (air Force)
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