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A hardpoint is an attachment location on a structural frame designed to transfer force and carry an external or internal load.The term is usually used to refer to the mounting points (more formally known as a weapon station or station) on the airframe of military aircraft that carry weapons (e.g. gun pods and rocket pods), ordnances (bombs and missiles) and support equipments (e.g. flares and ...
Common hard point locations are on the wings, be it wing tip, inner, middle, or outer wing hard points, or on the side or center of the fuselage. The type of aircraft then further drives the possible options in terms of stores loading. The combination of loads and stores for each mission is usually called the external stores configuration.
Underwing hard-points can be fitted with multiple ejector racks, allowing each hard-point to carry two 500 lb (230 kg) unguided bombs or LGBs—Mk.82 or GBU-12. [27] [self-published source] Active radar homing BVR AAMs can be integrated with the radar and data-link for mid-course updates. The aircraft can carry the PL-12/SD-10 along with the PL ...
Its armament would consist of four 13.2 mm akan m/39 auto cannons in the nose and an 8 mm ksp m/22-37R machine gun for the gunner. It would be equipped with a bomb bay that could hold eight 50 kg bombs or a single 250 kg bomb with a bomb fork along with hard points under the wings for four more 50 kg bombs (two under each wing).
In the late 1970s, Sweden sought to replace its aging Saab 35 Draken and Saab 37 Viggen. [7] The Swedish Air Force required an affordable Mach 2 aircraft with good short-field performance for a defensive dispersed basing plan in the event of invasion; the plan included 800 m long by 17 m wide rudimentary runways that were part of the Bas 90 system.
An offensive armament subsystem developed for the ACH-47 helicopter, the XM34 provides two M24A1 20mm cannons with ammunition boxes on sponsons at the front of the aircraft fixed forward. [7] These sponsons were also fitted with aircraft-style hardpoints that allowed the mounting of XM159B/XM159C 19-tube 2.75"-rocket launchers or M18/M18A1 7.62 ...
Armament. All armament is optional. The Bulldog was designed so that it could be fitted with four hard points. These armaments were tested on company demonstrator aircraft G-ASAL. They were never used in RAF service although some weapons training was done on the Bulldog trainers in Sweden.
Work on the Yak-104 was terminated in favour of an aircraft with a single lift/cruise engine with rotating nozzles, similar to the Hawker Siddeley P.1127, which was nearing completion in England. Unable to find a suitable engine or convince the government to order the development of one, the Yakovlev bureau was forced to follow a different course.