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The aircraft features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, an inflatable boat hull and a single engine in pusher configuration. The FIB has no wheeled landing gear, but as a result of customer demand it was later developed into the amphibious Polaris AM-FIB. [1]
The aircraft has a maximum gross weight of 406 kg (895 lb). It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, retractable tricycle landing gear mounted to its inflatable boat hull and a single engine in pusher configuration. [1] [2]
The Mitchell Wing B-10 is an American high-wing, open cockpit, single-seat, tailless, ultralight aircraft and motor glider designed by Don Mitchell and based on his Mitchell Wing hang-glider. It has been produced by a variety of companies in the form of kits and plans for amateur construction. [1] [2] It first flew in 1980. [3]
Surprisingly, what really launched the powered ultralight aviation movement in the United States was not the Rogallo flexible wing but a whole series of rigid-wing motorized hang gliders. [3] The Icarus V flying wing appeared with its tip rudders and swept-back style wing was used as a base for some powered experiments.
The SunFun started as a foot-launched glider design, the VJ-24, and was developed into a wheeled undercarriage motor glider, the VJ-24W. The VJ-24 was derived from the earlier Volmer VJ-23 Swingwing and differed from that design by replacing the wooden structure with metal and employing a constant chord, strut-braced wing in place of the VJ-23's cantilever, tapered wing.
The A-10 is a 1982 development of the Mitchell Wing B-10 ultralight, itself developed from the Mitchell Wing hang glider of 1977. Their designer Don Mitchell had worked on the Northrop YB-49 bomber project. In place of the B-10's composite wing, the A-10 features a metal wing, attached in cantilever fashion to an open cockpit that can be ...
An engine was installed by John Moody in 1975 so the glider could be launched from flat terrain. [1] [5] Early powered versions consisted simply of a motor added to the foot-launched hang glider version with control by a combination of weight shift for pitch and tip rudders for roll and yaw, with the tip rudders used together as air brakes.
The Monarch first flew in 1974 and was designed to be both a powered self-launching sailplane and also a pure glider, depending on whether an engine was fitted. The glider version is suitable for car-tow or winch-launching. [1] [2] The aircraft is built from fiberglass and epoxy laminates. The wing uses a D-cell leading edge.
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