By A. K. Kundu, S. Raghunathan
Plane layout three (2000) 261 - 273
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Extra resources for A proposition in design education with a potential in commercial venture in small aircraft manufacture
Two complete Defiant wings were used which were staggered to give a better view for the pilot while the guns were housed, along with the main wheels, in large spats. The options were four 20mm, three 40mm, two 20mm and two 40mm or two 20mm plus bombs or RPs; there was no provision for the 47mm but the required two 500lb (227kg) bombs were carried under the wing centre section and eight RPs were loaded under the outer wings. Maximum rate of climb (up to 3,OOOft [9l4mJ) was 2,200fVmin (671m/min) and range with normal load 750 miles (1,207km).
These could be bolted onto the wing, had no recoil (which meant that they could be carried on anything) and on types like the Tempest they ensured that, once fired, the aircraft could revert to its fighter role. Today the concept of the ground attack aircraft is well established. 43). 5. SM 323 (520) or 316 (508) al 16,000 (4,876) 265 (426) at 10,750 (3,277) ? 5M 291 (468) at 3,000 (914) 355 (571) at 3,000 (914) 315 (507) at 17,000 (5,182) 335 (539) at 17,000 (5,182) 317(510)at 18,000 (5,486) 315 (507) at 3,000 (914) ?
7mm) Browning machine guns outboard of the specified cannon, stacked one above the other two per side, while a 250lb (113kg) bomb container could be carried as an alternative load. 92's wing had split naps and Frise ailerons and the engine radiators were placed on the front of the nacelles. A total of 270gal (I,2281it) of fuel was carried in four tanks. Estimated rate of climb was 3,080fVmin (939m/min) at sea level and 3,220fVmin (981m/min) at 15,OOOft (4,572m); Turret Fighters ... ~ ',. 37). Les Whitehouse ~ --'~l'L I service ceiling 38,OOOft (II ,582m).
A proposition in design education with a potential in commercial venture in small aircraft manufacture by A. K. Kundu, S. Raghunathan