History and description of shoulder wing aircraft which is constructed principally from light alloy, although small amount of titanium is used for some components; basic airframe is common to all versions, with two-seat version's nose section being 35.4 in. longer than tactical version; various systems are described, in particular, autostabilizer and fuel gaging systems, developed by Smiths Industries; head-up display, developed by Spectro Avionics Ltd; tailplane power control by Fairey Hydraulics Ltd; brake parachute installation and its characteristics; tires, wheels and brakes, developed by Dunlop Ltd; ancillary equipment, supplied by various British companies, is also listed. (44206)
Anglo-French Jaguar strike/trainer aircraft
Aircr Eng
Aircraft Engineering ; 40 , n 8
1968
22 pages
Article (Journal)
English
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Anglo-French Jaguar Strike/Trainer Aircraft
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