Top Document: rec.aviation.military Frequently Asked Questions (part 1 of 5) Previous Document: B.6. JAST Next Document: B.8. Lockheed/Boeing F-22 See reader questions & answers on this topic! - Help others by sharing your knowledge The LCA (Light Combat Aircraft) is India's second indigenous jet fighter design, after the HF-24 Marut of the 1950s. Development began in 1983; the basic design was finalised in 1990, and two prototypes are currently approaching completion, with first flight expected sometime in 1995. The configuration is a delta wing, with no tailplanes or foreplanes, and a single vertical fin. The LCA will be constructed of aluminium-lithium alloys, carbon-fibre composites, and titanium. The design incorporates "control-configured vehicle" concepts to enhance manoeuvrability, and quadruplex fly-by-wire controls. Both prototypes are powered by General Electric F404-GE-F2J3 engines, but an indigenous engine, the GTX-35VS Kaveri, is being developed for the production LCA. No official name or other designation has been assigned to the LCA yet. Vital statistics: length 13.20 m, span 8.20 m, empty weight 5500 kg, clean TO weight 8500 kg, max TO weight not given, max speed 1699 km/h (Mach 1.6); power plant: one 83.4 kN GTRE GTX-35VS augmented turbofan; armament: one GSh-23 twin-barrel 23mm cannon (220 rounds); 7 hardpoints; max external load over 4000 kg. User Contributions:Top Document: rec.aviation.military Frequently Asked Questions (part 1 of 5) Previous Document: B.6. JAST Next Document: B.8. Lockheed/Boeing F-22 Part1 - Part2 - Part3 - Part4 - Part5 - Single Page [ Usenet FAQs | Web FAQs | Documents | RFC Index ] Send corrections/additions to the FAQ Maintainer: avfaq@meanmach.actrix.gen.nz
Last Update March 27 2014 @ 02:11 PM
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