The Hindustan Ardhra (lit. 'The Moist One') was a sailplane designed in India for pilot training by the government's Civil Aviation Department in the late 1970s as the ATS-1 Ardhra. It was a two-seat aircraft of conventional configuration and wooden construction. The Indian Air Force ordered fifty examples in the early 1980s to be produced by Hindustan Aeronautics and the type was approved for use for flying by cadets.
Operators India
Indian Air Force
Specifications Data from Jane's All the World's Aircraft 1988-89General characteristics Crew: 2 Length: 8.61 m (28 ft 3 in) Wingspan: 16.5 m (54 ft 2 in) Height: 2.464 m (8 ft 1 in) Wing area: 21.83 m2 (235.0 sq ft) Aspect ratio: 12.5 Airfoil: Wortmann FX-61-184 Empty weight: 328 kg (723 lb) Max takeoff weight: 508 kg (1,120 lb) Performance
Stall speed: 61 km/h (38 mph, 33 kn) Never exceed speed: 210 km/h (130 mph, 110 kn) g limits: +5.3 -2.65 Maximum glide ratio: 26 Rate of sink: 0.78 m/s (154 ft/min) Wing loading: 17.32 kg/m2 (3.55 lb/sq ft)
References
Further reading Taylor, Michael J.H. (1989). Jane's Encyclopaedia of Aviation. London: Studio Editions. p. 255. ISBN 978-0-517-69186-1. Taylor, John W.R.; Munson, Kenneth, eds. (1985). Jane's all the world's aircraft, 1985-86 (76 ed.). London: Jane's Pub. p. 746. ISBN 9780710608215.
