Rahul Sharma (Editor)

Hindustan Ardhra

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
210 km/h

Length
  
8.61 m

Wingspan
  
16 m

First flight
  
March 5, 1979

Manufacturer
  
Hindustan Aeronautics Limited

The Hindustan Ardhra 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.

Contents

Operators

 India

  • Indian Air Force

    • Specifications

    Data from Jane's All the World's Aircraft 1988-89

    General 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; 113 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

    Hindustan Ardhra Wikipedia
    (Text) CC BY-SA