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ITS-IVB

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This is an old revision of this page, as edited by TSRL (talk | contribs) at 21:48, 19 October 2018 (Design and development). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
ITS-IV
Role High performance research glider
National origin Poland
Manufacturer ZASPL
Designer Adam Nowotny, Franciszek Kotowski
First flight 30 July 1935
Number built 1

The ITS-IV was a

Design and development

The ITS IV was a high performance, two seat research sailplane was designed, initially by Adam Nowotny, to gather meteorological and airframe stress data. It was also intended to provide blind flying training. after Nowotny's death th e

[1]

[2]

Operational history

Specifications (ITS-IVB)

Data from J. Cynk (1971)[1] except where noted

General characteristics

  • Crew: Two
  • Length: 8.42 m (27 ft 7 in)
  • Wingspan: 20 m (65 ft 7 in)
  • Height: 2.2 m (7 ft 3 in) [2]
  • Wing area: 24.3 m2 (262 sq ft)
  • Aspect ratio: 15.8
  • Airfoil: Göttingen Gö 655
  • Empty weight: 254 kg (560 lb)
  • Gross weight: 431 kg (950 lb)

Performance

  • Maximum glide ratio: 22.5 at 73 km/h (45 mph; 39 kn) best
  • Rate of sink: 0.82 m/s (161 ft/min) at 63 km/h (39 mph; 34 kn) minimum[2]

References

  1. ^ a b Cynk, Jerzy (1971). Polish Aircraft 1893-1939. London: Putnam Publishing. p. 700-2. ISBN 0 370 00085 4.
  2. ^ a b c "ITS-IVb (ITS-IVb, 1935". Retrieved 16 October 2018.