Jump to content

ITS-8

From Wikipedia, the free encyclopedia
This is an old revision of this page, as edited by TSRL (talk | contribs) at 20:27, 24 May 2018 (Created page with '<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {|{{Inf...'). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)
Role Motor-glider
National origin Poland

Variants

ITS-8
ITS-8W
ITS-8R


Specifications (ITS-)

Data from J. Cynk (1971)[1]

General characteristics

  • Crew: One
  • Length: 6.4 m (21 ft 0 in)
  • Wingspan: 13.6 m (44 ft 7 in)
  • Wing area: 16.9 m2 (182 sq ft)
  • Empty weight: 180 kg (397 lb)
  • Gross weight: 290 kg (639 lb)
  • Powerplant: 1 × Koeber Kötter M3 flat twin engine, 13 kW (18 hp)
  • Propellers: 2-bladed Zomanski, 1.36 m (4 ft 6 in) diameter wooden

Performance

  • Maximum speed: 120 km/h (75 mph, 65 kn) at sea level
  • Cruise speed: 110 km/h (68 mph, 59 kn)
  • Service ceiling: 1,500 m (4,900 ft)
  • Rate of climb: 1.3 m/s (260 ft/min)
  • Rate of sink: 0.91 m/s (179 ft/min) engine off
  • Landing speed: 45 km/h (28 mph; 24 kn)

References

  1. ^ Cite error: The named reference Cynk was invoked but never defined (see the help page).



[[Category:]]