IS-4 Jastrząb

{{Infobox Aircraft Begin

| name=IS-4 Jastrząb

| image=Kraków, Muzeum Lotnictwa Polskiego IS-4.jpg

| caption=

}}{{Infobox Aircraft Type

| type= Glider

| national origin=Poland

| manufacturer= Instytut Szybownictwa

| designer= J Niespał

| first flight= 21 Dec 1949{{cite web| last=Piechowski|first=Piotr|title=IS-4 Jastrząb| url=http://www.piotrp.de/SZYBOWCE/pis4.htm|publisher=Piotr & Renate Piechowski| access-date=19 April 2013}}

| introduced=1950

| retired=

| status=

| primary user=

| number built= 37

| developed from=

| variants with their own articles=

}}

The IS-4 Jastrząb (Instytut Szybownictwa – gliding institute) was a single-seat aerobatic glider designed and built in Poland from 1949.

Development

The IS-4 was built for aerobatics with a high structural strength and a very high maximum speed which could not be achieved in a vertical dive. Due to the pilot's sitting position and the arrangements of the controls, it was difficult for pilots to exceed the 8g loading limit. During high speed flight it was possible for the air-brakes to be sucked out violently, so most pilots ensured that they remained closed by holding the airbrake control.

Variants

  • IS-4 Jastrząb – two prototypes built in 1949.
  • IS-4 Jastrząb bis – Thirty-five production aircraft, three of which were exported.

Specifications (IS-4 Jastrząb bis)

{{Aircraft specs

|ref=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II{{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II|year=1963|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=172–173|edition=1st|author2=K.G. Wilkinson|language=en, fr, de}}

|prime units?=met

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|length m=6.25

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|span m=12

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|height m=1.3

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|height note=at cockpit

|wing area sqm=12

|wing area sqft=

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|aspect ratio=12

|airfoil=RootNACA 2418, TipNACA 2412, MidNACA 0012

|empty weight kg=240

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|gross weight kg=357

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|stall speed kmh=67

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|never exceed speed kmh=450

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

  • Rough air speed max: {{convert|200|km/h|mph kn|abbr=on}}
  • Aerotow speed: {{convert|200|km/h|mph kn|abbr=on}}
  • Winch launch speed: {{convert|150|km/h|mph kn|abbr=on}}

|minimum control speed kmh=

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|minimum control speed kts=

|minimum control speed note=

|range km=

|range miles=

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|range note=

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|ferry range km=

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|endurance=

|ceiling m=

|ceiling ft=

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|g limits=+7 -4 at {{convert|200|km/h|mph kn|abbr=on}}

|roll rate=

|glide ratio= 20.2 at {{convert|87|km/h|mph kn|abbr=on}}

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=1.04

|sink rate ftmin=

|sink rate note= at {{convert|70|km/h|mph kn|abbr=on}}

|lift to drag=

|wing loading kg/m2=29.7

|wing loading lb/sqft=

|wing loading note=

|disk loading kg/m2=

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|fuel consumption kg/km=

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See also

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References

{{reflist}}

{{refbegin}}

  • {{cite web| last=Piechowski|first=Piotr|title=IS-4 Jastrząb| url=http://www.piotrp.de/SZYBOWCE/pis4.htm|publisher=Piotr & Renate Piechowski| access-date=19 April 2013}}
  • {{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II|year=1963|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=172–173|edition=1st|author2=K.G. Wilkinson|language=en, fr, de}}

{{refend}}

Further reading

  • Taylor, J. H. (ed) (1989) Jane's Encyclopedia of Aviation. Studio Editions: London. p. 29