Schleicher K7

{{Short description|German two-seat glider, 1960}}

{{Infobox Aircraft Begin

| name=K7 Rhönadler

| image=File:Navijak-k7.jpg

| caption=

}}{{Infobox Aircraft Type

| type=Glider

| national origin=West Germany

| manufacturer=Alexander Schleicher GmbH & Co

| designer=Rudolf Kaiser

| first flight=

| introduced=1960

| retired=

| status=Production completed

| primary user=

| more users=

| produced=

| number built=550

| developed from= Schleicher Ka-2

| variants with their own articles= Schleicher ASK 13

}}

The Schleicher K7 Rhönadler is a West German high-wing, two-seat, glider that was designed by Rudolf Kaiser and produced by Alexander Schleicher GmbH & Co.{{Cite web|url = http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=182|title = Ka-7 Schleicher|accessdate = 23 July 2011|last = Activate Media|year = 2006|url-status = dead|archiveurl = https://web.archive.org/web/20111117093614/http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=182|archivedate = 17 November 2011}}{{cite journal|last=Said|first=Bob|title=1983 Sailplane Directory|journal=Soaring Magazine|date=November 1983|id=USPS 499-920|publisher=Soaring Society of America}}

Often referred to as the Ka-7 or K-7, the US Federal Aviation Administration type certificate officially designates it as the K7.{{Cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/53f76bd8653231df8625748e0055efc5/$FILE/7g3.PDF |title = Type Certificate Data Sheet No. 7g3 |accessdate = 23 July 2011|last = Federal Aviation Administration|authorlink = |date=February 1961}}

Design and development

The K7 was intended as a two-place trainer with good performance, a rare combination in trainers of its time.

The K7 is constructed with a welded steel tube fuselage, covered in doped aircraft fabric covering. The wing is a wooden structure with a doped fabric covering and employs a Goettingen 533 (16%) airfoil at the wing root, transitioning to a Goettingen 533 (14%) section at the wing tip. The wing features powerful dive brakes. The landing gear is a fixed monowheel. The earlier Ka-2 variant has a plywood monocoque fuselage.{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 23 July 2011|last = Lednicer |first = David |authorlink = |year = 2010}}

After 550 had been built, the K7 was superseded in production by the Schleicher ASK 13.

The K7 can be converted into a K7/13 with a conversion kit to lower the wing to the mid-wing position and installation of a one-piece canopy, rendering the aircraft similar to the ASK-13.

Operational history

A K7 was flown to a new world multi-place glider speed record for flight around a {{convert|500|km|mi|0|abbr=on}} triangle of {{convert|84|km/h|mph|0|abbr=on}} in 1964 in South Africa.

File:AAFC cadets with a glider.jpg being taught how to operate the Ka-7 in 2010.]]

A K7 was assigned to 2 Wing AAFC and used to train Australian Air Force Cadets 228 Squadron at Bundaberg from 2007 to 2014.{{Cite web|url=http://www.aafc.org.au/what-we-do/gliding/|title=Gliding|last=|first=|date=1 January 2018|website=|archive-url=|archive-date=|access-date=20 April 2020}}

Variants

;Ka-2

:Early version with a plywood monocoque fuselage

;K7

:Main production version with a steel tube fuselage.

;K7/13

:K7 converted to a mid-wing arrangement, plus a single piece canopy, to resemble an AS-K 13

Specifications (K7)

File:600 BWSFG 20020928 108.jpg

File:Schleicher K7 C-GALN wing recovering.jpg

{{Aircraft specs

|ref=Sailplane Directory, Soaring and FAA Type Certificate 7g3, and The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde{{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde|year=1958|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=9–13|edition=1st |author2=K.G. Wilkinson |author3=Peter Brooks|language=English, French, German}}

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=8.15

|span m=16.0

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=17.56

|aspect ratio=14.6:1

|airfoil=root: Goettingen 533 (16%), mid: Goettingen 533 (14%), tip: Goettingen 533 (14%)

|empty weight kg=282

|max takeoff weight kg=484.5

|more general=

|stall speed kmh=59

|never exceed speed kmh=200

|never exceed speed note=

  • Rough air speed max: {{convert|130|km/h|mph kn|abbr=on}}
  • Aerotow speed: {{convert|130|km/h|mph kn|abbr=on}}
  • Winch launch speed: {{convert|100|km/h|mph kn|abbr=on}}

|g limits=+4 -2

|glide ratio=26:1 at {{convert|83|km/h|mph|abbr=on}}

|sink rate ms=0.70

|sink rate note= at {{convert|67|km/h|mph|abbr=on}}

|wing loading kg/m2=27.34

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

Notes

{{reflist}}

References

{{refbegin}}

  • {{Cite web|url = http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=182|title = Ka-7 Schleicher|accessdate = 23 July 2011|last = Activate Media|year = 2006|url-status = dead|archiveurl = https://web.archive.org/web/20111117093614/http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=182|archivedate = 17 November 2011}}
  • {{cite journal|last=Said|first=Bob|title=1983 Sailplane Directory|journal=Soaring Magazine|date=November 1983|id=USPS 499-920|publisher=Soaring Society of America}}
  • {{Cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/53f76bd8653231df8625748e0055efc5/$FILE/7g3.PDF |title = Type Certificate Data Sheet No. 7g3 |accessdate = 23 July 2011|last = Federal Aviation Administration|authorlink = |date=February 1961}}
  • {{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |accessdate = 23 July 2011|last = Lednicer |first = David |authorlink = |year = 2010}}
  • {{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde|year=1958|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=81–87|edition=1st |author2=K.G. Wilkinson |author3=Peter Brooks|language=English, French, German}}

{{refend}}