Vogt Lo-150

{{Short description|German single-seat glider}}

{{Infobox Aircraft Begin

| name=Lo-150

| image=

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}}{{Infobox Aircraft Type

| type=Glider

| national origin=West Germany

| manufacturer=

| designer=Alfred Vogt

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| number built=15

| developed from= Vogt Lo-100

| variants with their own articles=

}}

The Vogt Lo-150 is a West German high-wing, single seat glider that was designed by Alfred Vogt and produced by the Wolf Hirth Company.{{Cite web|url = http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=202|title = LO-150 Wolf Hirth|access-date = 16 July 2011|last = Activate Media|year = 2006|url-status = dead|archive-url = https://web.archive.org/web/20120819220012/http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=202|archive-date = 19 August 2012}}Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 91, Soaring Society of America November 1983. USPS 499-920

Design and development

The Lo-150 was developed from the {{convert|10|m|ft|1|abbr=on}} wing span aerobatic Vogt Lo-100 as a performance cross country sailplane.

The Lo-150 is constructed from wood, including its wooden monocoque fuselage. Its {{convert|15|m|ft|1|abbr=on}} span two-piece wing employs a Clark Y airfoil and incorporates flaps for glidepath control. Early examples use a take-off dolly and land on a fixed skid, while later ones use a fixed monowheel landing gear.{{Cite web|url = http://www.ae.illinois.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage |access-date = 1 July 2011|last = Lednicer |first = David |year = 2010}}

Fifteen Lo-150s were produced.

Operational history

Several Lo-150s were imported into the United States. A.J. Smith won the US Nationals flying an Lo-150 in 1961. Harold Jensen flew an Lo-150 {{convert|700|km|mi|0|abbr=on}} in 1962, winning the Barringer Trophy.

Specifications (Lo-150)

{{Aircraft specs

|ref=Sailplane Directory and Soaring 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 du Monde|year=1958|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=68–72|edition=1st|author2=K.G. Wilkinson |language=en, fr, de}}

|prime units?=met

|genhide=

|crew=one

|capacity=

|length m=6.15

|length ft=

|length in=

|length note=

|span m=15.0

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=10.9

|wing area sqft=

|wing area note=

|aspect ratio=20.6:1

|airfoil=Clark Y

|empty weight kg=200

|empty weight lb=

|empty weight note=equipped

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=310

|max takeoff weight lb=

|max takeoff weight note=

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|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=200

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

  • Rough air speed max: {{convert|150|km/h|mph kn|abbr=on}}
  • Aerotow speed: {{convert|150|km/h|mph kn|abbr=on}}
  • Winch launch max speed: {{convert|100|km/h|mph kn|abbr=on}}

|g limits=

|roll rate=

|glide ratio=34 at {{convert|105|km/h|mph kn|abbr=on}}

|sink rate ms=0.68

|sink rate ftmin=

|sink rate note= at {{convert|86|km/h|mph kn|abbr=on}}

|lift to drag=

|wing loading kg/m2=28.4

|wing loading lb/sqft=

|wing loading note=

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See also

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Notes

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References

{{refbegin}}

  • {{cite book|last=Shenstone|first=B.S.|title=The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde|year=1958|publisher=Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue|location=Zurich|pages=68–72|edition=1st|author2=K.G. Wilkinson |language=en, fr, de}}

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