Vogt Lo-150
{{Short description|German single-seat glider}}
{{Infobox Aircraft Begin
| name=Lo-150 | image= | caption= }}{{Infobox Aircraft Type | type=Glider | national origin=West Germany | manufacturer= | designer=Alfred Vogt | first flight= | introduced= | retired= | status= | primary user= | more users= | produced= | 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}}
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=
|more general=
|perfhide=
|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=
|more performance=
|avionics=
}}
See also
Notes
{{reflist}}
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}}
{{refend}}
External links
- [https://web.archive.org/web/20050502234032/http://vintagesailplanes.de/Lo150.htm Lo-150 photos] on Archive.org
{{Alfred Vogt aircraft}}