- Schreder HP-11
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The Schreder HP-11 is a homebuilt
glider designed byRichard Schreder in 1962. Schreder campaigned the prototype in the 1963 World Soaring Championships in Argentina, achieving a third-place finish.After minor modifications, including adoption of retractable undercarriage and deletion of the prototype's flap-aileron interconnect, Schreder marketed the HP-11A version as a kit. Several dozen were completed and flown through the mid-1970s.
The HP-11 is constructed almost entirely of aluminum alloy, using plastics and fiberglass composites only for non-structural fairings. The wings are of conventional riveted construction. The wing spar is an I-beam assembled from 7075-T6 alloy sheet and angle extrusions.
Like other Schreder sailplanes, the HP-11 uses 90-degree flaps for glidepath control.
pecifications
aerospecs
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met or eng?= engcrew=One
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length ft=
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span m=15.85
span ft=52
span in=0
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height ft=
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wing area sqm=9.7
wing area sqft=104
swept area sqm=
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rot area sqm=
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volume m3=
volume ft3=
aspect ratio= 26
empty weight kg=204
empty weight lb=450
gross weight kg=318
gross weight lb=700
lift kg=
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eng2 lbf-ab=max speed kmh=240
max speed mph=150
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ceiling m=
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glide ratio= 37
climb rate ms=
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sink rate ms= 0.55
sink rate ftmin= 108armament1=
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lists=References
* [http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=160 sailplanedirectory.com]
External links
* [http://soaridaho.com/Schreder/HP-11/HP-11_Links.html HP-11 Reference Info Link]
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