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词条 Schreder HP-17
释义

  1. Design and development

  2. Operational history

  3. Specifications (HP-17)

  4. See also

  5. References

name=HP-17 image=Schreder HP-17.jpg caption=The HP-17

}}{{Infobox Aircraft Type

type=Glider national origin=United States manufacturer= designer=Richard Schreder first flight= introduced= retired= status=Sole example no longer on the US registry primary user=Richard Schreder more users= produced= number built=one program cost= unit cost= developed from= variants with their own articles=
}}

The Schreder HP-17 was an American mid-wing, V tailed, single seat, experimental glider designed by Richard Schreder to test a new airfoil section.[1]

Design and development

The HP-17 was designed to test a new airfoil section, the Wortmann FX 72 MS-150A. This airfoil is a high-lift, low drag section that Scheder thought would be a good sailplane design.[1]

The HP-17 is all-metal in construction, except for its foam wing ribs. The wing features water ballast carried inside the wing spar. The wing also has full-span flaps and spoilerons in place of ailerons.[1]

Operational history

The HP-17 was given its baptism of fire in the 1973 US Nationals when Schreder flew it in the FAI 15 Metre Class. The aircraft placed 38th and thus was not deemed a success. After the competition it was not used again and Schreder tuned his attention to the much more successful HP-18 instead.[1]

The HP-17 was retained by Schreder for many years, but in April 2011 it was no longer registered, not in the National Soaring Museum and its current whereabouts are unknown.[1][2][3]

Specifications (HP-17)

{{Aircraft specs
|ref=Soaring[1]
|prime units?=imp


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=15
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=113
|wing area note=
|aspect ratio=21.4
|airfoil=Wortmann FX 72 MS-150A
|empty weight kg=
|empty weight lb=500
|empty weight note=including 200 lbs (90 kg) of water ballast
|gross weight kg=
|gross weight lb=940
|gross weight note=
|more general=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
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|cruise speed kmh=
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|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|g limits=
|roll rate=
|glide ratio=40:1
|sink rate ms=
|sink rate ftmin=102
|sink rate note=at {{convert|40|mph|0|abbr=on}}
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=8.3
|wing loading note=with full water ballast
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
  • List of gliders

|related=
|similar aircraft=
|lists=
}}

References

1. ^Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 23. Soaring Society of America, November 1983. USPS 499-920
2. ^{{Cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=HP-17&PageNo=1|title = Make / Model Inquiry Results|accessdate = 16 April 2011|last = Federal Aviation Administration|authorlink = |date=April 2011}}
3. ^{{cite web|url = http://www.soaringmuseum.org/collection.html|title = Sailplanes in Our Collection|accessdate = 26 February 2011|last = National Soaring Museum|authorlink = |year = 2011|deadurl = yes|archiveurl = https://web.archive.org/web/20110516142717/http://www.soaringmuseum.org/collection.html|archivedate = 16 May 2011|df = }}
{{Schreder Sailplanes}}

2 : United States sailplanes 1970–1979|Schreder aircraft

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