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词条 Schreder HP-20
释义

  1. Design and development

  2. Operational history

  3. Specifications (HP-20)

  4. See also

  5. References

name=HP-20 image= caption=

}}{{Infobox Aircraft Type

type=Glider national origin=United States manufacturer= designer=Richard Schreder first flight=1981 introduced=1981 retired= status= primary user= more users= produced= number built=one program cost= unit cost= developed from= variants with their own articles=
}}

The Schreder HP-20 is an American, high-wing, T-tail, single seat glider designed by Richard Schreder.[1]

Design and development

The HP-20 was designed by Schreder for the FAI 15 Metre Class. The HP-20 prototype was just complete when Schreder lost interest in the project and moved on to work on the HP-21 instead. The sole example of the HP-20 was built by Schreder in his workshop in Byran, Ohio and first flew in 1981.[1][2]

The HP-20 is all-metal with foam wing ribs. The design shares a similar fuselage to the HP-19, but has a different double-tapered wing of smaller area, {{convert|102|sqft|m2|abbr=on}} versus {{convert|113|sqft|m2|abbr=on}} for the HP-19. This gives the HP-20 a higher wing loading and higher best glide speed, although the glide ratio is the same as the HP-19 at 42:1. The airfoil is a Schreder modification of a Wortmann section, designated as Schreder 3. {{convert|200|lb|kg|0|abbr=on}} of water ballast can be carried. The landing gear is a retractable monowheel.[1]

Operational history

Even though Richard Schreder died in August 2002, in April 2011 the sole HP-20 was still registered to him.[2]

Specifications (HP-20)

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


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
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|length note=
|span m=15
|span ft=
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=102
|wing area note=
|aspect ratio=24.5
|airfoil=Schreder 3, a modification of a Wortmann section
|empty weight kg=
|empty weight lb=470
|empty weight note=
|gross weight kg=
|gross weight lb=970
|gross weight note=includes 200 lbs (91 kg) or water ballast
|more general=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
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|stall speed kmh=
|stall speed mph=
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|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=42:1 at 60 mph (98 km/h)
|sink rate ms=
|sink rate ftmin=120
|sink rate note=at 50 mph (80 km/h)
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=9.5
|wing loading note=
|more performance=
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}}

See also

{{aircontent
|see also=
  • List of gliders

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

References

1. ^Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 24. Soaring Society of America, November 1983. USPS 499-920
2. ^{{Cite web|url =http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=4240F|title = Make / Model Inquiry Results|accessdate = 19 April 2011|last = Federal Aviation Administration|authorlink = |date=April 2011}}
{{Schreder Sailplanes}}

2 : United States sailplanes 1980–1989|Schreder aircraft

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