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词条 Hutchinson HS-127
释义

  1. Design and development

  2. Operational history

  3. Specifications (HS-127 two seater)

  4. See also

  5. References

name=HS-127 image= caption=

}}{{Infobox Aircraft Type

type=Glider national origin=United States manufacturer= designer=Vernon Hutchinson first flight=1956 introduced=1956 retired= status= primary user= more users= produced= number built=One program cost= unit cost= developed from= variants with their own articles=
}}

The Hutchinson HS-127 is an American mid-wing glider that was designed and built by Vernon Hutchinson.[1][2]

Design and development

The HS-127 was designed and built by Hutchinson in 1956 as a single seat, V-tailed aircraft that incorporated spoilers mounted in the fuselage sides, above the wing roots. The aircraft was constructed from aluminium and employed a NACA 65 (3)-618 airfoil.[1]

In 1960 Hutchinson constructed a new fuselage for the aircraft with two seats in tandem and a conventional tail. The wings from the earlier single seat fuselage were used on the new fuselage. The designer incorporated split trailing edge dive brakes and claims this was the first use of balanced trailing edge dive brakes. Both versions of the aircraft bore the same Federal Aviation Administration aircraft registration, N62P.[1]

The aircraft's HS designation indicates Hutchinson Sailplane.[2]

Operational history

Hutchinson completed his Silver badge and Gold badge while flying the HS-127 and also flew a number of {{convert|200|mi|km|0|abbr=on}} flights in it. In May 2011 the aircraft was still registered to Hutchinson, 55 years after its completion.[1][2]

Specifications (HS-127 two seater)

{{Aircraft specs
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|crew=one
|capacity=one passenger
|length m=
|length ft=
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|span m=
|span ft=57
|span in=0
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|height m=
|height ft=
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|wing area sqm=
|wing area sqft=132
|wing area note=
|aspect ratio=24.6:1
|airfoil=NACA 65 (3)-618
|empty weight kg=
|empty weight lb=804
|empty weight note=
|gross weight kg=
|gross weight lb=1200
|gross weight note=
|more general=


|perfhide=
|max speed kmh=
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|max speed kts=
|max speed note=
|cruise speed kmh=
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|stall speed kmh=
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|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=33:1 at 67 mph (108 km/h)
|sink rate ms=
|sink rate ftmin=150
|sink rate note=at 58 mph (93 km/h)
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=9.1
|wing loading note=
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|avionics=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
  • List of gliders

}}

References

1. ^Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 44. Soaring Society of America November 1983. USPS 499-920
2. ^{{Cite web|url = http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=62P|title = Make / Model Inquiry Results|accessdate = 15 May 2011|last = Federal Aviation Administration|authorlink = |date=May 2011}}

2 : United States sailplanes 1950–1959|Homebuilt aircraft

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