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词条 Peterson J-4 Javelin
释义

  1. Design and development

  2. Operational history

  3. Specifications (variant specified)

  4. See also

  5. References

  6. External links

name=J-4 Javelin image= caption=

}}{{Infobox Aircraft Type

type=Glider national origin=United States manufacturer=Peterson Sailplane Corporation designer=Max A. Peterson first flight=1969 introduced=1973 retired= status=No longer in production primary user= more users= produced= number built=8 program cost= unit cost= developed from= variants with their own articles=
}}

The Peterson J-4 Javelin is an American, single seat, mid-wing glider that was designed by Max A. Peterson in the late 1960s and produced by the Peterson Sailplane Corporation in small numbers. The glider was type certified and put into production in 1973.[1][2][3]

Design and development

Peterson designed the J-4 based on lessons he learned with his earlier Peterson Medena design. The J-4 is a single seater, but can carry a child in the small seating area behind the pilot.[1][2]

The J-4's fuselage is made from steel tube with the lower part covered in a fiberglass shell and the upper part sheet aluminium. The wing is built around a chem-milled tubular spar and is assembled predominantly with pop rivets. The wing has no ailerons and instead roll control is via upper surface spoilerons that eliminate virtually all adverse yaw. Spoilers are also provided for glide-path control. The landing gear is a monowheel.[1][2]

First flown in 1969, the J-4 was Federal Aviation Administration type certified on 6 February 1973. A pilot production run of eight examples was completed, but production was not continued. Poly Industries of Ontario, California produced aircraft under licensing agreement from Peterson Sailplane Corporation, who held the type certificate.[1][2][3]

Operational history

In 1983, six of the original eight built were reportedly still flying and there were still six registered in April 2011.[2][4]

Specifications (variant specified)

{{Aircraft specs
|ref=Sailplane Directory, Soaring and FAA type certificate [1][2][3]
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|wing area sqft=126
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|aspect ratio=20.1:1
|airfoil=NACA 64(3)-618
|empty weight kg=
|empty weight lb=512
|empty weight note=
|gross weight kg=
|gross weight lb=804
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|never exceed speed kmh=
|never exceed speed mph=120
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|roll rate=
|glide ratio=30:1 at 65 mph (105 km/h)
|sink rate ms=
|sink rate ftmin=126
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=5.8
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See also

{{aircontent
|see also=
  • List of gliders

|related=
|similar aircraft=
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References

1. ^{{Cite web|url = http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=174|title = Javelin J-4 Peterson|accessdate = 5 April 2011|last = Activate Media|authorlink = |year = 2006|deadurl = yes|archiveurl = https://web.archive.org/web/20020502113354/http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=174|archivedate = 2 May 2002|df = }}
2. ^Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 17. Soaring Society of America, November 1983. USPS 499-920
3. ^{{Cite web|url = http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/8b7261470f10836185256721004e3f30/$FILE/G3we.PDF|title = TYPE CERTIFICATE DATA SHEET NO. G3WE |accessdate = 5 April 2011|last = Federal Aviation Administration|authorlink = |date=May 1976}}
4. ^{{Cite web|url = http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=PETERSON&Modeltxt=J-4&PageNo=1|title = Make / Model Inquiry Results|accessdate = 5 April 2011|last = Federal Aviation Administration|authorlink = |date=April 2011}}

External links

  • Photos and article about the J-4
  • Photo of J-4
  • Photo of J-4
{{Max A. Peterson aircraft}}

1 : United States sailplanes 1960–1969

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