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Jongblood Primary

From Wikipedia, the free encyclopedia
American homebuilt glider

Jongblood Primary
RoleGlider
Type of aircraft
National originUnited States
DesignerMike Jongblood
First flight1967
Introduction1967
StatusSole example reported as "in storage" in 1983
Number builtOne

TheJongblood Primary is an American single-seat,high-wing,strut-bracedprimary glider designed byMike Jongblood of southernCalifornia and first flown in 1967. The aircraft is unusual in that primary gliders went out of fashion in the 1930s and few have been built since.[1][2][3]

Design and development

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Jongblood designed and built this primary glider in 1966, with assistance from Hugh Knoop. The design was original and includes an originalairfoil design as well, designated as aJongblood II section.[1][2]

The aircraft is built from wood and covered in dopedaircraft fabric covering. The glider has a detachable pod to cover the pilot or can be flown open cockpit. It has a constant chord wing with a 4 ft (1.2 m) chord and a 32.5 ft (9.9 m) span. The wing features dual parallelstruts andjury struts, but has nospoilers or other glidepath control devices. Thetailplane is alsostrut-braced. Unlike most earlier primary glider designs that land on a fixed skid, this aircraft has a fixed monowheel.[1]

Only one was ever constructed.[1]

Operational history

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The Primary had accumulated over 200auto-tows and sevenaerotows, along with nine hours of flying time, by the end of 1968 and by 1983 had flown 22 hours total. It had flown a single three-hour flight and had recorded a height gain of 8,000 ft (2,438 m).[1]

By 1983 the aircraft was reported as being in storage. In May 2011 it was still on theFederal Aviation Administration registry listings, although itsregistration had expired on 31 March 2011.[1][2]

Specifications (Jongblood Primary)

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Data from Soaring[1]

General characteristics

  • Crew: one
  • Wingspan: 32 ft 6 in (9.91 m)
  • Wing area: 125 sq ft (11.6 m2)
  • Aspect ratio: 8:1
  • Airfoil: Jongblood II
  • Empty weight: 270 lb (122 kg)
  • Gross weight: 450 lb (204 kg)

Performance

  • Maximum glide ratio: 8:1 at 30 mph (48 km/h)

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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  1. ^abcdefgSaid, Bob:1983 Sailplane Directory,Soaring Magazine, page 44Soaring Society of America November 1983. USPS 499-920
  2. ^abcFederal Aviation Administration (May 2011)."Make / Model Inquiry Results". Archived fromthe original on August 12, 2012. RetrievedMay 16, 2011.
  3. ^Activate Media (2006)."Dagling T.3 Slingsby". Archived fromthe original on July 16, 2011. RetrievedMay 16, 2011.
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