Engineering:Schreder HP-14

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Short description: American single-seat glider
HP-14
General information
TypeClub class Sailplane
ManufacturerHomebuilt
Designer
Richard Schreder
History
First flight1966

The HP-14 is a Richard Schreder-designed all-metal glider aircraft that was offered as a kit for homebuilding during the 1960s and 1970s.[1] It was originally developed by retrofitting improved wings to the fuselage and tail of the HP-13, and first flew in 1966.[2] Schreder won the 1966 US national soaring championship in the prototype HP-14.[3]

The HP-14 features a folding V-tail and 90-degree flaps for glidepath control. The fuselage and wings are of all-aluminum riveted construction.[3]

Development

Variants

HP-14
Developed from a modified HP-13 fuselage, with V-tail, using the Wortmann section wings of the Schreder HP-12[4]
HP-14C
An 18-meter span HP-14 produced by Slingsby with a conventional cruciform tail,[4] flown by Nicholas Goodhart at the 1968 World Championships at Leszno in Poland. The initial prototype used an enlarged V-tail.{{Citation needed|date=October 2011} ;HP-14T
The HP-14 fitted with the 18-meter 'C' wing and a T-tail.[4]
Krutchkoff SHP-1
An HP-14 with a new fuselage designed by Andre Krutchkoff.[4]
Zauner OZ-4
Modified version with a 19.2 m (63.0 ft) wingspan and a 850 lb (386 kg) gross weight.[4]

Specifications (Slingsby HP-14C)

HP-14

Data from Coates, Andrew. "Jane's World Sailplanes & Motor Gliders new edition". London, Jane's. 1980. ISBN 0-7106-0017-8

General characteristics

  • Crew: 1
  • Length: 23 ft 10.5 in (7.28 m)
  • Wingspan: 59 ft 0.5 in (18 m)
  • Height: 3 ft 11 in (1.19 m)
  • Wing area: 146.2 sq ft (13.58 m2)
  • Aspect ratio: 23.9
  • Airfoil: Wortmann FX-61-163
  • Empty weight: 639 lb (290 kg)
  • Gross weight: 840 lb (381 kg)

Performance

  • Maximum speed: 134 mph (216 km/h, 116 kn)
  • Maximum glide ratio: 44 @ 96 km/h (60 mph)
  • Rate of sink: 98.4 ft/min (0.50 m/s)

References

Template:Schreder Sailplanes Template:Otto Zauner aircraft