Pacific D-8

The Pacific D-8 is an American, single-seat, high-wing glider, that was designed by Ken Coward and made available as plans for amateur construction.[3][4][5]

This article is about the American glider. For the unrelated the Czech motorglider with the same designation, see Pro FE D-8 Moby Dick.
D-8
Role Glider
National origin United States
Manufacturer Pacific Aircraft Company[1]
Designer Ken Coward
First flight May 1964
Introduction 1963
Status No longer available
Number built 5[2]

Design and development

The D-8 was conceived by Coward as an easy-to-build and inexpensive all-aluminium glider with good performance, that could be flown with or without a canopy. Later flight testing of a completed D-8 showed that the hoped-for performance was not achieved as the glide ratio was measured at just 17:1 with no canopy fitted.[3][4]

Coward designed the D-8 and sold plans, but never built a prototype. The first D-8 was built by Klaus Hill and Bruno Hauffe who purchased plans in 1963. Virl Kimber made the first flight of the aircraft in May 1964. Early aircraft built showed that the ailerons and rudder were too small and that the wing was set at too high an angle of incidence for safety and most were subsequently modified. The plans were changed to incorporate larger ailerons. The all-metal wing is a one piece unit 32 ft (9.8 m) in span and 125 lb (57 kg) in weight, that proved a challenge to design a trailer to carry.[5]

At least five were completed, including one built by members of the Lockhaven Glider Club in Pennsylvania. That same aircraft was used for extensive flight testing by a subsequent owner to accurately measure its performance. One was built as a powered motor glider.[2][3][4][6]

Specifications (D-8)

Data from Sailplane Directory and Soaring[3][4]

General characteristics

  • Crew: one
  • Wingspan: 31 ft 8 in (9.65 m)
  • Wing area: 100 sq ft (9.3 m2)
  • Airfoil: Modified NASA 4418
  • Empty weight: 253 lb (115 kg)
  • Gross weight: 460 lb (209 kg)

Performance

  • Maximum glide ratio: 17:1 (measured, no canopy)
  • Rate of sink: 252 ft/min (1.28 m/s) (measured, no canopy)
  • Wing loading: 4.6 lb/sq ft (22 kg/m2)

See also

Aircraft of comparable role, configuration, and era

References
  1. Air Trails: 80. Winter 1971. Missing or empty |title= (help)
  2. Federal Aviation Administration (March 2011). "Make / Model Inquiry Results". Retrieved 22 March 2011.
  3. Activate Media (2006). "D-8 Pacific". Archived from the original on 10 May 2002. Retrieved 22 March 2011.
  4. Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 17. Soaring Society of America, November 1983. USPS 499-920
  5. Renshaw, Kevin: Pacifying the Pacific D-8, Soaring Magazine Volume 46, Number 8, August 1982 pages 22-25. Soaring Society of America.
  6. Federal Aviation Administration (March 2011). "Make / Model Inquiry Results". Retrieved 22 March 2011.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.