Windward Performance Perlan II

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Perlan II
Role Glider
National origin United States
Manufacturer Windward Performance
Designer Greg Cole
Status Under development
Primary user Perlan Project

The Windward Performance Perlan II (English: Pearl) is an American mid-wing, two-seats-in-tandem, pressurized, experimental research glider that was designed by Greg Cole and is being built by Windward Performance for the Perlan Project.[1]

Design and development

The Perlan II is a follow-up design to the successful Perlan I and has as its design goal a flight exceeding 90,000 ft (27 km) in altitude. The project's goals include science, engineering and education. The aircraft will be used to study the polar vortex and its influence on global weather patterns.[1] The program also hopes to beat the 85,069ft altitude record set in 1975 by a SR-71.[2]


The aircraft is made from composites. Its 83.83 ft (25.55 m) span wing has a high aspect ratio of 27:1 and is equipped with airbrakes. The pressurization system produces a 8.5 psi differential, although the two-person crew will wear pressure suits for safety. The landing gear is a retractable monowheel gear. Because the aircraft will operate at extreme altitudes, in only 3% of sea level atmospheric pressure, it will also be flying at true airspeeds in excess of 0.5 Mach.[1] The aircraft was designed to minimize flutter and manage shock wave formation.

The original funding for the Perlan Project was provided by Steve Fossett and he flew the Perlan I, along with test pilot Einar Enevoldson to a glider altitude record of 50,761 ft (15 km) in the mountain waves of El Calafate, Argentina on 30 August 2006. Fossett was killed in a light aircraft crash a year later and the project floundered without funding. Since then more than US$2.8M has been raised to build the Perlan II, including a donation from Dennis Tito.[1] In November 2013, a crowd-funding effort was undertaken.

The Perlan II was expected to fly in early 2013 and will start with some flights in the US Sierra Nevada mountain wave. The record setting and research flights are intended to be flown in southern Argentina, by Einar Envoldson.[1]

Specifications (Perlan II)

Data from FreeFlight[1]

General characteristics

  • Crew: two
  • Length: 33.33 ft (10.16 m)
  • Wingspan: 83.83 ft (25.55 m)
  • Height: 7.25 ft (2.21 m)
  • Wing area: 263 sq ft (24.4 m2)
  • Aspect ratio: 27:1
  • Gross weight: 1,800 lb (816 kg)

Performance

  • Never exceed speed: 377 kn (434 mph, 698 km/h) 377 true airspeed, 56kts indicated
  • Service ceiling: 90,000 ft (27,000 m)
  • g limits: +6/-4

See also

Aircraft of comparable role, configuration, and era

Related lists

References

  1. ^ a b c d e f Staff report, The Perlan II project continues to develop, pages 24-25. FreeFlight, the Journal of the Soaring Association of Canada, Autumn, 2011.
  2. ^ "Gliding To The Edge Of Space". Retrieved 15 November 2013.

External links