MacCready Solar Challenger

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Solar Challenger
Solar Challenger drawing.jpg
A drawing of the Solar Challenger
Role Experimental aircraft
National origin United States
Manufacturer AeroVironment
Designer Paul MacCready
First flight6 November 1980
StatusMuseum piece
Number built1
Developed from Gossamer Penguin

The Solar Challenger was a solar-powered electric aircraft designed by Paul MacCready's AeroVironment. The aircraft was designed as an improvement on the Gossamer Penguin, which in turn was a solar-powered variant of the human-powered Gossamer Albatross. [1] It was powered entirely by the photovoltaic cells on its wing and stabilizer, without even reserve batteries, and was the first such craft capable of long-distance flight. [2] In 1981, it successfully completed a 163-mile (262 km) demonstration flight from France to England. [3]

Contents

History

The Solar Challenger was designed by a team [4] led by Paul MacCready as a more airworthy improvement on the Gossamer Penguin, directly incorporating lessons learned from flight testing the earlier aircraft. [5] As with the Gossamer Penguin, construction was sponsored by DuPont in exchange for publicity for the company's patented materials incorporated in the design. AstroFlight, Inc. supplied the motors and solar panels, designed by Robert Boucher. [2] [6] The plane's wings carried 16,128 solar cells yielding a maximum solar power of 3,800 watts. [5] It was flight tested in Western USA in winter 1980–1981. [7]

On July 7, 1981, the aircraft flew 163 miles from Pontoise – Cormeilles Aerodrome, north of Paris, France to Manston Royal Air Force Base in Manston, United Kingdom, staying aloft 5 hours and 23 minutes, with pilot Stephen Ptacek at the controls. [3] Currently the plane is owned by the Smithsonian Institution's Air and Space Museum. [8] [9]

Design

The Solar Challenger was designed to be sturdier, more powerful, and more maneuverable than the Gossamer Penguin so as to be able to withstand sustained high-altitude flight and normal turbulence. It was over three times as heavy (without pilot) as the Gossamer Penguin and had a shorter wingspan, but was proportionately more powerful, with electricity supplied by 16,128 solar cells powering two three-horsepower motors. The solar panels were directly affixed to the wing and large horizontal stabilizer, both of which had to be flat on top to accommodate them. The two motors, each 3 inches wide and 17 inches long and incorporating samarium-cobalt permanent magnets, operated in tandem on a common shaft to drive a single, controllable-pitch propeller. The design incorporated advanced synthetic materials with very high strength to weight ratios, including Kevlar, Nomex, Delrin, Teflon, and Mylar, all supplied by the aircraft's sponsor, Dupont. [2] [3]

Specifications

Data from [2] [5]

General characteristics

Performance

See also

Related development

Aircraft of comparable role, configuration, and era

Related Research Articles

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References

  1. ↑ Goebel, Greg, "Solar-Powered UAVS: HALSOL & Solar HAPP", The Prehistory Of Endurance UAVs, archived from the original on 2009-02-11, retrieved 2008-08-13
  2. 1 2 3 4 Lindsey, Robert (June 9, 1981), "Physicist's Solar Airplane Set to Challenge the English Channel", New York Times
  3. 1 2 3 Solar-Power Research and Dryden, Dryden Flight Research Center, NASA , retrieved 2008-08-13
  4. ↑ Ciotti, Paul, (2002) "More With Less", Encounter Books, San Francisco, ISBN   1-893554-50-3
  5. 1 2 3 4 Solar Challenger - Exclusive first hand report, of Paul MacCready's solar powered aircraft project Archived 2011-08-20 at the Wayback Machine Martyn Cowley, with drawings by Pat Lloyd. Aeromodeller, June 1981
  6. ↑ Boucher, Robert J, (1984), History of Solar Flight
  7. ↑ "Solar Challenger" by Don Monroe (1981) (Archive)
  8. ↑ "Solar-Plane Sets Height Record", Space Daily, August 6, 1998, retrieved 2008-08-13.
  9. ↑ "The Solar Challenger | Exhibitions | Smithsonian". www.si.edu. Archived from the original on 2013-09-26.
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