MacCready Gossamer Albatross: Difference between revisions

Gossamer Albatross
	The Gossamer Albatross II at Dryden Flight Research Center in 1980
Role	experimental aircraft
National origin	United States
Manufacturer	AeroVironment
Designer	Paul MacCready
First flight	1979
Status	museum piece (both)
Number built	2
Developed from	Gossamer Condor
Developed into	Gossamer Penguin

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Revision as of 10:45, 14 July 2012

The Gossamer Albatross is a human-powered aircraft built by American aeronautical engineer Dr. Paul B. MacCready's AeroVironment. On June 12, 1979 it completed a successful crossing of the English Channel to win the second Kremer prize.

Design and development

The aircraft was designed and built by a team led by Paul B. MacCready, a noted US aeronautics engineer, designer, and world soaring champion. Gossamer Albatross was his second human-powered aircraft, the first being the Gossamer Condor, which had won the first Kremer prize on August 23, 1977 by completing a mile-long figure-eight course. The second Kremer challenge was then announced as a flight across the Channel recalling Louis Blériot's crossing of 1909.

The Albatross was powered using pedals to drive a large two-bladed propeller. Piloted by amateur cyclist Bryan Allen, it completed the 35.8 km (22.2 mi) crossing in 2 hours and 49 minutes, achieving a top speed of 29 km/h (18 mph) and an average altitude of 1.5 metres (5 ft).

The aircraft is of unusual "canard" configuration, using a large horizontal stabilizer forward of the wing in a manner similar to the Wright brothers' successful "Flyer" aircraft. The Gossamer Albatross was constructed using a carbon fiber frame, with the ribs of the wings made with expanded polystyrene; the entire structure was then wrapped in a thin, transparent plastic (mylar aka PET film). The empty mass of the structure was only 32 kg (71 lb), although the gross mass for the Channel flight was almost 100 kg (220 lb). To maintain the craft in the air it was designed with very long tapering wings (high aspect ratio), like those of a glider, allowing the flight to be undertaken with a minimum of power. In still air the required power was of the order of 0.4 horsepower (300 W), though even mild turbulence made this figure rise rapidly. The Albatross I is on display at the Smithsonian Institution's Udvar-Hazy Center.

MacCready's team built two Albatrosses; the back-up plane was jointly tested as part of the NASA Langley/Dryden flight research program in 1980 and was also flown inside the Houston Astrodome, the first ever controlled indoor flight by a human-powered aircraft. The Albatross II is currently on display at the Museum of Flight in Seattle, Washington.

Solar-powered variants

A follow-up to the Albatross was the solar-powered Gossamer Penguin in 1980. The Penguin airframe had been built by the MacCready team as a third craft for the cross-channel attempt; in most of its dimensions it was three-quarters the size of the Gossamer Albatross, and was held in reserve as a speedier if slightly higher-powered alternative to be used if it were found that the Channel weather precluded success by the slower-flying Albatross. The Penguin was fragile and not very airworthy, but led to a better aircraft, the Solar Challenger. Designed by Paul MacCready, the Solar Challenger had a wingspan of 14.3 meters (47 ft) and a mass of 90 kilograms (198 pounds). Its wings were covered with 16,128 photovoltaic cells, with a total output power of 2,600 watts, about enough to drive a pair of hair dryers. The Solar Challenger was capable of reaching an altitude of 12,000 feet (3,700 m). On July 7, 1981 the aircraft, piloted by Steve Ptacek, accomplished the 262 kilometer (163 mile) flight from Paris to Manston in the UK.^[1]

Specifications (Gossamer Albatross)

Data from MuseumofFlight.org^[2]

General characteristics

Crew: 1

Performance

Notes and references

^ "Solar-Powered UAVS: HALSOL & Solar HAPP", The Prehistory Of Endurance UAVs, by Greg Goebel, in the Public Domain
^ MuseumofFlight.org, Referenced May 19, 2010

External links

[vector1-1] "Solar-Powered UAVS: HALSOL & Solar HAPP", The Prehistory Of Endurance UAVs, by Greg Goebel, in the Public Domain

[Gossamer_Specs-2] MuseumofFlight.org, Referenced May 19, 2010

[1]

[2]

@@ Line 31: / Line 31: @@
 [[Image:Gossamer_cabin.jpg|thumb|left|The cabin of the Gossamer Albatross]]
-The aircraft is a "[[canard (aeronautics)|canard]]" configuration, using a large foreplane in front of the main wing that is   used by the pilot to maintain pitch in a manner similar to the [[Wright brothers]]' successful [[Wright Flyer|"Flyer"]] aircraft. The ''Gossamer Albatross'' was constructed using a [[carbon fiber]] frame, with the ribs of the wings made with expanded [[polystyrene]]; the entire structure was then wrapped in a thin, transparent plastic ([[BoPET|mylar]] aka [[BoPET|PET film]]). The empty mass of the structure was only 32&nbsp;kg (71&nbsp;lb), although the gross mass for the Channel flight was almost 100&nbsp;kg (220&nbsp;lb). To maintain the craft in the air it was designed with very long tapering wings (high [[aspect ratio (wing)|aspect ratio]]), like those of a glider, allowing the flight to be undertaken with a minimum of power. In still air the required power was of the order of 0.4 horsepower (300 W), though even mild turbulence made this figure rise rapidly. The Albatross I is on display at the Smithsonian Institution's [[Udvar-Hazy Center]].
+The aircraft is of unusual "[[canard (aeronautics)|canard]]" configuration, using a large horizontal stabilizer forward of the wing in a manner similar to the [[Wright brothers]]' successful [[Wright Flyer|"Flyer"]] aircraft. The ''Gossamer Albatross'' was constructed using a [[carbon fiber]] frame, with the ribs of the wings made with expanded [[polystyrene]]; the entire structure was then wrapped in a thin, transparent plastic ([[BoPET|mylar]] aka [[BoPET|PET film]]). The empty mass of the structure was only 32&nbsp;kg (71&nbsp;lb), although the gross mass for the Channel flight was almost 100&nbsp;kg (220&nbsp;lb). To maintain the craft in the air it was designed with very long tapering wings (high [[aspect ratio (wing)|aspect ratio]]), like those of a glider, allowing the flight to be undertaken with a minimum of power. In still air the required power was of the order of 0.4 horsepower (300 W), though even mild turbulence made this figure rise rapidly. The Albatross I is on display at the Smithsonian Institution's [[Udvar-Hazy Center]].
 [[Image:Gossamer_Albatross_II_at_the_Museum_of_Flight.JPG|thumb|The Gossamer Albatross II at the [[Museum of Flight]] in Seattle]]

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