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| {{Short description|1980s British human-powered aircraft}} | {{Short description|1980s British human-powered aircraft}} | ||
| {{Orphan|date=January 2025}} | |||
| {{DISPLAYTITLE:To ''Phoenix''}} | {{DISPLAYTITLE:To ''Phoenix''}} | ||
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| {{Use British English|date=January 2025}} | {{Use British English|date=January 2025}} | ||
| {|{{Infobox aircraft begin | {|{{Infobox aircraft begin | ||
| |name = | |name =To ''Phoenix'' | ||
| |image = | |image =To Phoenix.jpg | ||
| |caption = | |caption =The To ''Phoenix'' in flight, 28 March 1982 | ||
| }} | }} | ||
| {{Infobox aircraft type | {{Infobox aircraft type | ||
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| The '''Phoenix''' was a ], designed and built in the 1980s by the British architect Frederick To. It was notable for being an inflatable ] design and for its low airspeed.<ref name=AEROSPACE/><ref name=POPSCI/> | The '''Phoenix''' was a ], designed and built in the 1980s by the British architect Frederick To. It was notable for being an inflatable ] design and for its low airspeed.<ref name=AEROSPACE/><ref name=POPSCI/> | ||
| Taking inspiration from Daniel Perkins' work with the '']'', Fred To wished to resolve issues with storage and crashibility that previous human-powered aircraft had suffered from. To this end, the Phoenix was designed to have a simple layout, be easily stored, and be robust enough to survive accidents without damage.<ref name=AEROSPACE/> |
Taking inspiration from Daniel Perkins' work with the '']'', Fred To wished to resolve issues with storage and crashibility that previous human-powered aircraft had suffered from. To this end, the Phoenix was designed to have a simple layout, be easily stored, and be robust enough to survive accidents without damage.<ref name=AEROSPACE/> | ||
| ==Design and development== | ==Design and development== | ||
| The ''Phoenix'' was a flying-wing configuration, with a rectangular wing planform. A reflex aerofoil, based on a Wortmann 15% aerofoil, but increased to 20% thickness was used. An aspect ratio of 6 was selected as that was considered to be the practical limit for pitch stability for such a design. The wing was built up using polyester film, and was constructed using a series of conjoined tubes running the full span of the wing. The wing was also skinned using polyester film, with a series of curved riblets applied at intervals across the span helping to maintain the desired aerofoil cross-section. When fully deflated, the wing could be folded down and stowed onto a car's roofrack.<ref name=AEROSPACE/> |
The ''Phoenix'' was a flying-wing configuration, with a rectangular wing planform. A reflex aerofoil, based on a Wortmann 15% aerofoil, but increased to 20% thickness was used. An aspect ratio of 6 was selected as that was considered to be the practical limit for pitch stability for such a design. The wing was built up using polyester film, and was constructed using a series of conjoined tubes running the full span of the wing. The wing was also skinned using polyester film, with a series of curved riblets applied at intervals across the span helping to maintain the desired aerofoil cross-section. When fully deflated, the wing could be folded down and stowed onto a car's roofrack.<ref name=AEROSPACE/> | ||
| Downturned ] at each wingtip provided directional control. The fuselage was constructed from carbon-fibre tubing, with the pilot seated in an upright cycling position and powering the tractor propeller via a chain drive. Control was by ] and rudders in the winglets. These were operated by ] controlled by the pilot.<ref name=KITPLANES/><ref name=AEG/> |
Downturned ] at each wingtip provided directional control. The fuselage was constructed from carbon-fibre tubing, with the pilot seated in an upright cycling position and powering the tractor propeller via a chain drive. Control was by ]s and rudders in the winglets. These were operated by ] controlled by the pilot.<ref name=KITPLANES/><ref name=AEG/> | ||
| ==Flight tests== | ==Flight tests== | ||
| Initial flight tests were conducted in August 1981 at sportgrounds in ], ], when a series of three towed flights took place. During the last of these flights, the aircraft crashed from a height of {{convert|25|ft|m|abbr=on}}, without any damaged being incurred. The first human-powered flight took place on 28 March 1982, at the ], with Ian Parker acting as pilot. Further flights were made that day, all of about 20 seconds duration. It was noted that the ''Phoenix'' took a long time to reach flight speed, which To determined was due to the air mass contained within the inflatable wing being some {{convert|200|lb|kg|abbr=on}}.<ref name=AEROSPACE/><ref name=HPF/> |
Initial flight tests were conducted in August 1981 at sportgrounds in ], ], when a series of three towed flights took place. During the last of these flights, the aircraft crashed from a height of {{convert|25|ft|m|abbr=on}}, without any damaged being incurred. The first human-powered flight took place on 28 March 1982, at the ], with Ian Parker acting as pilot. Further flights were made that day, all of about 20 seconds duration. It was noted that the ''Phoenix'' took a long time to reach flight speed, which To determined was due to the air mass contained within the inflatable wing being some {{convert|200|lb|kg|abbr=on}}.<ref name=AEROSPACE/><ref name=HPF/> | ||
| Contemporary articles mentioned that To was designing a smaller, hybrid-powered inflatable HPA, with it weighing {{convert|60|lb|kg|abbr=on}} spanning {{convert|50|ft|m|abbr=on}} and flying at {{convert|15|mph|kph|abbr=on}}.<ref name=POPSCI/><ref name=JANES82/> |
Contemporary articles mentioned that To was designing a smaller, hybrid-powered inflatable HPA, with it weighing {{convert|60|lb|kg|abbr=on}} spanning {{convert|50|ft|m|abbr=on}} and flying at {{convert|15|mph|kph|abbr=on}}.<ref name=POPSCI/><ref name=JANES82/> | ||
| ==Specifications== | ==Specifications== | ||
| Line 190: | Line 191: | ||
| <ref name=HPF>{{cite web |title=Human Powered Flight - Early 80s |url=https://www.humanpoweredflight.co.uk/page/human-powered-flight-early-80s |website=Human Powered Flight |access-date=12 January 2025}}</ref> | <ref name=HPF>{{cite web |title=Human Powered Flight - Early 80s |url=https://www.humanpoweredflight.co.uk/page/human-powered-flight-early-80s |website=Human Powered Flight |access-date=12 January 2025}}</ref> | ||
| <ref name=JANES82>{{cite book |editor-last1=Taylor |editor-first1=John W. R. |date=1982 |title=Jane's All The World's Aircraft 1982-83 |location=London |publisher=Jane's Publishing Co. Ltd. |pages= |
<ref name=JANES82>{{cite book |editor-last1=Taylor |editor-first1=John W. R. |date=1982 |title=Jane's All The World's Aircraft 1982-83 |location=London |publisher=Jane's Publishing Co. Ltd. |pages=518–519|isbn=0710607482}}</ref> | ||
| <ref name=KITPLANES>{{cite web |last=Sigler |first=Dean |title=Alternative Energies |url=https://www.kitplanes.com/alternative-energies-21/ |website=Kitplanes |date=16 December 2013 |access-date=12 January 2025}}</ref> | <ref name=KITPLANES>{{cite web |last=Sigler |first=Dean |title=Alternative Energies |url=https://www.kitplanes.com/alternative-energies-21/ |website=Kitplanes |date=16 December 2013 |access-date=12 January 2025}}</ref> | ||
| Line 200: | Line 201: | ||
| ==External links== | ==External links== | ||
| * | * | ||
| ] | ] | ||
Revision as of 17:35, 12 January 2025
1980s British human-powered aircraft | This article is an orphan, as no other articles link to it. Please introduce links to this page from related articles; try the Find link tool for suggestions. (January 2025) |
| To Phoenix | |
|---|---|
| |
| The To Phoenix in flight, 28 March 1982 | |
| Role | Human-powered aircraftType of aircraft |
| National origin | United Kingdom |
| Manufacturer | Fred To |
| First flight | 1981 |
| Number built | 1 |
The Phoenix was a human-powered aircraft, designed and built in the 1980s by the British architect Frederick To. It was notable for being an inflatable tailless design and for its low airspeed.
Taking inspiration from Daniel Perkins' work with the Reluctant Phoenix, Fred To wished to resolve issues with storage and crashibility that previous human-powered aircraft had suffered from. To this end, the Phoenix was designed to have a simple layout, be easily stored, and be robust enough to survive accidents without damage.
Design and development
The Phoenix was a flying-wing configuration, with a rectangular wing planform. A reflex aerofoil, based on a Wortmann 15% aerofoil, but increased to 20% thickness was used. An aspect ratio of 6 was selected as that was considered to be the practical limit for pitch stability for such a design. The wing was built up using polyester film, and was constructed using a series of conjoined tubes running the full span of the wing. The wing was also skinned using polyester film, with a series of curved riblets applied at intervals across the span helping to maintain the desired aerofoil cross-section. When fully deflated, the wing could be folded down and stowed onto a car's roofrack.
Downturned winglets at each wingtip provided directional control. The fuselage was constructed from carbon-fibre tubing, with the pilot seated in an upright cycling position and powering the tractor propeller via a chain drive. Control was by elevons and rudders in the winglets. These were operated by RC servoes controlled by the pilot.
Flight tests
Initial flight tests were conducted in August 1981 at sportgrounds in Chiswick, West London, when a series of three towed flights took place. During the last of these flights, the aircraft crashed from a height of 25 ft (7.6 m), without any damaged being incurred. The first human-powered flight took place on 28 March 1982, at the London Docklands, with Ian Parker acting as pilot. Further flights were made that day, all of about 20 seconds duration. It was noted that the Phoenix took a long time to reach flight speed, which To determined was due to the air mass contained within the inflatable wing being some 200 lb (91 kg).
Contemporary articles mentioned that To was designing a smaller, hybrid-powered inflatable HPA, with it weighing 60 lb (27 kg) spanning 50 ft (15 m) and flying at 15 mph (24 km/h).
Specifications
Data from Jane's All the World's Aircraft 1982-83
General characteristics
- Crew: 1
- Length: 5.49 m (18 ft 0 in)
- Wingspan: 31.09 m (102 ft 0 in)
- Height: 4.22 m (13 ft 10 in)
- Wing area: 154.9 m (1,667 sq ft)
- Aspect ratio: 6
- Airfoil: Wortmann reflex
- Empty weight: 50 kg (110 lb)
- Gross weight: 109 kg (240 lb)
- Propellers: 2-bladed fixed-pitch, 5.49 m (18 ft 0 in) diameter turning @ 45 rpm
Performance
- Cruise speed: 13 km/h (8.1 mph, 7.0 kn)
See also
Aircraft of comparable role, configuration, and era
- HMPAC Puffin
- Malliga 1
- Paxton man-powered aircraft
- Perkins Reluctant Phoenix
- Weybridge Mercury
- Wright Micron
- Wright MPA Mk 1
Related lists
References
- ^ To, F.E. (June–July 1985). "Phoenix: A Polyester-Film Inflatable Man-Powered Aircraft". Aerospace. London, UK: Royal Aeronautical Society. pp. nk. ISSN 2052-451X.
- ^ Kocivar, Ben (March 1982). "Inflatable pedal plane". Popular Science. New York, NY: Times Mirror Magazines, Inc. pp. 70–71. Retrieved 12 January 2025.
- Sigler, Dean (16 December 2013). "Alternative Energies". Kitplanes. Retrieved 12 January 2025.
- "The 50th Anniversary of Human-Powered Flight". Aircraft Enthusiast's Group. Retrieved 12 January 2025.
- "Human Powered Flight - Early 80s". Human Powered Flight. Retrieved 12 January 2025.
- ^ Taylor, John W. R., ed. (1982). Jane's All The World's Aircraft 1982-83. London: Jane's Publishing Co. Ltd. pp. 518–519. ISBN 0710607482.