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Rutan Voyager

From Wikipedia, the free encyclopedia
American aircraft; first to fly around the world non-stop, unrefueled (1986)
"Scaled Composites Voyager" redirects here. For the Scaled Composites SpaceShipTwo "Voyager", seeVSS Voyager.
"Voyager aircraft" redirects here. For the RAF Voyager, seeFuture Strategic Tanker Aircraft. For other uses, seeVoyager (disambiguation).
Model 76 Voyager
Voyager returning from its flight
General information
TypeRecord plane
ManufacturerRutan Aircraft Factory
Designer
Number built1
RegistrationN269VA
History
Introduction date1984
First flightJune 22, 1984
Retired1987
Preserved atNational Air and Space Museum

TheRutan Model 76 Voyager is an aircraft designed byBurt Rutan that became the first to fly around the world without stopping or refueling. It was piloted byDick Rutan andJeana Yeager. The flight took off fromEdwards Air Force Base's 15,000 foot (4,600 m) runway in theMojave Desert on December 14, 1986, and ended 9 days, 3 minutes and 44 seconds later on December 23, setting aflight endurance record. The aircraft flew westbound 26,366 statute miles (42,432 km; theFAI accredited distance is 40,212 km)[1] at an average altitude of 11,000 feet (3,350 m).

Design and development

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Voyager on display in theNational Air and Space Museum, Washington DC

The aircraft was imagined byBurt Rutan and his brotherDick Rutan in 1980.[2] Burt sketched his concept for the aircraft for Dick andJeana Yeager during a lunch in 1981.[3] The idea was sketched out on the back of a napkin. Voyager was built inMojave, California over a period of five years, mainly by volunteers working under both the Rutan Aircraft Factory and an organization named Voyager Aircraft.Burt Rutan served as the lead designer for the project, and the chief aerodynamicist wasJohn Roncz.[4]

Theairframe made offiberglass,carbon fiber, andKevlar weighed 939 pounds (426 kg) when empty. With the engines included, the unladen weight of the plane was 2,250 pounds (1,020 kg). When it was fully loaded with fuel for its historic flight it weighed 9,694.5 pounds (4,397.4 kg).[5] The aircraft had an estimatedlift-to-drag ratio (L/D) of 27.[6] Thecanard and wing airfoils were custom-designed, and the aircraft was analyzed usingcomputational fluid dynamics.[7]Vortex generators were added to thecanard to reduce sensitivity to surface contamination by rain.[8]

Voyager hadfront and rear propellers, powered by separate engines. It was originally flown on June 22, 1984, powered byLycoming O-235 engines with fixed-pitch propellers.[9] In November 1985, the aircraft was rolled out, fitted with world-flight engines, an air-cooledTeledyne Continental O-240 in the forward location and a liquid-cooledTeledyne Continental IOL-200 in the aft location.[10] Both were firstly fitted with wooden, variable-pitch electrically actuatedMT-Propellers.[11] The plan was for the rear engine to be operated throughout the flight. The front engine was intended to provide additional power for takeoff and the initial part of the flight under heavy load.

On July 15, 1986, Dick Rutan and Yeager completed a test flight off the coast of California, in which they flew for 111 hours and 44 minutes, traveling 11,857statute miles (19,082 km) in twenty circuits betweenSan Luis Obispo andStewarts Point,[12][13] breaking theprevious record held since 28 May 1931 by aBellanca CH-300 fitted with aPackard DR-980 diesel engine, piloted by Walter Edwin Lees and Frederic Brossy which had set a record by staying aloft for 84 hours and 32 minutes without being refueled. The first attempt at the Voyager test flight was ended by the failure of a propeller pitch-change motor that resulted in an emergency landing atVandenberg Air Force Base.[14] On a test flight on September 29, 1986, the airplane had to make an emergency landing due to a propeller blade departing the aircraft.[15] As a result, the decision was made to switch to aluminiumHartzell hydraulically actuated propellers.[16] In acrash program, Hartzell made custom propellers for the aircraft, which were first flown on November 15, 1986.[17][18]

World flight

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Voyager's world flight takeoff took place on the longest runway atEdwards AFB at 8:01 am local time on December 14, 1986, with 3,500 of the world's press in attendance.[19] As the plane accelerated, the tips of the wings, which were heavily loaded withfuel, were damaged as they unexpectedly flew down and scraped against the runway, ultimately causing pieces(winglets) to break off at both ends (the pilot had wanted to gain enough speed for the inner wings, rather than the fragile outer wings, to lift the plane; in 67 test flights, the plane had never been loaded to capacity). The aircraft accelerated very slowly and needed approximately 14,200 feet (2.7 mi; 4.3 km) of the runway to gain enough speed to lift from the ground, the wings arching up dramatically just before take-off. The two damaged winglets remained attached to the wings by only a thin layer of carbon fiber and were removed by flying the Voyager in aslip, which introduced side-loading, tearing the winglets off completely. Some of the carbon fiber skin was pulled off in the process, exposing the blue foam core. Burt Rutan following with pilotMike Melvill determined that Voyager was still within its performance specifications despite the damage and decided to allow the flight to continue. During the flight, the two pilots had to deal with extremely cramped quarters. To reduce stress, the two had originally intended to fly the plane in three-hour shifts, but flight handling characteristics while the plane was heavy prevented routine changeovers, and they became very fatigued. Dick Rutan reportedly stayed at the controls without relief for almost the first three days of the flight.

Damaged left wingtip

The plane also continuously reminded the pilots of its pitch instability and fragility. They had to maneuver around bad weather numerous times, most perilously around the 600-mile-wide (1,000 km)Typhoon Marge.[20]Libya denied access to the country'sairspace in response toOperation El Dorado Canyon earlier that year. There were contentious radio conversations between the Rutan brothers as Dick flew around weather and, at one time, turned around and began doubling back. As they nearedCalifornia to land, afuel pump failed and had to be replaced with its twin pumping fuel from the other side of the aircraft.

In front of 55,000 spectators and a large press contingent, including 23 live feeds breaking into scheduled broadcasting across Europe and North America, the plane safely came back to earth, touching down at 8:06 a.m. at the same airfield 9 days after take-off. Rutan made three low passes over the landing field before putting Voyager down. The average speed for the flight was 116 miles per hour (187 km/h). There were 106 pounds (48 kg) of fuel remaining in the tanks,[5] only about 1.5% of the fuel they had at take-off.

Sanctioned by the FAI and theAOPA, the flight was the first successful aerial nonstop, non-refueled circumnavigation of the Earth that included two passes over the Equator (as opposed to shorter ostensible "circumnavigations" circling the North or South Pole). This feat has since been accomplished only one other time, bySteve Fossett in theVirgin Atlantic GlobalFlyer (also designed by Rutan). For the feat, Yeager, the Rutans, and crew chief/builder Bruce Evans received the 1986Collier Trophy.[21]

Specifications

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Replica of the rearTeledyne Continental Motors engine of the Rutan Voyager

Data from NASM[5]

General characteristics

  • Crew: two
  • Length: 29 ft 2 in (8.89 m)
  • Wingspan: 110 ft 8 in (33.73 m)
  • Height: 10 ft 3 in (3.12 m)
  • Wing area: 363 sq ft (33.7 m2)
  • Airfoil: Roncz 1046 (root), Roncz 1080 (tip), 1082/1082T (canard)[22]
  • Empty weight: 2,250 lb (1,021 kg)
  • Gross weight: 9,694.5 lb (4,397 kg)
  • Powerplant: 1 × TeledyneContinental O-240 4-cylinder horizontally-opposed engine, 130 hp (97 kW) (front engine)
  • Powerplant: 1 × TeledyneContinental IOL-200 4-cylinder horizontally-opposed engine, 110 hp (82 kW) (rear engine)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 122 mph (196 km/h, 106 kn)
  • Range: 24,986 mi (40,212 km, 21,712 nmi)
  • Endurance: 216 hours

See also

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References

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Notes

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  1. ^"Official FAI database". Archived fromthe original on 2013-12-24. Retrieved2012-12-23.
  2. ^"Scaled Composites/Rutan Voyager Partial Replica".eaa.org. RetrievedMarch 24, 2021.
  3. ^"Voyager Slides, Chapter 01: Voyager Chronology, a Brief Overview".dmc.tamuc.edu. Archived fromthe original on March 30, 2022. RetrievedMarch 24, 2021.
  4. ^"John Roncz, Master Aerodynamicist To Experimental Aircraft, Flies West".AVweb. Firecrown. October 5, 2023. Retrieved1 August 2024.
  5. ^abcRutan Voyager – Smithsonian National Air and Space MuseumArchived 2018-07-20 at theWayback Machine.
  6. ^David Noland, "Steve Fossett and Burt Rutan's Ultimate Solo: Behind the Scenes",Popular Mechanics, Feb. 2005 (web versionArchived 2006-12-11 at theWayback Machine).
  7. ^Lednicer, David, "A VSAERO Analysis of Several Canard Configured Aircraft", SAE paper 881485, presented at the SAE Aerospace Technology Conference and Exposition, Anaheim, California, October 1988.
  8. ^Bragg, M. B. and Gregorek, G. M., "An Experimental Study of a High Performance Canard Airfoil with Boundary Layer Trip and Vortex Generators", AIAA Paper No. 86-0781-CP, The 14th Aerodynamic Testing Conference Publication, March 1986.
  9. ^Yeager, Rutan & Patton 1987, p. 107.
  10. ^Yeager, Rutan & Patton 1987, p. 121.
  11. ^Yeager, Rutan & Patton 1987, p. 124.
  12. ^"Aerospace World".Air Force Magazine. Vol. 69, no. 3. September 1986. p. 43.
  13. ^Yeager, Rutan & Patton 1987, p. 181.
  14. ^Yeager, Rutan & Patton 1987, p. 66.
  15. ^Yeager, Rutan & Patton 1987, p. 198.
  16. ^Yeager, Rutan & Patton 1987, p. 209.
  17. ^Yeager, Rutan & Patton 1987, p. 213.
  18. ^Roncz, John G., "Propeller Development for the Rutan Voyager", SAE paper 891034, presented at the SAE General Aviation Aircraft Meeting & Exposition, Wichita, Kansas, April 1989.
  19. ^Norris 1988, p. 19.
  20. ^Joint Typhoon Warning Center (1987).Chapter 3: Northwest Pacific and North Indian Ocean Tropical CyclonesArchived 2011-06-07 at theWayback Machine. Retrieved on 2007-12-19.
  21. ^Larson, George C. (January 2012). "From Point A to Point A".Air & Space Smithsonian., p. 84.
  22. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

Bibliography

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External links

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