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Lockheed Vega

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Lockheed Vega
Red Lockheed Vega 5b flown by Amelia Earhart in breaking two world records.
Role transport
Manufacturer Lockheed Aircraft Limited
Designer John Knudsen Northrop and Gerrard Vultee
First flight July 4, 1927
Introduction Template:Avyear
Status 6 surviving examples (?)
Primary users Commercial air carriers
USAAC
Number built 132

The Vega was a six-passenger monoplane built by the Lockheed company starting in 1927. It became famous for its use by a number of record breaking pilots who were attracted to the rugged and very long-ranged design. Amelia Earhart became the first woman to fly the Atlantic single handed in one, and Wiley Post flew his around the world twice.

Design and development

Designed by John Knudsen Northrop and Gerrard Vultee, both of whom would later form their own companies, the plane was originally intended to serve with Lockheed's own airline routes. They set out to build a four-seat aircraft that was not only rugged, but the fastest aircraft as well. Utilizing the latest designs in monocoque fuselages, cantilever wings and the best engine available, the Vega delivered on the promise of speed.

The fuselage was monocoque, built from sheets of plywood, skinned over wooden ribs. Using a large concrete mold, a single half of the fuselage shell was laminated in sections with glue and then a rubber bladder was lowered into the mold and inflated with air to compress the lamination into shape. Two fuselage halves were then nailed and glued over a previously made rib framework. With the fuselage constructed in this fashion, the wing spar had to be kept clear, so they decided to make a single spar cantilever mounted on the very top of the aircraft. The only part of the aircraft that wasn't particularly streamlined was the landing gear although production versions wore sleek "spats". For power they chose the Wright Whirlwind, which delivered 225 horsepower (168 kW).

Operational history

US Air Corps Y1C-12. [1]

The first Vega 1, named the Golden Eagle, flew from Lockheed's Los Angeles plant on July 4, 1927. It could cruise at a then-fast 120 mph (193 km/h), and had a top speed of 135 mph (217 km/h). However. the four-passenger (plus one pilot) load was considered too small for airline use. A number of private owners placed orders for the design however, and by the end of 1928, they had produced 68 of this original design. In the 1928 National Air Races in Cleveland, Vegas won every speed award.

Looking to improve the design, Lockheed delivered the Vega 5 in 1929. Adding the Pratt & Whitney R-1340 Wasp engine of 450 hp (336 kW) improved weights enough to allow two more seats to be added. A new NACA cowling increased cruise speed to 155 mph (249 km/h) and top speed to 165 mph (266 km/h). However, even the new six-seat configuration proved to be too small, and the 5 was purchased primarily for private aviation and executive transport. A total of 64 Vega 5s were built. In 1931, the US Air Corps bought two Vega 5s; one designated C-12 and one as the C-17. The C-17 differed by having an extra set of fuel tanks in the wings.

The Vega could be difficult to land. In her memoir, Elinor Smith wrote that it had "all the glide potential of a boulder falling off a mountain."[1] In addition, forward and side visibility from the cockpit was extremely limited; Lane Wallace, a columnist for Flying magazine, wrote that "Even [in level flight], the windscreen would offer a better view of the sky than anything else, which would make it more of a challenge to detect changes in attitude or bank angle. On takeoff or landing, there'd be almost no forward visibility whatsoever."

Variants

Vega 1
Five-seat cabin monoplane, accommodation for one pilot and four passengers, powered by a 225-hp (168-kW) Wright J-5, J-5A, J-5AB or J-5C Whirlwind radial piston engine.
Vega 2
Five-seat cabin monoplane, powered by a 300-hp (224-kW) Wright J-6 Whirlwind radial piston engine.
Vega 2A
Redesignation of one Vega 2 aircraft, modified for higher gross weights operators.
Vega 2D
Redesignation of two Vega 1s and one Vega 2, each fitted with a 300-hp (224-kW) Pratt @ Whitney Wasp radial piston engine.
Vega 5
Improved version, powered by a 410-hp (306-kW) Wasp A, 450-hp (336-kW) Wasp B or 420-hp (313-kW) Wasp C1 radial piston engine.
Vega 5A Executive
Executive transport version, with a plush interior.
Vega 5B
Seven-seat passenger transport version, built for higher gross weight operations with commercial operators.
Vega 5C
Seven-seat cabin monoplane, with revised tail surfaces, built for higher gross weight operations.
DL-1
Vega 5C with a light alloy fuselage. Built by the Detroit Aircraft Corporation.
DL-1B
Seven-seat cabin monoplane, similar to the DL-1. Built by the Detroit Aircraft Corporation.
DL-1 Special
One-off air racing and record breaking version. One was built by the Detroit Aircraft Corporation, exported to the United Kingdom.
Y1C-12
One DL-1 acquired by the US Army Air Corps for service tests and evaluation.
Y1C-17
One DL-1B acquired by the US Army Air Corps for service tests and evaluation.
UC-101
One Vega 5C impressed into service with the US Army Air Force in 1942.

Survivors

Wiley Post's "Winnie Mae," a model 5C, at the Steven F. Udvar-Hazy Center

Operators

 Australia
 United States

Specifications (Vega 5)

General characteristics

Performance

See also

Related development

Related lists

References

Notes
  1. ^ Smith 1981, p. 94.
  2. ^ Lockheed 5B Vega Note: Amelia Earhart's Vega 5B, a company demonstrator was c/n 22 NC7952.
  3. ^ "The Return of the Winnie Mae." Sport Aviation, October 1969.


Bibliography
  • Allen, Richard Sanders. Revolution in the Sky: Those Fabulous Lockheeds, The Pilots Who Flew Them. Brattleboro, Vermont: The Stephen Greene Press, 1964.
  • Boyne, Walter J. Beyond the Horizons: The Lockheed Story. New York: St. Martin's Press, 1998. ISBN 0-312-19237-1.
  • Francillon, René J. Lockheed Aircraft since 1913. Annapolis, Maryland: Naval Institute Press, 1987. ISBN 0-85177-835-6.
  • Smith, Elinor. Aviatrix. New York: Harcourt Brace Jovanovich, 1981. ISBN 0-15110-372-0.