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Not What You Meant?  There are 31 definitions for Robin.

Curtiss Robin

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Curtiss Robin
Curtiss Robin Challenger
Type Touring
Manufacturer Curtiss Aeroplane and Motor Company
Maiden flight 7 August 1928[1]
Introduced 1928
Status A number still flying[1]
Primary user U. S. Private Owner Market[1]
Number built 769[1]
Unit cost $7,500 U.S. Dollars (1938)

The Curtiss Robin, introduced in 1928, was a high wing monoplane with an 8-cylinder V8 OX-5 90 hp (67 kW) engine. It was later fitted with the more powerful Challenger engine, which developed between 170 and 185 hp (127 to 138 kW). The OX-5 version was flown by Douglas "Wrongway" Corrigan as well as The Flying Keys.

Contents

Design

The Robin, a workmanlike cabin monoplane had a wooden wing and steel tubing fuselage. The cabin accomidated three, two passegers seated side-by-side behind the pilot. Early Robins were distinguished by large flat fairings over the parallel diagional wing bracing struts, which were abandond on later versions when found ineffective at creating lift[1]. The original landing gear were bungee rubber cord shock absorbers, later replaced by an oleo-pneumatic system, a number of Robins had twin-floats added. Payload with 50 U.S. gal (190 L) fuel was 452 lb (205 kg), cruising speed 102 mph (164 km/h), landing speed 48 mph (77 km/h), gas capacity 50 U.S. gal (25 U.S. gal in each wing tank) (2×85 L), oil capacity 5 U.S. gal (19 L). Price at factory field was $7,500.

Military service

A single modified Robin (with a 110hp Warner R-420-1) was used by the United States Army Air Corps, and designated XC-10. This aircraft was used in a test program for radio-controlled (and unmanned) flight.

Specifications (Robin OX-5)

1928 Curtiss Robin advertisement. Note that the Robin in the photo does not have a radial engine.
1928 Curtiss Robin advertisement. Note that the Robin in the photo does not have a radial engine.

General characteristics

  • Crew: three
  • Length: 25 ft 1 in[2] (7.65 m)
  • Wingspan: 41 ft[2] (12.5 m)
  • Height: 8 ft[1] (2.44 m)
  • Wing area: 223 ft²[1] (20.72 m²)
  • Empty weight: 16318 lb (743 kg)
  • Loaded weight: 621 lb (436 kg)
  • Max takeoff weight: 12600 lb (1180 kg)
  • Powerplant:Curtiss OX-5 liquid-cooled V-8, 90 hp (67 kW)

Performance

References

  1. ^ a b c d e f g "The Complete Encyclopedia of World Aircraft" cover Editors: Paul Eden & Soph Moeng, (Amber Books Ltd. Bradley's Close, 74-77 White Lion Street, London, NI 9PF, 2002, ISBN 0-7607-3432-1), 1152 pp.
  2. ^ a b "U.S. Army Aircraft 1908-1946" by James C. Fahey, 1946, 64pp.

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Curtiss Robin from Wíkipedia. ©2006 by Wíkipedia. Licensed under the GNU Free Documentation License. View a list of authors or edit this article.

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