Origins and Context
Project Silver Bug emerged from Avro Canada's Project Y-2, a classified effort to develop a disc-shaped aircraft capable of vertical takeoff and landing.1 The U.S. Air Force funded the project in 1953, seeing potential for a revolutionary combat aircraft that could operate without conventional runways.2
Program Structure
The program produced the VZ-9AV Avrocar, an 18-foot diameter experimental aircraft powered by three Continental J69 turbojet engines.3 The design used a central turbine to direct exhaust through a peripheral nozzle for lift and thrust vectoring control.4
Legacy
Despite ambitious goals of Mach 2+ speeds and 70,000+ feet altitude capability, the Avrocar proved unstable above 3 feet and never exceeded 35 mph in testing.5 The program was cancelled in 1961 after spending approximately $10 million, though it advanced understanding of VTOL technologies.6
References
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"Joint ATIC-WADC Report on Project Silver Bug." Air Technical Intelligence Center, Wright-Patterson AFB, 15 February 1955. ↩
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"Program Planning Report, Project 1794 Extension Program." National Archives and Records Administration, April 1957. ↩
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Zuk, Bill. "AVROCAR: Canada's Flying Saucer." The Boston Mills Press, 2001. ↩
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"Project 1794 Final Development Summary Report." National Archives and Records Administration, June 1956. ↩
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"Technical Report TR-AC-47: Project Silver Bug." Air Technical Intelligence Center, Wright-Patterson AFB, 1955. ↩
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Day, Dwayne. "Avrocar: The U.S. Military's Flying Saucer." Smithsonian Air & Space Magazine, 2014. ↩