This sampling of newly released saucer-type aircraft documents contain detailed technical data and drawings related to the work undertaken by AVRO Aircraft Limited for the Air Force under Project 1794.

Project 1794 was interested in designing and testing a proposed supersonic vertical take-off and landing saucer type aircraft in 1957-58.

The Air Force Declassification Office declassified these documents in June 2001 and the National Declassification Center, National Archives, just recently approved them for public release.

Below are direct links to four documents.

Declassified Documents

Project Planning Report Project 1794, February 1957 [124 Pages, 22.6MB ]

Project Planning Report Project 1794 Final Development Report, 2 April – 30 May 1956 [116 Pages, 29.8MB]

Special Projects Group Technical Report No. 112, September 1957 [217 Pages, 15.3MB]

Untitled Project 1794 Report, Date Unknown [37 Pages, 4.75MB]

The post Project 1794 (Saucer-Type Aircraft) first appeared on The Black Vault.

Project Silver Bug was the American “Black” project version of the Avro Aircraft Canada Y-2 undertaken by the United States Air Force in 1953.

Declassified Documents

Project Silver Bug Technical Report

Loading...

Taking too long?

Reload document

| Open in new tab

Download [580.60 KB]

The post Project Silver Bug first appeared on The Black Vault.

The VZ-9-AV Avrocar (official designation but often listed as VZ-9) was a Canadian VTOL aircraft developed by Avro Aircraft Ltd. as part of a secret U.S. military project carried out in the early years of the Cold War.

The Avrocar intended to exploit the Coandă effect to provide lift and thrust from a single “turborotor” blowing exhaust out the rim of the disk-shaped aircraft to provide anticipated VTOL-like performance. In the air, it would have resembled a flying saucer.

Two prototypes were built as “proof-of-concept” test vehicles for a more advanced USAF fighter and also for a U.S. Army tactical combat aircraft requirement. In flight testing, the Avrocar proved to have unresolved thrust and stability problems that limited it to a degraded, low-performance flight envelope; subsequently, the project was cancelled in 1961.

Declassified Documents

The Avrocar Flight Test Plan, 15 July 1959 [14 Pages, 1mb]

 Analysis of Tests of the Avrocar in the NASA 40 x 80ft Wind Tunnel, Ames Research Center, February 1961 [298 Pages, 187MB] – An analysis is presented of some aspects of the full scale wind tunnel tests of the Avrocar vehicle. Methods used to analyze force and pressure data are formulated and results are compared with theory and small scale model tests. Aerodynamically, the performance demonstrated by the first Avrocar vehicle in its initial configuration was disappointing in that a low lift curve slop, a large nose-up pitching moment and insufficient jet vectoring capability precluded flight in free air and in the ground cushion above about 35 mph. Modifications to the aircraft based on these and other test results have been made, the major change being in the redesign of the trailing edge region where a rearwardfacing nozzle, containing a pitch control vane to provide adequate jet vectoring control, has been incorporated. The jet flap effect thus obtained is expected to allow flight in free-air as well as at higher speeds in the ground cushion.

History of the Air Force Flight Test Center, Edwards Air Force Base, California, 1 January – 30 June 1961 [4 Pages, 1.69mb] – This is a partial release of this document, which includes only the portion on the Avrocar and the title page.

The post Avrocar first appeared on The Black Vault.