Declassified UFO / UAP Document
Program Planning Report: Project 1794 Extension Program
AI-Generated Summary
This report details the 1957-1958 development plan for the Avro Project 1794, a circular-wing VTOL aircraft. It outlines the technical specifications, testing requirements, and funding for the construction of a flying prototype (P.V. 704) under USAF contract.
This document is a declassified Program Planning Report for the Project 1794 Extension Program, issued by Avro Aircraft Limited in April 1957. The report details a planned 20-month development program for a high-performance, supersonic VTOL (Vertical Take-Off and Landing) aircraft concept. The project is designed to supplement the company's private venture, designated P.V. 704, which involves the construction of a single flying prototype. The aircraft is described as having a circular wing planform, 35.3 feet in diameter, utilizing six Armstrong Siddeley Viper turbo-jet engines mounted radially within the wing. These engines act as gas generators to drive a pair of contra-rotating compressors via a radial in-flow turbine. The report outlines the technical requirements for the program, including design studies for potential weapon system applications (special reconnaissance, interceptor, or fighter-bomber), extensive wind tunnel testing to investigate subsonic, transonic, and supersonic flight regimes, and propulsion system development. A significant portion of the report is dedicated to the 'six Viper rig,' a test facility designed to evaluate the propulsion system's performance, including combustion and fuel system development. The document also addresses the critical stability and control challenges inherent in the circular wing design, proposing a pneumatic shutter system to manage jet exhaust direction for pitch stabilization. The program is funded by the United States Air Force, with a total requirement of $1,483,847 in Canadian funds. The report includes detailed work charts, scheduling, and cost estimates for the various phases of the project, which was scheduled to run from February 1, 1957, to October 31, 1958. The document emphasizes the necessity of further testing to confirm performance potential and to resolve issues identified in previous study contracts, particularly regarding the transonic speed range and low-speed transition regimes. The report concludes with administrative details regarding reporting requirements and the management structure of the Special Projects Group at Avro Aircraft Limited.
The Avro VTOL aircraft is essentially a proposal for a high performance supersonic aeroplane in which the entire interior of the wing is utilized for the propulsion system, air and gas flow, having also - due to the characteristics of the propulsion system and the wing planform - a VTOL-STOL capability.
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Official Assessment
The document outlines a 20-month development program for the Avro VTOL aircraft concept (Project 1794), focusing on design, aerodynamics, propulsion, and stability. It confirms the feasibility of the concept and details the plan to build a flying prototype (P.V. 704) while conducting extensive wind tunnel and static testing.
Key Persons
- J. C. M. FrostChief Design Engineer, Special Projects Group, Avro Aircraft Limited
- H. C. MoodyEngineering Manager, Special Projects Group, Avro Aircraft Limited