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Investigation to Determine the Feasibility of Using Inflatable Balloon Type Drag Devices for Recovery Applications in the Transonic, Supersonic, and Hypersonic Flight Regime. Part I. Functional and Performance Demonstration

Report Number: ASD TDR 62-702 Part 1
Author: Aebischer, A. C.
Corporate Author: Goodyear Aircraft Corporation
Date of Publication: 1962-10
Pages: 111
AD Number: AD0291682

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Lockheed Martin Missiles & Fire Control
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