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

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

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Provenance: Lockheed Martin Missiles & Fire Control

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