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(s): Aebischer, A. C.
Corporate Author(s): Goodyear Aircraft Corporation
Date of Publication: 1962-10
Pages: 111
DoD Task:
Identifier: AD0291682
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Aebischer, A. C.
Corporate Author(s): Goodyear Aircraft Corporation
Date of Publication: 1962-10
Pages: 111
DoD Task:
Identifier: AD0291682
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control