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Development of the Boeing SST Inlet, Control, and Power System
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 1, 1967 by SAE International in United States
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Functional requirements and limitations of the Boeing supersonic inlet system are presented and several of the design considerations are discussed. Some trade studies are defined and examples of current hardware concepts are presented. The overall reliability program is discussed in terms of the test program, design objectives, and cost considerations.