NASA NTRS · 19900034894
Hypersonic propulsion
Abstract
The paper reviews the whys and hows of the concept of supersonic combustion for hypersonic propulsion. Attention is given to the problem areas, the current research and development efforts, and their implications. The operating boundary of the SCRAMJET is reasonably well defined. The paper also explores some air-breathing alternatives that may go beyond SCRAMJETS.
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Cheng, SIN-I.. 1989-01-01. Hypersonic propulsion. https://ntrs.nasa.gov/citations/19900034894
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