Research and Exploratory Development for the Office of Aeronautical Research, National Aeronautics and Space Administration.
Abstract
The objective of this research is to determine some of the design criteria and the expected performance of the combustor and nozzle for hypersonic ramjets with supersonic combustion of hydrogen in the flight Mach number range from 5 to at least 10. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1968
- Accession Number
- AD0846423
Entities
People
- C. L. Yates
- F. S. Billig
- J. A. Schetz
- J. L. Rice
- J. P. Wagner
Organizations
- Johns Hopkins University