THEORETICAL COMBUSTION PERFORMANCE OF RAMJET FUELS: HYDROGEN,
Abstract
The report is the first of a series prepared as a compilation of available data on theoretical combustion performance of various fuels. The performance parameters to be given primary consideration are flame temperature and air specific impulse; others, including fuel specific impulse, mole change and expansion ratio are also included.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 13, 1956
- Accession Number
- AD0657150
Entities
People
- Waldo T. Renich
Organizations
- Johns Hopkins University Applied Physics Laboratory