NASA technical note TN (series). D-4851. Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines [with list of references]; by Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum.
Publication Title:
Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines [with list of references]; by Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum.
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NASA technical note TN (series). D-4851. Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines [with list of references]; by Reino J. Salmi, John P. Wanhainen, and Ned P. Hannum.
Series Title:
NASA technical note TN (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
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National Aeronautics and Space Administration
Authors:
Salmi, Reino J., Wanhainen, John P., and Hannum, Ned P.