NASA NTRS · 19670048114
Results from short-duration altitude-chamber techniques for simulating rocket base heating problems.
Abstract
Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
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Wilson, H. B., Jr.. 1967-05-01. Results from short-duration altitude-chamber techniques for simulating rocket base heating problems.. https://ntrs.nasa.gov/citations/19670048114
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