NASA NTRS · 19930090156
Combustor Performance with Various Hydrogen-oxygen Injection Methods in a 200-pound-thrust Rocket Engine
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Heidmann, M F, Baker, Louis, Jr. 1958-09-30. Combustor Performance with Various Hydrogen-oxygen Injection Methods in a 200-pound-thrust Rocket Engine. https://ntrs.nasa.gov/citations/19930090156
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