Small rocket engine Patent
Regenerative cooling system for small rocket engine having restart capability and using noncryogenic hypergolic propellants
Latto, W. T., Jr.↗
Engineering topics
Publications and source records attributed to Latto, W. T., Jr..
Regenerative cooling system for small rocket engine having restart capability and using noncryogenic hypergolic propellants
Structural damage and stability problems due to exhaust jet impingement on nearby rocket vehicle surfaces
Exhaust jets - manned space flight
Interaction of highly underexpanded exhaust jets with adjacent surfaces
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