Theses and Dissertations
Evaluation of the longitudinal static stability of the US-2A aircraft.
Hydrogen-oxygen relaxation effects on spacecraft operations in the 70 km to 100 km altitude region.
An Investigation of the Effects of Acceleration and Strand Length on Post-Fire Residue of Aluminized Propellants.
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Advisor
Author
Branch Of Service
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Lieutenant Commander, United States Navy (3)
Date Issued
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1970 (3)
Degree
Department
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Aeronautical Engineering (3)