EFFECTS OF LIQUID PROPELLANT EXPLOSIONS ON NUCLEAR ROCKET ENGINES. Final Report.
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Exploring the Mechanism of Ammonium Dinitramide Synthesis through DFT Calculations. [PDF]
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Free surface bubbly flow in an open capillary channel. [PDF]
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Effect of aluminum and ammonium perchlorate particle sizes on the condensed combustion products characteristics of aluminized NEPE propellants. [PDF]
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Design and characterization of high-performance energetic hydrogels with enhanced mechanical and explosive properties. [PDF]
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