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keywords:(metal particle)
Evaluation of Additively Manufactured Metals for Use on Oxygen Systems
Pocket Model for Aluminum Agglomeration Based on Propellant Microstructure
Overview of CERMET Fuel Development at Marshall Space Flight Center
Thermal Characteristics of Rocket Jet Containing Alumina Particles
Design Issues for Propulsion Systems Using Metallized Propellants
Antiaircraft System and Method Employing Small Projectiles
Advanced Launch Vehicle Upper Stages Using Liquid Propulsion and Metallized Propellants
Upper Stages Using Liquid Propulsion and Metallized Propellants
Launch Vehicle Performance Using Metallized Propellants
Powdered Magnesium-Carbon Dioxide Rocket Combustion Technology for In Situ Mars Propulsion
Purdue University Get Away Special II (PUGAS II)
Radar Attenuation Measurements of Selected Solid Propellants and the Effect of Additives