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keywords:(Double Base Propellants)
Rheological, Ballistic, and Mechanical Properties of 3D Printed, Photocured Composite Propellants
-Ferrocenedicarboxylic Acid Salts as Burning Rate Modifiers of Double-Base Propellant
Surface Temperature Measurements of Burning Solid Propellants Using Phosphor Thermography
Review of Recent Russian Work on Double Base Propellants
Preparation and Properties of HMX/Nitrocellulose Nanocomposites
Quasi-One-Dimensional Modeling of Internal Ballistics and Axial Acoustics in Solid Rocket Motors
Experimental Characterization of Transient Burning Properties of RDX–XLDB Propellant
Fast-Impulse Nanothermite Solid-Propellant Miniaturized Thrusters
Afterburning Effects on Thermal Environment of Liquid Oxygen/Kerosene Rocket Under Low Altitudes
Characterization of Propellant Modulus and Rocket Motor Stress-Free Temperature Using Stress Sensors
Numerical Modeling and Studies of Ignition Transients in End-Burning-Grain Solid Rocket Motors
Prediction of In-Flight Radio Frequency Attenuation by a Rocket Plume
Ballistic Modifiers for Propellants
Effect of Oxidizer on the Combustion Performance of Boron-Based Fuel-Rich Propellant
Method and Apparatus for Reducing Smoke at Launch of High Performance Rockets
An Ultrasonic Method for Testing the Adhesion of Plastic Coatings on Propellent Charges