Influence of Hydroxyl-Terminated Polybutadiene Variants on the Wettability of Ammonium Perchlorate
Author:
Affiliation:
1. California State University, Long Beach, Long Beach, California 90840
2. Naval Air Warfare Center Weapons Division, China Lake, California 93555
Funder
Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38607
Reference41 articles.
1. Burning Rate of Solid Propellant Ingredients, Part 1: Pressure and Initial Temperature Effects
2. Oxidizer coarse-to-fine ratio effect on microscale flame structure in a bimodal composite propellant
3. Comprehensive Study of Ammonium Perchlorate Particle Size/Concentration Effects on Propellant Combustion
4. An experimental study of the effects of catalysts on an ammonium perchlorate based composite propellant using 5kHz PLIF
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