Burning-Rate Predictor for Multi-Ingredient Propellants: Nitrate-Ester Propellants-Reference-Cited by-同舟云学术

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Burning-Rate Predictor for Multi-Ingredient Propellants: Nitrate-Ester Propellants

Published:2004-05 Issue:3 Volume:20 Page:440-454
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Miller Martin S.¹,Anderson William R.¹

Affiliation:

1. U.S. Army Research Laboratory, Aberdeen Proving Ground, Maryland 21005

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.10386

Reference36 articles.

1. A new approach to propellant formulation: minimizing life-cycle costs through science-based design

2. HMX and RDX - Combustion mechanism and influence on modern double-base propellant combustion

3. On the numerical accuracy of homogeneous solid propellant combustion models

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1. Investigation of Flame Structures of Double-Base Propellant and Modified Double-Base Propellant Containing Nitramine Using OH-PLIF and Kinetic Simulation;Molecules;2024-03-06

2. Modeling transient combustion and regression behavior of NEPE propellant based on random particle packing;Applied Mathematical Modelling;2024-02

3. Laser Ignition of Two Low-Vulnerability RDX-Based Gun Propellants: Influence of the Atmosphere on Ignition and Combustion Properties;Combustion Science and Technology;2023-02-27

4. High‐Pressure Combustion Studies of Energetic Materials;Nano and Micro‐Scale Energetic Materials;2023-01-27

5. Effects of particle size and content of RDX on burning stability of RDX-based propellants;DEF TECHNOL;2022

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