On the combustion of heterogeneous AP/HTPB composite propellants: A review

C Dennis, B Bojko - Fuel, 2019 - Elsevier
The combustion of ammonium perchlorate (AP) in a polymer binder matrix of hydroxyl-
terminated-polybutadiene (HTPB) is reviewed, covering the experimental and modeling …

Modeling of combustion and ignition of solid-propellant ingredients

MW Beckstead, K Puduppakkam, P Thakre… - Progress in Energy and …, 2007 - Elsevier
Techniques for modeling energetic-material combustion and ignition have evolved
tremendously in the last two decades and have been successfully applied to various solid …

Computational combustion

CK Westbrook, Y Mizobuchi, TJ Poinsot… - Proceedings of the …, 2005 - Elsevier
Progress in the field of computational combustion over the past 50 years is reviewed.
Particular attention is given to those classes of models that are common to most system …

Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization

K Chen, Z Ye, Y Yu, X Xue, Y Yu - International Communications in Heat …, 2023 - Elsevier
This work is to investigate the dynamic instability and unsteady heat and mass transfer
mechanism of Ammonium perchlorate/Hydroxyl-terminated polybutadiene (AP/HTPB) …

[KIRJA][B] Local and nonlocal micromechanics of heterogeneous materials

VA Buryachenko - 2022 - Springer
Materials that are either manufactured or occur in nature and used both in industry and in
our daily lives (metals, rocks, wood, soil, suspensions, and biological tissue) are very …

Diffuse interface method for solid composite propellant ignition and regression

M Meier, E Schmidt, P Martinez, JM Quinlan… - Combustion and …, 2024 - Elsevier
Abstract Solid Composite Propellants (SCPs) are extensively used in the field of propulsion
for their chemical and mechanical stability in long-term storage, and for having simple …

Effects of inclusions on the performance of a solid rocket motor

F Ponti, S Mini, L Fadigati, V Ravaglioli, A Annovazzi… - Acta Astronautica, 2021 - Elsevier
Some of the most common defects that can be generated during the production of solid
propellant are voids and porosity, usually associated with the casting process, and cracks …

Modeling of heterogeneous propellant combustion: A survey

TL Jackson - AIAA journal, 2012 - arc.aiaa.org
HETEROGENEOUS solid energetic materials are widely used in the aerospace and defense
industries in rockets, explosives, and diverse pyrotechnic devices. Their basic microstructure …

Micro-flow properties of NEPE propellant in a rotating depressurization combustion environment of solid rocket motor

K Chen, X Xue, Z Ye, Y Yu - Aerospace Science and Technology, 2024 - Elsevier
A profound understanding of microflow processes within the combustion chamber is
paramount for optimizing engine performance and ensuring safe operation in the realm of …

Investigation on unsteady thermal process of NEPE propellant based on an refined chemical kinetic model

K Chen, Z Ye, Y Yu, X Xue, Y Yu - International Journal of Heat and Mass …, 2024 - Elsevier
This study presents a sophisticated investigation into the intricate heat and mass transfer
mechanisms of NEPE composite propellant under realistic rocket motor conditions, with …