Review on the Dewetting of the Particle‐Matrix Interface in Composite Solid Propellants

ZJ Zou, HF Qiang, YY Li… - Propellants, Explosives …, 2023 - Wiley Online Library
Dewetting is the main damage mode of composite solid propellants, and the research on the
initiation mechanism and evolution process of dewetting damage is an important way to …

Building rocstar: Simulation science for solid propellant rocket motors

W Dick, R Fiedler, M Heath - 42nd AIAA/ASME/SAE/ASEE Joint …, 2006 - arc.aiaa.org
The University of Illinois Center for Simulation of Advanced Rockets addresses the
computational simulation of solid propellant rockets from first principles using a highly …

Research on microscopic structure–activity relationship of AP particle–matrix interface in HTPB propellant

Z Zou, H Qiang, J Zhou, F Zhang, X Wang, Y Li - e-Polymers, 2024 - degruyter.com
The matrix and particle interface of hydroxyl-terminated polybutadiene (HTPB) propellant is
the weakest part of its mechanical properties, making it prone to dewetting damage and …

Model based IVHM system for the solid rocket booster

DG Luchinsky, VV Osipov… - 2008 IEEE …, 2008 - ieeexplore.ieee.org
We report progress in the development of a model-based hybrid probabilistic approach to an
on-board IVHM for solid rocket boosters (SRBs) that can accommodate the abrupt changes …

Internal ballistics simulation of a solid propellant rocket motor

MF Gomes - 2013 - search.proquest.com
Na concepção e desenvolvimento de motores foguete sólidos, o uso de ferramentas
numéricas capazes de simular, prever e reconstruir o comportamento de um dado do motor …

Bayesian framework for in-flight SRM data management and decision support

SV Osipov, DG Luchinsky… - 2007 IEEE …, 2007 - ieeexplore.ieee.org
We report progress in the development of a novel Bayesian framework for an in-flight failure
decision and prognostic (FD&P) system for solid rocket boosters (SRBs) based on a …

Fundamental understanding of propellant/nozzle interaction for rocket nozzle erosion minimization under very high pressure conditions

KK Kuo, K Brezinsky, S Hanagud, S Irle… - US Office of Naval …, 2005 - apps.dtic.mil
To substantially increase the operating pressures of future missiles, this MURI project
addresses scientific understanding and methods for mitigation of rocket nozzle erosion by …

Integrated vehicle health management for solid rocket motors

DG Luchinsky, VV Osipov… - Aerospace …, 2010 - books.google.com
Solid rocket motors (SRMs) are an integral part of human space flight providing a reliable
means of breaking away from the Earth's gravitational pull. The development and …

Model-based diagnostics and prognostics for solid rocket motors

DG Luchinsky, VV Osipov… - … Conference of the …, 2009 - papers.phmsociety.org
Progress in development of the physics model based diagnostic and prognostic system for
solid rocket motors (SRMs) of the new generation of the crew exploration vehicles is …

Development of an on-board failure diagnostics and prognostics system for Solid Rocket Booster

V Smelyanskiy, D Luchinsky, V Osipov… - 44th AIAA/ASME/SAE …, 2009 - arc.aiaa.org
We develop a case breach model for the on-board fault diagnostics and prognostics system
for subscale solid-rocket boosters (SRBs). The model development was motivated by recent …