TWO competing needs in the solid rocket motor (SRM) industry are reducing development
costs and improving reliability, both of which require better capability to simulate SRM …

BURNING of solid propellant (SP) is mostly unsteady due to the changes in burning
environment in response to transient events such as initial pressurization, combustion …

To efficiently compute arbitrary propellant grain evolution of the burning surface with uniform
and non-uniform burning rate for solid rocket motor, a unified framework of burning surface …

In this study, the design of a solid propellant grain is optimized using neural networks.
Variables must be balanced while designing a solid propellant grain to achieve the required …

This research investigated the 3D printing and burning of fuel grains with complex geometry
and the development of software capable of modeling and predicting the regression of a …

The evolution of multi-dimensional grains of solid rocket motor propellant was carried out
using the partial interface tracking method. This method applies the Lagrangian approach to …

A computationally efficient high-order solver is developed to compute the wall distances by
solving the relevant partial differential equations, namely: Eikonal, Hamilton–Jacobi (HJ) …

A detailed study of a set of combined acceleration methods is presented with the objective of
accelerating the solid rocket motor grain burnback simulation based on the level set method …

The presence of the erosive burning effect during the operation of a solid rocket motor
(SRM) is one of the most important factors affecting the proper operation of the motor. To …

Determination of the grain geometry is an important and critical step in the design of solid
propellant rocket motors, because accurate calculation of grain geometrical properties plays …