Development of a hybrid method in a 3-D numerical burn-back analysis for solid propellant grains

SH Oh, HJ Lee, TS Roh - Aerospace Science and Technology, 2020 - Elsevier
This study was performed to analyze the performance of a solid propulsion system quickly
and accurately. Systems that are currently in operation use a propellant with a complicated …

Internal ballistics simulation of a NAWC tactical SRM

E Cavallini, B Favini, M Di Giacinto, F Serraglia - 2011 - asmedigitalcollection.asme.org
In the design and development of solid propellant rocket motors, the use of numerical tools
able to predict the behavior of a given motor is particularly important in order to decrease the …

P80 SRM pressure oscillations reconstruction

M Laureti, G Rossi, B Favini, F Paglia - 2018 Joint Propulsion …, 2018 - arc.aiaa.org
VEGA is a small launch vehicle developed by the European Space Agency (ESA) and ELV
SpA, the Italian company in charge of the vehicle system development, integration, and …

Numerical study on quasi-one-dimensional internal ballistics of throttling segregated fuel-oxidizer systems

W Ge, W Zhibang, W Fuqi, G Ben, W Limin… - Acta Aeronautica et …, 2024 - sciopen.com
A predictive unsteady quasi-one-dimensional internal ballistic numerical model and a set of
performance regulation mechanism formulas are established for throttling segregated fuel …

Pressure Oscillations in Aft-Finocyl SRMs

M Laureti, B Favini - AIAA Scitech 2019 Forum, 2019 - arc.aiaa.org
The problem of pressure oscillations, occurring during the quasi-steady state of aft-finocyl
solid rocket motors, is investigated by using the Q1D model AGAR (Aerodynamically …

Solid rocket motor burn simulation considering complex 3D propellant grain geometries

G Mejia, R Jachura, SR Gomes, L Rocco… - 52nd AIAA/SAE/ASEE …, 2016 - arc.aiaa.org
I. Introduction ockets based on chemical energy (with solid or liquid propellants) are
currently the only means to access Space. Therefore, research and development of this area …

Extended Application and Experimental Verification of a New Erosive Burning Model Coupled Heat Transfer between Gas and Grain Based on a Star-Grain Solid …

L Sun, Y Ma, F Bao, Y Liu, W Hui - Energies, 2022 - mdpi.com
The estimation of erosive burning is of great importance for the internal ballistics
computation of a solid rocket motor (SRM) with a large aspect ratio. Because of the variety of …

Aeroacoustics of Aft-Finocyl Solid Rocket Motors

M Laureti, G Rossi, B Favini - 2018 Joint Propulsion Conference, 2018 - arc.aiaa.org
The problem of pressure oscillations in solid rocket motors (SRMs) has received
considerable attention in the past fourty years, especially for the class of large segmented …

Numerical simulation of ignition transient for solid rocket motors with large aspect ratio

Y Ma, M Zhan, F Bao, L Sun… - 2021 12th International …, 2021 - ieeexplore.ieee.org
Despite the short duration, ignition transient plays a very important role in the whole
operation of a solid rocket motor. A two-dimensional model is proposed to simulate the …

[PDF][PDF] Vortex-sound modelling in aft-finocyl solid rocket motors

G Rossi, M Laureti, B Favini, E Cavallini… - EUCASS, 7th European …, 2017 - academia.edu
This paper has the aim to investigate the correlation between some ballistic geometrical
parameters of a SRM and the calibration of AGAR Q1D model of the pressure oscillations …