Precise Design of Solid Rocket Motor Heat Insulation Layer Thickness under Nonuniform Dynamic Burning Rate
With the purpose of obtaining optimal designs of the heat insulating layers in solid rocket motors, we have proposed a numerical approach to compute the ideal thickness of the heat insulating layer. The proposed method is compatible with solid rocket motors that have any shape and any manner of eros...
Main Authors: | Ran Wei, Futing Bao, Yang Liu, Weihua Hui |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2019-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2019/5789430 |
Similar Items
-
Combined Acceleration Methods for Solid Rocket Motor Grain Burnback Simulation Based on the Level Set Method
by: Ran Wei, et al.
Published: (2018-01-01) -
Erratum to “Combined Acceleration Methods for Solid Rocket Motor Grain Burnback Simulation Based on the Level Set Method”
by: Ran Wei, et al.
Published: (2018-01-01) -
A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors
by: Yanjie Ma, et al.
Published: (2019-01-01) -
Parameters Affecting the Erosive Burning of Solid Rocket Motor
by: Abdelaziz Almostafa, et al.
Published: (2018-01-01) -
Thermo-Structural Response Caused by Structure Gap and Gap Design for Solid Rocket Motor Nozzles
by: Lin Sun, et al.
Published: (2016-06-01)