Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach-Reference-Cited by-同舟云学术

Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach

Published:2018-07 Issue:4 Volume:55 Page:936-947
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Tola Ceyhun¹,Nikbay Melike¹

Affiliation:

1. Istanbul Technical University, Istanbul 34469, Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34066

Reference18 articles.

1. A Review of Analytical Methods for Solid Rocket Motor Grain Analysis

2. A Hybrid Approach for Design Optimization of Wagon Wheel Grain for SRM

3. A Hybrid Optimization Approach for SRM FINOCYL Grain Design

4. AcikS. “Internal Ballistic Design Optimization of a Solid Rocket Motor,” M.S. Dissertation, Mechanical Engineering Dept. Middle East Technical Univ., Ankara, Turkey, 2010.

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