Study on the Improvement of Adhesion Strength between Composite Solid Propellant, Liner, and Heat‐Resistant Material-Reference-Cited by-同舟云学术

Study on the Improvement of Adhesion Strength between Composite Solid Propellant, Liner, and Heat‐Resistant Material

Published:2020-07-03 Issue:8 Volume:45 Page:1227-1233
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Prop., Explos., Pyrotech.

Author:

Park Sungjun J.¹,Choi Sunghan H.¹,Lee Sangwon W.¹,Jeon Jongwon J.¹,Park Jungho H.¹

Affiliation:

1. Missile System Integration / Propulsion CenterHanwha Corporation Daejeon Korea

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202000031

Reference10 articles.

1. A study on the adhesion of HTPB liner and PCP propellant;Hong M. P.;Journal of the Korean Society of Propulsion Eng.,2001

2. S. E. Twichell R. B. Keller Solid Rocket Motor Internal Insulation 1976 NASA-SP-8093.

3. Thermal insulation by heat resistant polymers for solid rocket motor insulation

4. Alain Davenas Solid rocket Propulsion Technology Pergamon Press 1992.

5. The study on service life evaluation test of composite solid propellant;Song H. J.;Journal of the Korean Society of Propulsion Engineers fall conference,2012

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