Dissection Method of Solid Rocket Motor Chamber Based on Ultrasonic Vibration Sawing-Reference-Cited by-同舟云学术

Dissection Method of Solid Rocket Motor Chamber Based on Ultrasonic Vibration Sawing

Published:2021-12-07 Issue:2 Volume:47 Page:
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants Explo Pyrotec

Author:

Guo Yu¹²,Shen Zhibin¹²,Li Haiyang¹²,Cui Huiru³

Affiliation:

1. College of Aerospace Science and Engineering National University of Defense Technology Changsha 410073 P. R. China

2. Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions Changsha 410073 P. R. China

3. College of Defense Engineering Army Engineering University of PLA Nanjing 210007 P. R. China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202100153

Reference29 articles.

1. E. F. Lund Minuteman long range service life analysis overview. AIAA/SAE 12th propusion conference Palo alto California USA July 26–29 1976 AIAA Paper 76–716.

2. HTPB Propellant Aging

3. Study on the correlativity of ageing properties between motor grain and propellant carton;Li Y. L.;Journal of Solid Rocket Technology,2003

4. Introduction to missile storage life extension technology;Meng T.;China Aerospace Press,2013

5. H. Schubert K. Menke Service life determination of rocket motors by comprehensive property analysis of propellant grains. AGARD Confence Proceedings 586 Athens Greece May 10–14 1996 AGARD-CP-586.

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