Assessment of Mechanical Properties of Aged Composite Propellant Using Non‐Destructive Indentation Technique in Solid Propellant Rocket Motor-Reference-Cited by-同舟云学术

Assessment of Mechanical Properties of Aged Composite Propellant Using Non‐Destructive Indentation Technique in Solid Propellant Rocket Motor

Published:2022-05-05 Issue:6 Volume:47 Page:
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants Explo Pyrotec

Author:

Kumar Bihari Bipin¹,Kumaraswamy Adepu²,Jain Mukesh¹,Murthy Krothapalli P S¹

Affiliation:

1. High Energy Materials Research Laboratory Sutarwadi Pune-411021 India

2. Defence Institute of Advanced Technology Girinagar Pune-411025 India

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202100339

Reference17 articles.

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2. R. Zalewski T. Wolszakiewicz Analysis of Uniaxial Tensile Tests for Homogeneous Solid Propellants under Various Loading Conditions Central European Journal of Energetic Materials 2011 8 223–231 ISSN 1733–7178.

3. S. Cerri M. A. Bohn K. Menke L. Galfetti Aging behaviour of HTPB based rocket propellant formulations Central European Journal of Energetic Materials 2009 6 149–165 ISSN 1733–7178

4. Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements

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