Development of an impact based pyroshock test setup using finite element and response surface methods-Reference-Cited by-同舟云学术

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Development of an impact based pyroshock test setup using finite element and response surface methods

Published:2023-11-07 Issue: Volume: Page:1-18
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

Kılıç Namık¹

Affiliation:

1. Research and Development, BİAS Mühendislik, İstanbul, Turkey

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2023.2278675

Reference30 articles.

1. Babuska V. S. Gomez S. Smith and C. Hammetter. 2016. “Spacecraft Pyroshock Attenuation in Three Parts.” Accessed June 10 2023. https://s3vi.ndc.nasa.gov/ssri-kb/static/resources/1413578.pdf

2. Bement L. J. and M. L. Schimmel. 1995. A Manual Pyrotechnic Design Development and Qualification . NASA. https://ntrs.nasa.gov/api/citations/19950024937/downloads/19950024937.pdf

3. Numerical Simulation of Exploding Separation for Aerospace Pyrotechnical Actuated Separation Device;Chen M.;Initiators Pyrotechnics,2007

4. On the damping effect due to bolted junctions in space structures subjected to pyro-shock

5. ECSS-E-HB-32-25A: Mechanical Shock Design and Verification Handbook. 2015. Accessed June 10 2023. https://ecss.nl/hbstms/ecss-e-hb-32-25a-mechanical-shock-design-and-verification-handbook-14-july-2015

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