Shelf-life analysis of solid rocket engine using HTPB/AP based on kinetic-chemical parameters of DSC analysis and burn on a test bench-Reference-Cited by-同舟云学术

Shelf-life analysis of solid rocket engine using HTPB/AP based on kinetic-chemical parameters of DSC analysis and burn on a test bench

Published:2019-12-18 Issue:1 Volume:42 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Gonçalves Rene F. B.^ORCID,Iwama Ernesto N.,Domingues Marcela G.,Rocco José A. F. F.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

http://link.springer.com/content/pdf/10.1007/s40430-019-2143-7.pdf

Reference16 articles.

1. Binda RV(2015) Estudo dos fatores que influenciam a predição de vida útil de motor-foguete sólido, Dissertation, Instituto Tecnológico de Aeronáutica

2. Kirchhof E et al (2016) Estimate of PBX (plastic-bonded explosive) shelf life with accelerated aging. Quim Nova 39(6):661–668

3. Gonçalves RFB, Rocco JAFF, Iha K (2013) Thermal decomposition kinetics of aged solid propellant based on ammonium perchlorate - AP/HTPB binder. In: Elkordy AA (ed) Applications of calorimetry in a wide context—differential scanning calorimetry, isothermal titration calorimetry and microcalorimetry, 1st edn. IntechOpen, pp 325–342

4. Agard G (1997) Structural assessment of solid propellant grains. In: Advisory group for aerospace research & development, p 212

5. Kubota N (2002) Propellants and explosives: thermochemical aspects of combustion, 2nd edn. Weinheim

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