Prediction of burn rate of ammonium perchlorate–hydroxyl-terminated polybutadiene composite solid propellant using supervised regression machine learning algorithms
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42401-024-00305-1.pdf
Reference22 articles.
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2. López R, Salazar A, Rodríguez J (2020) Fatigue crack propagation behaviour of carboxyl-terminated polybutadiene solid rocket propellants. Int J Fract 223(1):3–15. https://doi.org/10.1007/s10704-020-00435-5
3. Starkova O, Gagani AI, Karl CW, Rocha IB, Burlakovs J, Krauklis AE (2022) Modelling of environmental ageing of polymers and polymer composites—durability prediction methods. Polymers 14(5):907. https://doi.org/10.3390/polym14050907
4. Kumar A, Chavan PV, Bhatkhande DS, Sadavarte VS, Santosh Mada SSNM, Pande SM (2023) Migration of energetic plasticizer in advanced energetic composite propellant grains. Propell Explos Pyrotech 48(2):e202200185. https://doi.org/10.1002/prep.202200185
5. Trębiński R, Janiszewski J, Leciejewski Z, Surma Z, Kamińska K (2020) On influence of mechanical properties of gun propellants on their ballistic characteristics determined in closed vessel tests. Materials 13(14):3243. https://doi.org/10.3390/ma13143243
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