Conclusions
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1.
As a result of the action of ultraviolet and ionizing radiations and thermal cycling, partial destruction of the adhesive, which causes partial removal of the polymer from the irradiated surface, and a reduction of the dynamic moduli of elasticity and the speed of sound in the glasslike state are observed in KMU-3l. In the case of shielding of the fiberglass surface with a protective film, damage of the sample surface is eliminated.
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2.
Prolonged action of natural factors causes the appearance of additional transverse bonds due to the formation of reactive groups, a reduction of the internal stresses, and an increase in the structural uniformity of the adhesive, which results in an improvement of a number of physicomechanical indicators, an expansion of the temperature range of the work capacity, and a stabilization of the physicomechanical characteristics.
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3.
KMU-3l fiberglass on the whole preserves for 686 days a high level of physicomechanical characteristics and a work capacity over a wide temperature range.
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Literature cited
I. P. Khoroshilova, T. R. Kapitonova, and V. P. Lozovskaya, “KMU-3148-03, KMU-l-04n, and KMU-3 epoxy fiberglasses,” in: Aviation Materials. Nonmetallic Composite Materials [in Russian], No. 2, Moscow (1977), pp. 19–23.
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I. I. Perepechko and L. A. Kvacheva, Vysokomolekulyar. Soed., Ser. B,11, No. 1, 3 (1969).
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Translated from Mekhanika Kompozitnykh Materialov, No. 2, pp. 211–215, March–April, 1983.
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Gunyaev, G.M., Dushin, M.I., Ivonin, Y.N. et al. Effect of natural exposure in space on the physicomechanical properties of fiberglass. Mech Compos Mater 19, 144–148 (1983). https://doi.org/10.1007/BF00604215
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DOI: https://doi.org/10.1007/BF00604215