Development of a method to increase flight range air, aerospace and space vehicles through the application of nanotechnology

Аuthors

Altunin V. A.^1*, Davlatov N. B.^{1, 2}, Zaripova M. A.², Safarov M. M.², Gortyshov Y. F.¹, Yanovskaya M. L.³

1. Kazan National Research Technical University named after A.N. Tupolev, Kazan, Russia
2. Tajik Technical University named after academician M.S. Osimi, Dushanbe, Republic of Tajikistan
3. Central Institute of Aviation Motors, CIAM, 2, Aviamotornaya St., Moscow, 111116, Russia

*e-mail: altspacevi@yahoo.com

Abstract

An analysis of possible ways to increase the service life and efficiency of aircraft jet engines was car-ried out. The features of hydrazine liquid fuel and its application in science and technology are re-vealed. The results of experimental studies of the thermophysical and thermodynamic properties of liquid pure hydrazine under conditions of natural convection at various pressures and temperatures, as well as the results of introducing pure dry fullerenes into it, are shown. Based on experimental studies with pure hydrazine and its mixtures with pure dry carbon nanoparticles – fullerenes, a meth-od has been developed to increase the flight range of air and spacecraft for various purposes.

Keywords:

liquid pure hydrazine, pure dry fullerenes, range and flight time of aircraft

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