Experimental investigation of density and thermal capacity of liquid pure hydrazine with the introduction of pure dry fullerenes

Article

Published: 07.02.2020

Authors: Altunin V.A., Davlatov N.B., Zaripova M.A., Safarov M.M., Aliev I.N., Yanovskaya M.L.

Published in issue: #2(98)/2020

DOI: 10.18698/2308-6033-2020-2-1957

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

The paper presents the results of experimental investigation concerning the introduction of non-metallic nano-additives — pure dry fullerenes of C60, C70, C84 grades — into liquid pure hydrazine. The study shows the effect of fullerenes on increasing the efficiency of liquid pure hydrazine by changing its density and thermal capacity through the relative coefficients of the system "(hydrazine + fullerenes) / hydrazine" at temperatures T = 293…560 K and pressures P = 0,101…49.01 MPa. The ways of increasing the efficiency of aircraft engines and power plants and aircraft themselves with the use of a new fuel type "hydrazine — fullerenes" have been developed. Findings of the study are new and necessary for calculations on making efficient jet engines and power plants of expendable and nonexpendable aircraft for ground, air, aerospace and space-based dual-use basing.

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