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scientific edition of Bauman MSTU

SCIENCE & EDUCATION

Bauman Moscow State Technical University.   El № FS 77 - 48211.   ISSN 1994-0408

Thermodynamically Modeled Non-equilibrium Structure of Combustion Products and Decomposition of Hydrazine-based Liquid Propellants

# 05, May 2016
DOI: 10.7463/0516.0841540
Article file: SE-BMSTU...o040.pdf (1517.26Kb)
authors: A.A. Dorofeev1,*, D.M. Yagodnikov1



1 Bauman Moscow State Technical University, Moscow, Russia

The paper studies the emerging hallmarks and the characteristics of a two-parameter chemical non-equilibrium structure of the combustion products of liquid propellants as applied to the low-thrust liquid propellant engines (LT LPE) operating in the aircraft control system. The study is based on hydrazine and nitrogen tetroxide products. The paper also analyses the catalytic and thermal decomposition of these substances in terms of inter-conditionality of the working process components in the combustion chamber and liquid pre-burner. The paper offers a technique to simulate these types of non-equilibrium as applied both to the a priori estimate and to the parametric optimization of LT LPE performance. It presents the possible equations of chemical dissociation reactions of hydrazine under various conditions, which determine a chemical disequilibrium of the process, and gives the examples to specify the source files for the software systems "Astra 4.rs" or "Terra".
The technique is implemented and tested on the basis of the software systems "Astra4.rs" and "Terra" in calculating the structure and properties of the liquid propellant combustion products, which include hydrazine, combustion products, ammonia, and products of their catalytic thermal decomposition. The paper provides numerical values of the upper and lower concentration limits of the non-equilibrium of a generated propellant, which correspond to the equilibrium ratio of concentrations between ammonia and products of its decomposition, as well as meet the absence of ammonia pyrolysis. For possible conditions of the non-equilibrium work process the values of void specific impulse are calculated.

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