CALCULATION AND THEORETICAL ESTIMATION OF THE ENERGY POTENTIAL OF HIGHLY FILLED PROPOSITIONAL COMPOSITIONS
- V.N. Komov, V.O. Popov
This article is devoted to the theoretical and computational studies of highly filled propellants. The dependences of the
most important characteristics of propellant compositions (the strength of gunpowder, the amount of formed gaseous products, the
combustion temperature) on the degree of filling with powerful explosives (RDX, HMX, HAV) have been established. Using the
REAL software package, the energy characteristics of promising propellants based on cellulose nitrates with a nitrogen content of
11.5% to 13.2% and a technological fluoropolymer additive F-42 have been determined. The calculated data allow you to choose
propellant compositions from a variety of formulation options for solving a wide range of problems with the required complex of
thermodynamic characteristics: (T from 1959 to 4327 K, FP from 443.7 to 1335 kJ / kg, with Mg from 27.2 to 46.4 mol / kg).
- Index terms:
powder power, propellant, high energy filler, synthetic polymer base, combustion temperature.