Effect of Me/B-Powder on the Ignition of High-Energy Materials

Detalles Bibliográficos
Parent link:Propellants, Explosives, Pyrotechnics
Vol. 46, iss. 11.— 2021.— [P. 1709-1716]
Autor principal: Korotkikh A. G. Aleksandr Gennadievich
Autor Corporativo: Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Otros Autores: Sorokin I. V. Ivan Viktorovich
Sumario:Title screen
The study of the ignition characteristics of high-energy materials (HEMs) is important in solving a number of practical problems related to the assessment of explosion safety, the calculation of transition processes in power installation for various purposes (rocket and space technologies, weapons, pyrotechnics). This paper presents the experimental data on the thermal oxidation of ultrafine powder (UFP) based on Al/B, Ti/B, Ni/B, and Fe/B and the experimental characteristics of the ignition of HEM based on ammonium perchlorate, butadiene rubber, and metal fuel. In the course of processing thermal analysis data, the values of oxidation temperatures, the specific heat effect of the oxidation reaction, and the rate of weight gain of powder during heated at a constant rate of 10 °C/min in air were determined. It was shown that the oxidation of Ti/B and Ni/B UFPs begins at temperature of 490–500 °C, which is 60–70 °C lower than the onset oxidation temperature for boron powder. The use of 15.7 wt.% the mixed UFP based on Al/B, Ti/B, Ni/B or Fe/B in HEM reduces the ignition delay time by 7–50 % compared to boron-based HEM in the range of heat flux density from 60 to 200 W/cm2. Based on experimental data of the ignition delay time versus the heat flux density, the formal activation energy, the multiplication of the specific heat flux of the reactions by the pre-exponent and the ignition temperature are calculated which could be used in mathematical modeling of the ignition for composite solid propellant containing metal fuels.
Режим доступа: по договору с организацией-держателем ресурса
Lenguaje:inglés
Publicado: 2021
Materias:
Acceso en línea:https://doi.org/10.1002/prep.202100180
Formato: Electrónico Capítulo de libro
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=665992

MARC

LEADER 00000naa0a2200000 4500
001 665992
005 20250211165408.0
035 |a (RuTPU)RU\TPU\network\37196 
035 |a RU\TPU\network\36735 
090 |a 665992 
100 |a 20211126d2021 k||y0rusy50 ba 
101 0 |a eng 
102 |a US 
135 |a drcn ---uucaa 
181 0 |a i  
182 0 |a b 
200 1 |a Effect of Me/B-Powder on the Ignition of High-Energy Materials  |f A. G. Korotkikh, I. V. Sorokin 
203 |a Text  |c electronic 
300 |a Title screen 
320 |a [References: 20 tit.] 
330 |a The study of the ignition characteristics of high-energy materials (HEMs) is important in solving a number of practical problems related to the assessment of explosion safety, the calculation of transition processes in power installation for various purposes (rocket and space technologies, weapons, pyrotechnics). This paper presents the experimental data on the thermal oxidation of ultrafine powder (UFP) based on Al/B, Ti/B, Ni/B, and Fe/B and the experimental characteristics of the ignition of HEM based on ammonium perchlorate, butadiene rubber, and metal fuel. In the course of processing thermal analysis data, the values of oxidation temperatures, the specific heat effect of the oxidation reaction, and the rate of weight gain of powder during heated at a constant rate of 10 °C/min in air were determined. It was shown that the oxidation of Ti/B and Ni/B UFPs begins at temperature of 490–500 °C, which is 60–70 °C lower than the onset oxidation temperature for boron powder. The use of 15.7 wt.% the mixed UFP based on Al/B, Ti/B, Ni/B or Fe/B in HEM reduces the ignition delay time by 7–50 % compared to boron-based HEM in the range of heat flux density from 60 to 200 W/cm2. Based on experimental data of the ignition delay time versus the heat flux density, the formal activation energy, the multiplication of the specific heat flux of the reactions by the pre-exponent and the ignition temperature are calculated which could be used in mathematical modeling of the ignition for composite solid propellant containing metal fuels. 
333 |a Режим доступа: по договору с организацией-держателем ресурса 
461 |t Propellants, Explosives, Pyrotechnics 
463 |t Vol. 46, iss. 11  |v [P. 1709-1716]  |d 2021 
610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
610 1 |a термическое окисление 
610 1 |a зажигание 
610 1 |a воспламенение 
700 1 |a Korotkikh  |b A. G.  |c specialist in the field of power engineering  |c Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences  |f 1976-  |g Aleksandr Gennadievich  |3 (RuTPU)RU\TPU\pers\34763  |9 18113 
701 1 |a Sorokin  |b I. V.  |c Specialist in the field of heat and power engineering  |c Engineer of Tomsk Polytechnic University  |f 1992-  |g Ivan Viktorovich  |3 (RuTPU)RU\TPU\pers\45838 
712 0 2 |a Национальный исследовательский Томский политехнический университет  |b Инженерная школа энергетики  |b Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)  |3 (RuTPU)RU\TPU\col\23504 
801 2 |a RU  |b 63413507  |c 20211126  |g RCR 
856 4 |u https://doi.org/10.1002/prep.202100180 
942 |c CF