The energetic potential of azo- and azoxyfurazan nitro derivatives as components of composite rocket propellants

The energetic potential of azo- and azoxyfurazan nitro derivatives as components of composite rocket propellants Научная публикация

Журнал

Chemistry of Heterocyclic Compounds
ISSN: 1573-8353 , E-ISSN: 0009-3122

Вых. Данные

Год: 2016, Том: 52, Номер: 12, Страницы: 1070-1077 Страниц : 8 DOI: 10.1007/s10593-017-2008-x

Авторы

Lempert David B. ¹ , Sheremetev Aleksei B. ²

Организации

1	Institute of Problems of Chemical Physics, Russian Academy of Sciences, 1 Akademika Semenova Ave., Chernogolovka 142432, Moscow obl., Russia
2	N. D. Zelinsky Institute of Organic Chemistry, Russian Academy of Sciences, 47 Leninsky Ave., Moscow 119991, Russia

The energetic potential of solid composite rocket propellants on the basis of solid and liquid nitro derivatives of azo- and azoxyfurazans was studied by using thermochemical calculations. Quantitative relationships were established between the energetic parameters of propellants, the selected binder, and the properties of the studied component. It was shown that the studied solid nitrofurazans can serve as the foundation of metal-free compositions of solid composite rocket propellants, giving specific impulse over 263 s, while the use of liquid nitrofurazans as plasticizers of the binder can improve the ballistic effectiveness of rocket propellants containing aluminum hydride by 2–4 s.

Lempert D.B. , Sheremetev A.B.
The energetic potential of azo- and azoxyfurazan nitro derivatives as components of composite rocket propellants
Chemistry of Heterocyclic Compounds. 2016. V.52. N12. P.1070-1077. DOI: 10.1007/s10593-017-2008-x WOS Scopus OpenAlex

≡ Web of science:	WOS:000393034400013
≡ Scopus:	2-s2.0-85030093396
≡ OpenAlex:	W2575383721