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Effects of Aluminum Additions on the Specific Impulse of Propellants Based on High-Enthalpy Oxidizers Containing NO2 and NF2 Groups Full article

Journal Russian Journal of Physical Chemistry B
ISSN: 1990-7923 , E-ISSN: 1990-7931
Output data Year: 2019, Volume: 13, Number: 5, Pages: 755-762 Pages count : 8 DOI: 10.1134/s1990793119040183
Authors Dorofeenko E.M. 1 , Sheremetev A.B. 2 , Lempert D.B. 1
Affiliations
1 Institute of Problems of Chemical Physics, Russian Academy of Sciences, Chernogolovka, Moscow oblast, 142432 Russia
2 Zelinskii Institute of Organic Chemistry, Russian Academy of Sciences, Moscow, 119991 Russia

Abstract: The combustion products ratio and the energy characteristics were evaluated for solid composite propellants containing a mixture of 5,10-bis(trinitromethyl)furazano[3,4-e]di([1,2,4]triazolo)[4,3-a:3',4'-c]pyrazine (I) and 5,10-bis(difluoroamino-dinitromethyl)furazano[3,4-e]di([1,2,4]triazolo)[4,3-a:3',4'-c]pyrazine (II), a binder, and aluminum in various ratios. The introduction of small amounts of Al made it possible to increase the achieved specific impulse Isp by 2.0–2.5 s; the increase was maximum at F/H > 1, but stopped after COF2 started to form in the combustion products at the nozzle exit.
Cite: Dorofeenko E.M. , Sheremetev A.B. , Lempert D.B.
Effects of Aluminum Additions on the Specific Impulse of Propellants Based on High-Enthalpy Oxidizers Containing NO2 and NF2 Groups
Russian Journal of Physical Chemistry B. 2019. V.13. N5. P.755-762. DOI: 10.1134/s1990793119040183 WOS Scopus OpenAlex
Identifiers:
≡ Web of science: WOS:000501181400005
≡ Scopus: 2-s2.0-85075623390
≡ OpenAlex: W2990675489
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