Temat: FOX-7 - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Investigation of an Aluminized Binder/AP Composite Propellant Containing FOX-7
Autorzy:: Florczak, B.
Powiązania:: https://bibliotekanauki.pl/articles/358557.pdf
Data publikacji:: 2008
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
Tematy:: FOX-7
aluminized composite propellant
burning rate
Opis:: This paper presents the results of thermodynamical calculations and investigations of the thermochemical and balistic properties of aluminized composite solid propellants Binder/AP/A1 containing FOX-7. The calculation was conducted by using ICT-Thermodynamic Code. The heat of combustion was determined in a stationary bomb calorimeter IKA C 4000. The breakdown temperatures were taken with the DTA 551 Ex measuring apparatus and the burning rate was measured in a subscale rocket motor utilizing the ESAM v. 3.3.0 system. It was revealed that the introduction of FOX -7 into the propellant composition causes a reduction of the energetic characteristics and the burning rate of the propellant.
Źródło:: Central European Journal of Energetic Materials; 2008, 5, 3-4; 65-75
1733-7178
Pojawia się w:: Central European Journal of Energetic Materials
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

Tytuł:: A Comparison of Properties of Aluminized Composite Propellants Containing HMX and FOX-7
Autorzy:: Florczak, B.
Powiązania:: https://bibliotekanauki.pl/articles/358559.pdf
Data publikacji:: 2008
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
Tematy:: detonation transition
HMX
FOX-7
aluminized composite propellant
Opis:: Modern rocket propellants contain inter alia nitroamines (i.e. RDX, HMX). Therefore, the detonation properties of composite solid propellants are very important for good functioning of rocket motors and for storage. One of the new materials of that kind, with low sensitivity, is FOX-7 which was applied here as one of the components of composite solid propellant. This paper presents the thermodynamical calculations and thermochemical research results as well as the results of a study of transition into detonation of an aluminized composite propellant containing HMX. The said properties were compared with those of a propellant containing FOX-7.
Źródło:: Central European Journal of Energetic Materials; 2008, 5, 3-4; 103-111
1733-7178
Pojawia się w:: Central European Journal of Energetic Materials
Dostawca treści:: Biblioteka Nauki

Artykuł

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