- Tytuł:
- Investigation of an Aluminized Binder/AP Composite Propellant Containing FOX-7
- Autorzy:
- Florczak, B.
- Tematy:
-
FOX-7
aluminized composite propellant
burning rate - Pokaż więcej
- Wydawca:
- Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
- Powiązania:
- https://bibliotekanauki.pl/articles/358557.pdf  Link otwiera się w nowym oknie
- 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.
- Dostawca treści:
- Biblioteka Nauki
Artykuł