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Preliminary research of composite rocket propellants with hexogen and titanium oxide powder

Composite solid propellants based on ammonium perchlorate/hydroxyl-terminated polybutadiene/isophorone dyisocyanate including two levels of hexogen (RDX) are presented in this paper. The mass of RDX increased in relation to oxidant, with constant bimodal fraction ratio. Combustion of the propellants...

Deskribapen osoa

Gorde:
Egile Nagusiak: Rodić Vesna, Bogosavljević Marica, Milojković Aleksandar, Mijatov Slavko
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: Military Technical Institute, Belgrade 2018-01-01
Saila:Scientific Technical Review
Gaiak:
composite solid propellant
ammonium perchlorate
hydroxyl-terminated polybutadiene
hexogen
titanium (iv)oxide
ballistic characteristics
thermochemical parameters
Sarrera elektronikoa:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2018/1820-02061802036R.pdf
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