B. Florczak

发表

Investigation of an Aluminized Binder/AP Composite Propellant Containing FOX-7

B. Florczak, 2008 .

A Comparison of Properties of Aluminized Composite Propellants Containing HMX and FOX-7

B. Florczak, 2008 .

TESTING THE PROPERTIES OF HETEROGENEOUS SOLID ROCKET PROPELLANTS BASED ON HTPB RUBBER

B. Florczak, Rafał Bogusz, Tomasz Sałaciński, 2016 .

The composite propellants with high-burning rate and low-pressure exponent

B. Florczak, J. Szymczak, M. Lipiński, 2003 .

Determination of Glass Transition Temperature of Double-Base Rocket Propellants with the Use of Dynamic Mechanical Analysis

M. Miszczak, J. Zmywaczyk, P. Koniorczyk, 2015 .

Investigation of Selected Ingredients of Composite Propellants Using DTA, SEM and Calorimetric Techniques

M. Szala, B. Florczak, A. Maranda, 2015 .

Studies of the Influence of Nano Iron(III) Oxide on Selected Properties of Solid Heterogeneous Propellants Based on HTPB

B. Florczak, A. Maranda, K. Drożdżewska, 2016 .

Theoretical thermodynamic combustion properties of composite propellants

B. Florczak, 2009 .

Viscosity Testing of HTPB Rubber Based Pre-binders

B. Florczak, 2014 .