Thermo-analytical study of 2,2,2-trinitroethyl-formate as a new oxidizer and its propellant based on a GAP matrix in comparison with ammonium dinitramide

Author:

Abd-Elghany MohamedORCID,Elbeih Ahmed,Klapötke Thomas M.

Funder

Ludwig-Maximilian University of Munich

Office of Naval Research

Bundeswehr – Wehrtechnische Dienststelle für Waffen und Munition

Publisher

Elsevier BV

Subject

Analytical Chemistry,Fuel Technology

Reference51 articles.

1. Recent advances in new oxidizers for solid rocket propulsion;Trache;Green Chem.,2017

2. Chemical Rocket Propulsion;DeLuca,2017

3. Chemical Rocket Propulsion;Singh,2017

4. The influence of porosity of ammonium perchlorate (AP) on the thermomechanical and thermal properties of the AP/polyvinylchloride (PVC) composite propellants;Mezroua;J. Therm. Anal. Calorim.,2014

5. Thermal behavior and decomposition kinetics of composite solid propellants in the presence of amide burning rate suppressants;Trache;J. Therm. Anal. Calorim.,2018

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