Effects of Ti and Mg particles on combustion characteristics of boron–HTPB-based solid fuels for hybrid gas generator in ducted rocket applications

Author:

Hashim Syed Alay,Karmakar Srinibas,Roy Arnab

Funder

Indian Institute of Technology Kharagpur

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference60 articles.

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2. Hybrid propellants gas generator;Russo Sorge,1999

3. Study of a hybrid gas generator for a ducted rocket;Komornik;Combust. Explos. Shock Waves,2017

4. Combustion of energetic fuel for ducted rockets (I);Kubota;Propellants, Explos. Pyrotech.,1991

5. Boron particle combustion in solid rocket ramjets;Liu;J. Aerosp. Eng.,2014

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