1. Hydroxyl-terminated polybutadiene telechelic polymer (HTPB): binder for solid rocket propellants rubber;Ajaz;Chem. Technol.,1995
2. Hydroxyl-Terminated Polybutadiene-based polyurethane networks as solid propellant binder-state of the art;Sekkar;J. Propulsion power,2015
3. In hybrid rocket motors a gaseous oxidant (e.g. nitrous oxide) is driven over a solid fuel and the decomposition and combustion of the organic vapors produces propulsion. See: K.K. Kuo, M.J. Chiaverini, Application of glycidyl azide polymer to hybrid rocket motor, in: Fundamentals of Hybrid Rocket Combustion and Propulsion; American Institute of Aeronautics and Astronautics, Inc. Reston Va (2007).
4. Recent advances in hybrid propulsion;Cantwell;Int. J. Energetic Mater. Chem. Propuls.,2010
5. Theoretical analysis of hydrides in solid and hybrid rocket propulsion;Maggi;Int. J. Hydrogen Energy,2012