Abstract
The Pennsylvania State University has actively pursued hybrid rocket fuel regression rate and combustion research for 15 years. Initial work focused on developing and testing a high-pressure slab-burning hybrid motor with X-ray diagnostics for characterizing the local, real-time regression rates of hydroxyl terminated p olybutadiene (HTPB) with gaseous oxygen. Fuel decomposition and pyrolysis investiga tions were also carried out. Follow-on work is continuing to investigate high regression r ate hybrid fuels with various metal additives in center-perforated hybrid motors using both HTPB and paraffin binders. The addition of aluminum powders to paraffin-based solid-fuel formulations was shown to increase the regression rates by a factor of 4 comp ared to neat HTPB. This regression rate increase corresponds to a mass-burning rate increase ~7 times that of HTPB when the increase in fuel density is considered. This artic le reviews some of the more significant results from previous investigations and presents r ecent data from on-going test programs. Nomenclature
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
