| Review and evaluation of models for self-pressurizing propellant tank dynamics JE Zimmerman, BS Waxman, B Cantwell, G Zilliac 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 4045, 2013 | 37 | 2013 |
| Mass flow rate and isolation characteristics of injectors for use with self-pressurizing oxidizers in hybrid rockets BS Waxman, B Cantwell, G Zilliac, JE Zimmerman 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 3636, 2013 | 34 | 2013 |
| Peregrine hybrid rocket motor development G Zilliac, BS Waxman, AM Karabeyoglu, B Cantwell, BJ Evans 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3870, 2014 | 33 | 2014 |
| An Investigation of Injectors for Use with High Vapor Pressure Propellants with Applications to Hybrid Rockets BS Waxman Stanford University, 2014 | 24 | 2014 |
| Peregrine hybrid rocket motor ground test results G Zilliac, B Waxman, E Doran, J Dyer, A Karabeyoglu, B Cantwell 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4017, 2012 | 21 | 2012 |
| Effects of injector design on combustion stability in hybrid rockets using self-pressurizing oxidizers BS Waxman, JE Zimmerman, B Cantwell, G Zilliac 50th aiaa/asme/sae/asee joint propulsion conference, 3868, 2014 | 16 | 2014 |
| Paraffin and Nitrous Oxide Hybrid Rocket as a Mars Ascent Vehicle Demonstrator B Waxman, R Beckwith, F Tybor, J Zimmerman, A Stoll AIAA SPACE 2010 Conference & Exposition, 8840, 2010 | 12 | 2010 |
| Comparison of nitrous oxide and carbon dioxide with applications to self-pressurizing propellant tank expulsion dynamics JE Zimmerman, BS Waxman, BJ Cantwell, GG Zilliac Proc. 60th JANNAF Propulsion Meet, 2013 | 10 | 2013 |
| Effects of Injector Design and Impingement Techniques on the Atomization of Self-Pressurizing Oxidizers B Waxman, B Cantwell, G Zilliac 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3906, 2012 | 8 | 2012 |
| Slides for Use in Thesis Defense of Benjamin S. Waxman B Waxman, G Zilliac | | 2014 |
