| No. | Year | Author Name | Problems |
| 1 | 1995 | D. J. Vonderwell et al. | Optimization of Hybrid-Rocket-Booster Fuel-Grain Design |
| 2 | 1998 | P. L. Vergez | Tactical Missile Guidance with Passive Seekers Under High Off-Boresight Launch Conditions |
| 3 | 1998 | M. K. Hudson et al. | UV, visible, and infrared spectral emissions in hybrid rocket plumes |
| 4 | 2000 | A. M. Wright et al. | The effect of high concentration guanidinium azo-tetrazolate on thrust and specific impulse of a hybrid rocket |
| 5 | 2000 | R. Shanks et al. | A Labscale Hybrid Rocket Motor for Instrumentation Studies |
| 6 | 2001 | M. F. Desrochers et al. | A ground test rocket thrust measurement system |
| 7 | 2003 | M. A. Karabeyoglu et al. | Development of High-Burning-Rate Hybrid-Rocket-Fuel Flight Demonstrators |
| 8 | 2003 | A. Karabeyoglu et al. | Scale-up tests of high regression rate liquefying hybrid rocket fuels |
| 9 | 2004 | M. K. Hudson et al. | Guanidinium Azo-Tetrazolate (GAT) as a High Performance Hybrid Rocket Fuel Additive |
| 10 | 2004 | G. A. Risha et al. | Characterization of nano-sized particles for propulsion applications |
| 11 | 2005 | A. Karabeyoglu et al. | Design of an Orbital Hybrid Rocket Vehicle Launched from Canberra Air Platform |
| 12 | 2011 | D. B. Larson et al. | Characterization of the Performance of Paraffin/LiAlH4 Solid Fuels in a Hybrid Rocket System |
| 13 | 2013 | A. Sossi et al. | Combustion of HTPB-Based Solid Fuels Loaded with Coated Nanoaluminum |