Experimental investigation of fuel regression rate in a HTPB based lab-scale hybrid rocket motor

Turbulent boundary layer combustion in the hybrid rocket

G. A. Marxman, Mitchell Gilbert · Symposium (International) on Combustion · 1963 · 253 citations

Engineering, Aerospace Engineering, Combustion Science +4

Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene/Gaseous-Oxygen Hybrid Rocket Motors

Philmon George, S. Krishnan, P. M. Varkey et al. · Journal of Propulsion and Power · 2001 · 144 citations

Engineering, Profile Modification, Mechanical Engineering +16

Investigation of Metallized and Nonmetallized Hydroxyl Terminated Polybutadiene/Hydrogen Peroxide Hybrid Rockets

Erin Farbar, J. Louwers, Tarik Kaya · Journal of Propulsion and Power · 2007 · 63 citations · Full text

Engineering, Profile Modification, Fluid Mechanics +21

Fundamentals of hybrid boundary layer combustion

G. A. Marxman, R. J. MUZZY, C. E. Wooldridge · Heterogeneous Combustion Conference · 1963 · 63 citations

Combustion Science, Combustion Theory, Engineering +1

Numerical analysis of fuel regression rate distribution characteristics in hybrid rocket motors with different fuel types

XinTian Li, Hui Tian, Guobiao Cai · Science China Technological Sciences · 2013 · 52 citations

Numerical Analysis, Engineering, Different Fuel Types +7