论文信息 - Hybrid rocket upper stage optimization: effects of grain geometry - 字舞流文

Hybrid rocket upper stage optimization: effects of grain geometry

Lorenzo Casalino | Lorenzo Casalino | Dario Giuseppe Pastrone | Francesco Simeoni

[1] Lorenzo Casalino,et al. Optimal Design of Hybrid Rocket Motors for Microgravity Platform , 2008 .

[2] Lorenzo Casalino,et al. Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages , 2008 .

[3] Lorenzo Casalino,et al. Optimal Low-Thrust Escape Trajectories Using Gravity Assist , 1999 .

[4] Terry Abel,et al. Development and testing of a peroxide hybrid upper stage propulsion system , 2001 .

[5] Lorenzo Casalino,et al. Integrated Design of Hybrid Rocket Upper Stage and Launcher Trajectory , 2009 .

[6] Lorenzo Casalino,et al. Optimal Design and Control of Hybrid Rockets for Access to Space , 2005 .

[7] D. J. Vonderwell,et al. Optimization of hybrid-rocket-booster fuel-grain design , 1995 .

[8] Lorenzo Casalino,et al. Optimization of Hybrid Sounding Rockets for Hypersonic Testing , 2012 .

[9] Lorenzo Casalino,et al. Oxidizer Control and Optimal Design of Hybrid Rockets for Small Satellites , 2005 .

[10] Jim Benson,et al. Safe and Affordable Human Access to LEO , 2005 .

[11] H. Seifert,et al. Rocket Propulsion Elements , 1963 .

[12] Stephen D. Heister,et al. Combustion Experiments in Hydrogen Peroxide/Polyethylene Hybrid Rocket with Catalytic Ignition , 2000 .

[13] Lorenzo Casalino,et al. Optimization of a Hybrid Rocket Upper Stage with Electric Pump Feed System , 2010 .