Monopropellant Hydrogen Peroxide Rocket Systems: Optimum for Small Scale
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[1] Matthew T. Keennon,et al. Development of the Black Widow Micro Air Vehicle , 2001 .
[2] D. Gibbon,et al. The use of Liquefied Gases in Small Satellite Propulsion Systems , 2001 .
[3] Eric Wernimont,et al. REVIEW OF HYDROGEN PEROXIDE MATERIAL SAFTY DATA SHEETS , 2002 .
[4] Sanford Gordon,et al. Computer program for calculation of complex chemical equilibrium compositions , 1972 .
[5] B. Reed,et al. Material Compatibility Testing with H AN-Based Monopropellants , 2001 .
[6] Phil L. Palmer,et al. Characterisation of a Monopropellant Microthruster Catalytic Bed , 2005 .
[7] Mark C. Ventura,et al. Long Term Storability of Hydrogen Peroxide , 2005 .
[8] Dennis Meinhardt,et al. Monopropellant selection criteria - Hydrazine and other options , 1999 .
[9] Eric J Wernimont. System Trade Parameter Comparison of Monopropellants: Hydrogen Peroxide vs Hydrazine and Others , 2006 .
[10] Dieter M. Zube,et al. Evaluation of HAN-Based Propellant Blends , 2003 .
[11] Wim De Groot. Propulsion Options for Primary Thrust and Attitude Control of Microspacecraft , 1999 .
[12] W S Cheung,et al. Hydrogen Peroxide Based Propulsion System for Micro Air Vehicle Applications , 1999 .
[13] Eckart Walter Schmidt,et al. Hydrazine and Its Derivatives: Preparation, Properties, Applications , 1984 .