Described is a method of thrust modulation of a solid propellant rocket motor. The method involves the injection of monatomic gases, helium and organ, into the combustion chamber, which modifies the flame structure over the grain surface and, consequently, changes the burning rate, thus modifying the thrust.
Modulacao Do Empuxo de Motor Foguete a Propelente Solido (Thrust Modulation of a Solid Propellant Rocket Engine)
1987
85 pages
Report
Keine Angabe
Englisch
Electrically operated propellant for solid rocket motor thrust management
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