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- W289383315 abstract "Theoretical thrust equations for the diverse nozzle expansion condition were derived. By using the obtained thrust equations, parametric studies were carried out to estimate the effect of pressure exponent, minimum operation pressure, ambient pressure and extinguishment pressure on thrust modulation performance in pintle-nozzle solid rocket motors. Analysis results showed that thrust turndown ratio can be easily attained by small nozzle-throat area variation at high pressure exponent, low minimum operation pressure, high ambient pressure and high extinguishment pressure condition. At those conditions, the highest chamber pressure to obtain the intended thrust turndown ratio can be minimized." @default.
- W289383315 created "2016-06-24" @default.
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- W289383315 date "2009-04-01" @default.
- W289383315 modified "2023-09-29" @default.
- W289383315 title "Thrust modulation performance analysis of pintle-nozzle motor" @default.
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- W289383315 doi "https://doi.org/10.5139/jksas.2009.37.4.392" @default.
- W289383315 hasPublicationYear "2009" @default.
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