2012
DOI: 10.5028/jatm.2012.04032312
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An optimized hybrid rocket motor for the SARA platform reentry system

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Cited by 8 publications
(1 citation statement)
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“…Moreover, it allows multiple reignitions besides enhancing thrust-control insofar as the flow adjustment is also possible. This control also makes hybrid rocket motors applicable in space vehicles in which trajectory correction is also needed, such as in spacecraft reentry 3 . The HRM has already being envisaged for commercial ends viz.…”
Section: Introductionmentioning
confidence: 98%
“…Moreover, it allows multiple reignitions besides enhancing thrust-control insofar as the flow adjustment is also possible. This control also makes hybrid rocket motors applicable in space vehicles in which trajectory correction is also needed, such as in spacecraft reentry 3 . The HRM has already being envisaged for commercial ends viz.…”
Section: Introductionmentioning
confidence: 98%