A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Species in igniter gas</td><td class="align_center">Mass fraction</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">CO<sub>2</sub></td><td class="align_center">0.562687</td></tr><tr><td class="align_left">CO</td><td class="align_center">0.219515</td></tr><tr><td class="align_left">N<sub>2</sub></td><td class="align_center">0.189779</td></tr><tr><td class="align_left">SO<sub>2</sub></td><td class="align_center">0.028019</td></tr><tr><td class="align_left">O<sub>2</sub></td><td class="align_center">0</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Gas species and their fractions.</div>

International Journal of Aerospace Engineering

tab1

Table 1

Table 1: A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors 