Multidisciplinary Design Optimization and Analysis of Hydrazine Monopropellant Propulsion System

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td align="left">Optimum pressure</td><td align="center">Optimum Isp</td><td align="center">Optimum bed-loading</td><td align="center">Minimum total mass</td><td align="center">Optimum propellant mass</td><td align="center">Optimum dry mass</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td align="left">10.15 bars</td><td align="center">215.7 sec</td><td align="center">0.38</td><td align="center">3.34 kg</td><td align="center">1.64 kg</td><td align="center">1.67 kg</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Results of multidisciplinary design of hydrazine propulsion system.

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Multidisciplinary Design Optimization and Analysis of Hydrazine Monopropellant Propulsion System 