Dynamic Characteristics of LOX/Kerosene Variable Thrust Liquid Rocket Engine Test System Based on General Modular Simulation Method

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Parameters</td><td class="align_center">LOX</td><td class="align_center">Kerosene</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Piston diameter (mm)</td><td class="align_center">40</td><td class="align_center">26</td></tr><tr><td class="align_left">Number of pistons</td><td class="align_center">3</td><td class="align_center">9</td></tr><tr><td class="align_left">Piston clearance (mm)</td><td class="align_center">0.065</td><td class="align_center">0.035</td></tr><tr><td class="align_left">Piston eccentricity</td><td class="align_center">0</td><td class="align_center">0</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Partial model parameters for pump simulation.</div>

International Journal of Aerospace Engineering

tab6

Table 6

Table 6: Dynamic Characteristics of LOX/Kerosene Variable Thrust Liquid Rocket Engine Test System Based on General Modular Simulation Method 