Orbital Dynamics of a Simple Solar Photon Thruster

<table>Earth-Venus transfer control effort for SSPT for <svg height="14.0375" id="M78" style="vertical-align:-2.53308pt" version="1.1" viewbox="0 0 65.387497 14.0375" width="65.387497" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,14.0375)">
<g transform="translate(72,-60.77)">
<text transform="matrix(1,0,0,-1,-71.95,63.35)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝜒</tspan>
<tspan style="font-size: 12.50px; " x="12.027886" y="0">=</tspan>
<tspan style="font-size: 12.50px; " x="24.068275" y="0">0</tspan>
<tspan style="font-size: 12.50px; " x="30.319775" y="0">.</tspan>
<tspan style="font-size: 12.50px; " x="33.445526" y="0">1</tspan>
<tspan style="font-size: 12.50px; " x="39.697025" y="0">2</tspan>
<tspan style="font-size: 12.50px; " x="45.948524" y="0">5</tspan>
</text>
</g>
</g>
</svg>.</table>

Mathematical Problems in Engineering

Orbital Dynamics of a Simple Solar Photon Thruster

Figure 6