Awesome!.

The manned rockets mission is to orbit earth once. Then land back where it took off. Another function of rocket engine. Is when the coil heats both LQ-Hydrogen and LQ-Oxygen They bounce around then eventually bounce away from the heated electric super conducting thermal nucleo reactive coils. Which bounce and turn into burned energy. Due to the molecules natural flammability and volitility. When fuel quantities are in higher volumes. MxE equals thrust. But lower volumes of fuel. Increase specific impulses. (I wonder if I got that little equation correctly?)

the rocket engine*

Luckily they have an aneutronic plasma fusion reactor on board. In order to power the super heat conductive coils. It is also very small and practical. Because this thing hogs somewhere around twenty megawatts or higher. Depending on how much power the coil receives will effectively use significantly less fuel and have higher specific impulses whilst increasing killa newtons. And may burn a clean hole in the launch pad. The aneutronic fusion reactor isn't powerful enough to generate that much energy. Normally it would be used on its own as an engine. Or be used to enhance longer burn periods for ion engines. Meaning the energy capacity won't drain. But the fuel will. Xenon would be used in an Ion engine. They are also efficient but very slow. Again higher specific impulses then killa newtons.

And has high gimbal ratio's.