The CH4, H2+O2, and RP1+O2 RCS thrusters all use oxygen gas instead of LqdOxygen as a resource; this appears to be inconsistent with the scientific papers linked in the documentation, which describe liquid-propellant RCS.
The papers linked in the documentation all use gaseous oxygen propellants, other than the CH4 thruster. Gaseous oxygen propellant was chosen for all variants for consistency.
The CH4, H2+O2, and RP1+O2 RCS thrusters all use oxygen gas instead of LqdOxygen as a resource; this appears to be inconsistent with the scientific papers linked in the documentation, which describe liquid-propellant RCS.