I'm trying to wrap my head around a conceptual problem involving a simple pendulum with a rocket attached to its mass. Imagine the rocket expels gas to provide a tangential thrust force. However, the thrust is calibrated such that it's not sufficient to swing the pendulum upward; instead, it only counteracts the gravitational pull, bringing the pendulum to a point of equilibrium (let's say, 45°) where the downward gravitational force equals the upward thrust.
Under ideal conditions, where we negate the effects of friction, air resistance, and other non-conservative forces, I can't seem to understand the conservation of energy in this system. The rocket's fuel conversion into kinetic energy of the expelled gases generates thrust that maintains this equilibrium. Yet, with the pendulum statically held in this equilibrium state:
Where does the energy imparted by the thrust go, considering the pendulum itself does not seem to gain kinetic or potential energy?