The capsule had 2 main thruster types, the main thruster which is used to control the descent, and the 4 sets of maneuvering thrusters which are used to orient the capsule in 3D space. Since the simulation was simplified to 2D this resulted in 3 total thrusters, the main thruster as well as 2 sets of maneuvering thrusters. Mathematically the main thruster worked solely in the +y direction of the reference frame, while the maneuvering thrusters rotated the reference frame, simulating the rotation of the space craft. To simplify the rotational dynamics I treated the entire capsule as a point mass and the thrusters as applying a constant moment. In addition, I was able to obtain and implement the mass flow rate of the thrusters, so as the thrusters were fired the total mass of the spacecraft would decrease, this will be covered in more depth a little later. I simplified the fuel storage by having all the fuel shared between the thrusters, realistically each thruster group had its own fuel tank, however this does not impact the overall dynamics of the system, and thus could be omitted.