“…MPFL with freon-11 was chosen for MPF's HRS due to its following attractive features. [Delil, 2004b]: 1) Ease of integration with the spacecraft, 2) No orientation constraints, 3) Control temperatures of remotely located components, 4) Modulate the system's temperature with changing environmental conditions and equipment power, 5) Versatile thermal control system for future missions (Smaller in size, cheaper, and lighter). Since then, MPFL has been used in various space exploration missions.…”