There are two common types of liquid propellant feeding system. They are pressure fed and pump system. It is important to properly design a feeding system inorder to ensure combustion stability. Which avoids the risk of engine operation catastrophic failure. We at Independence-X are looking at better options for a feeding system, in terms of cost and reliability. We are planning to design and construct a special feeding system for our Liquid Rocket Engine (LRE), by implementing a digital valve control system to help reduce the numbers of moving parts which will dramatically reduce its weight besides its unique mechanical design unlike conventional turbomachinery pumps. To date, turbopump has shown the best performance compared to pistonpump or pressure fed.