A cubesat Microfluidic Electrospray Propulsion (MEP) system module prototype will be designed, built and demonstrated. This system is under development to deliver >1000 m/s of delta-V to a three unit cubesat with less than 80 grams of solid indium propellant. It will include 4 prototype MEP thrusters and a power processing unit with a dry mass less than 100 grams.
The Cubesat Microfluidic Electrospray Propulsion (MEP) system module prototype will be designed, built and tested to demonstrate that a four MEP thruster system can be integrated into a single module on a cubesat electronic board. The MEP thruster is shown in Figure 1. It is an electrospray thruster with microfabricated components, a highly integrated capillary force driven feed system and indium propellant that is stored as a solid metal in the thruster head. It has no valves or pressurized reservoirs. Four of these thrusters will plug into one side of the cubesat board with the Power processing Unit (PPU) on the opposite side. The PPU will consist of COTS components. It will be designed to operate four 100 micronewton MEP thrusters. Existing lower thrust prototype MEP thrusters will be demonstrated in the module. The performance of the system will be characterized and control of the module will be demonstrated in a vacuum environment.More »
|Organizations Performing Work||Role||Type||Location|
|Jet Propulsion Laboratory (JPL)||Lead Organization||NASA Center||Pasadena, California|