Chip based MEMS Ion Thruster to significantly enhance Cold Gas Thruster Lifetime for LISA

11th International LISA Symposium

Tajmar, M.^1 ; Laufer, P.^1 ; Bock, D.^1

Institute of Aerospace Engineering, Technische Universitat Dresden, Germany^1

关键词: Cold-gas thrusters;    LISA Pathfinder;    Micro propulsion;    Micro thruster;    Mission duration;    Operating principles;    Specific impulse;    Thruster system;   

Others  :  https://iopscience.iop.org/article/10.1088/1742-6596/840/1/012012/pdf
DOI  :  10.1088/1742-6596/840/1/012012

来源: IOP

【 摘 要 】

Micropropulsion is a key component for ultraprecise attitude and orbit control required by the eLISA mission. LISA pathfinder uses cold gas micro thrusters that are accurate but require large tanks due to their very low specific impulse, which in turn limits the possible mission duration of the follow up eLISA mission. Recently, we developed a compact MEMS ion thruster on the chip with a size of only 1cm2that can be simply attached to a gas feeding line like the one used for cold gas thrusters. It provides a specific impulse greater than 1000 s and only requires a single DC voltage. Since the operating principle is based on field emission, very low thrust noises similar to FEEP thrusters are expected but with gas propellants. The MEMS ion thruster chip could be mounted in parallel to the existing gold gas system providing high Isp and therefore long mission durations while leaving the cold gas system in place. To enable a possible mission extension, the MEMS ion thruster could take over from the cold gas system as a backup while maintaining the existing micropropulsion thruster system with its heritage therefore minimum risk.