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The Laser Ranging Interferometer (LRI) technology demonstrator on-board the Gravity Recovery and Climate Experiment Follow-On (GRACE-FO) mission has proved an unmatched sub-nanometer per square root of Hertz ranging performance above 100 mHz surpassing the noise floor of the until then state-of-the-art K/Ka-band ranging instrument by orders of magnitude. The LRIs reliability and its outstanding performance have led to the decision of implementing LRI-like systems as primary instruments for the measurement of the intersatellite range in all currently planned NASA, DLR and ESA Earth gravity missions.Interferometric laser ranging has proven to be an indispensable technique for the long-term monitoring of Earths gravitational field and its spatial and temporal variations, enabling in-depth analyses of many Essential Climate Variables (ECVs). We propose to bring this proven technology to an application in a constellation of satellites dedicated to Mars gravity research as outlined in the paper titled MaQuIsConcept for a Mars Quantum Gravity Mission.In this talk we will give an overview of the architecture of the LRI as it is currently flying on GRACE-FO as well as the measurement principle and its consequences for the overall mission design. Additionally, we are going to highlight a few of the following development activities, which could be applied for a mission around Mars: enhancement of the long-term stability of the laser frequency, improved redundancy schemes as well as a novel sensor type for the acquisition and maintenance of the constellation. Progress with respect to these aspects will yield a next generation of intersatellite laser interferometers with improved performance and enhanced reliability.
Koch et al. (Mon,) studied this question.