Lunette: A Two-Lander Discovery-Class Geophysics Mission to the Moon

Abstract

The document “The Scientific Context for the Exploration of the Moon” [1] designated understanding the structure and composition of the lunar interior (to provide fundamental information on the evolution of a differentiated planetary body) as the second highest priority lunar science concept that needed to be addressed. To this end, the Science Mission Directorate formulated the International Lunar Network (ILN) mission concept (web site) that enlisted international partners to enable the establishment of a geophysical network on the lunar surface. NASA would establish the first four “anchor nodes” in the 2018 time frame. These nodes are envisioned to use radioisotope power systems to allow operation of each node for at least 6 years. Each anchor node will contain a seismometer, magnetometer, laser retroreflector, and a heat flow probe [2] and will be distributed across the lunar surface to form a much more widespread network that the Apollo passive seismic, magnetometer, heat flow, and the Apollo and Luna laser retroreflector networks. (Fig. 1). It is planned that the four anchor nodes will be launched on an Atlas 5 launch vehicle and the cost is estimated to exceed that for a New Frontiers mission. What we present here is an alternative to the ILN architecture that will still return the data required to understand the nature of the lunar interior and determine how the Moon evolved.