Abstract

We developed advances laser retroreflectors for solar system exploration, geodesy and for precision test of General Relativity (GR) and new gravitational physics: a micro-reflector array (INRRI, Instrument for landing-Roving laser Retroreflectors Investigations), a midsize reflector array for the European Earth Observation (EO) program, Copernicus (CORA, COpernicus laser Retroreflector Array), a large, single-retroreflector (MoonLIGHT, Moon Laser Instrumentation for General relativity High accuracy Tests). These laser retroreflectors will be fully characterized at the SCF_Lab (Satellite/lunar/GNSS laser ranging/altimetry Cube/microsat Characterization Facilities Laboratory), a unique and dedicated infrastructure of INFN-LNF (www.lnf.infn.it/esperimenti/etrusco/). Our research program foresees several activities: 1) Developing and characterizing the mentioned laser retroreflector devices to determine landing accuracy, rover positioning during exploration and planetary/Moon’s surface georeferencing. These devices will be passive, laser wavelength- independent, long-lived reference point. INRRI will enable the performance of full-column measurement of trace species in the Mars atmosphere by future space-borne lidars. These measurements will be complementary to highly localized measurements made by gas sampling techniques on the Rover or by laser back-scattering lidar techniques on future orbiters and/or from the surface. INRRI will also support laser and quantum communications, carried out among future Mars Orbiters and Mars Rovers. This will be possible also because the INRRI laser retroreflectors will be metal back-coated and, therefore, will not change the photon polarization. The added value of INRRI is its low mass, compact size, zero maintenance and its usefulness for any future laser altimetry, ranging, communications, atmospheric lidar capable Mars orbiter, for virtually decades after the end of the Mars surface mission, like the Apollo and Lunokhod lunar laser retroreflectors. MoonLIGHT and INRRI are proposed for landings on the Moon (two Google Lunar X Prize Missions, namely Moon Express; Russia’s Luna-27 mission, as well as others under consideration/negotia- tion, also with the help of ASI, ESA and other partnerships); 2) Precision tests of GR with LLR to MoonLIGHT reflectors. Development of new fundamental gravity physics models and study of experimental constraints to these models use also laser ranging and laser reflectors throughout the solar system: extension of general relativity to include Spacetime Torsion, Non-Minimal Coupling between matter and curvature (so-called “ ” theories, or NMC gravity); 3) Extension of program to: Mars, Phobos and Deimos, Jupiter and Saturn icy/rocky moons, Near Earth Asteroids.

Highlights

  • The SCF_Lab (Satellite/lunar/GNSS laser ranging and altimetry and CubeSat/microsat Characterization Facility Laboratory) of INFN-LNF is designed to cover virtually LRAs (Laser Retroreflector Arrays) of CCRs (Cube Corner Retroreflectors) for missions in the whole solar system, with a modular organization of its instrumentation, two redundant SCF (SCF_Lab Characterization Facilities), and an evolutionary measurement approach, including customization and potentially upgrade on-demand.The SCF_Lab is dedicated to the characterization and modeling of the space segment of SLR (Satellite Laser Ranging [1]-[4]), LLR (Lunar Laser Ranging, [5]-[12]) and PLRA (Planetary Laser Ranging and Altimetry) for industrial and scientific applications

  • The SCF is very versatile for its large number of measurement ports, very long horizontal translations and capabilities for LLR and PLRA CCR payloads

  • Together with the SCF and SCF-G, we developed new industry-standard thermal-optical-vacuum tests to characterize and model the detailed optical performance and thermal behavior in representative space conditions (SCF-Test, background intellectual property of INFN)

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Summary

Introduction

The SCF_Lab (Satellite/lunar/GNSS laser ranging and altimetry and CubeSat/microsat Characterization Facility Laboratory) of INFN-LNF is designed to cover virtually LRAs (Laser Retroreflector Arrays) of CCRs (Cube Corner Retroreflectors) for missions in the whole solar system, with a modular organization of its instrumentation, two redundant SCF (SCF_Lab Characterization Facilities), and an evolutionary measurement approach, including customization and potentially upgrade on-demand (see http://www.lnf.infn.it/esperimenti/etrusco/ for a general description). We developed next-generation laser retroreflectors for: a flat, large LRA for satellite navigation, GRA (GNSS Retroreflector Array); a micro-reflector array for solar system exploration and geodesy, INRRI (Instrument for landing-Roving laser Retroreflectors Investigations); a midsize reflector array for Earth Observation (EO) and exploration, CORA (COpernicus laser Retroreflector Array); a single, large retroreflector fro LLR, MoonLIGHT (Moon Laser Instrumentation for General relativity High accuracy Tests) for the precision test of General Relativity (GR) [3] [5]-[12] and new gravitational physics [13]-[16] These are being designed, built and characterized at the SCF_Lab. We use LAGEOS (LAser GEO dynamics Satellite) and Apollo LRAs as reference payloads standards of the ILRS (International Laser Ranging Service; see http://ilrs.gsfc.nasa.gov). The thermal SCF-Test of a flat-shape 3 × 3 CCR matrix with LAGEOS/Apollo CCRs and mounting scheme, built by the SCF_Lab, is described in [3] and [4]

LLR and Gravitational Physics
MoonLIGHTs
LRA for Solar System Exploration and Geodesy
Earth Observation
National and International Framework
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