Georeferencing Of Landers/Rovers, Test Of General Relativity, Metrics Of Lunar Interior With Laser Retroreflectors

Author: 
Simone Dell'Agnello
Abstract Title: 
Georeferencing Of Landers/Rovers, Test Of General Relativity, Metrics Of Lunar Interior With Laser Retroreflectors
Presentation PDF: 
Abstract Type: 
Oral
Abstract Body: 
Since 1969 Lunar Laser Ranging (LLR) to Apollo/Lunokhod laser retroreflector (CCR) arrays supplied accurate tests of General Relativity and new gravitational physics: possibile changes of the gravita-tional constant Gdot/G, weak and strong equivalence principle, gravitational self-energy (PPN parameter beta), geodetic precession, inverse-square force-law [1][2][3]; it cal also constraints gravitomagnetism. Some of these measurements also allowed for testing extensions of General Relativity, including spacetime torsion, non-minimally coupled gravity (that may ex-plain the gravitational universe without dark matter and dark energy)[4]; in principle, although technically and programmatically very challenging, also effective quantum gravity exploting the L1 lagrangian point. LLR has also provided, and will continue to provide, significant information on the composition of the deep interior of the Moon, complementary to the GRAIL mission of NASA. LLR first provided evidence of the existence of a fluid component of the deep lunar inte-rior, confirmed also by lunar seismometry data [1]. In 1969 CCR arrays contributed a negligible frac-tion of LLR error. Since laser stations improved by >100, now, because of lunar librations, current arrays dominate the error. We developed a next-generation single large CCR, MoonLIGHT-NGR (Moon Laser Instrumentation for General relativity high-acccuracy test - Next Generation Retroreflector) unaffected by librations that supports an improvement of the space segment of the LLR accuracy up to x100. INFN also developed INRRI (INstrument for landing-Roving laser Retroreflector Investigations), a microreflector to be laser-ranged by orbiters. MoonLIGHT/INRRI, cha-racterized at SCF-Lab [5] of INFN-LNF, Italy, for their deployment on the lunar surface or the cislunar space, will accurately position landers-rovers-hoppers-orbiters of GLXP/agency missions, thanks to LLR ob-servations from select ground station of the Internatio-nal Laser Ranging Service (like APOLLO in the USA, GRASSE in France and MLRO in Italy). INRRI was launched with the ESA ExoMars EDM 2016 mission, deployed on the Schiaparelli lander [6]. INRRI is also proposed for the ESA ExoMars 2020 Rover. Based on a NASA-ASI Implementing Arran-gement signed in July 2017, a similar INFN payload (LaRRI, Laser RetroReflector for InSight) has been delivered to JPL and integrated on the NASA InSight 2018 Mars Landers in August 2017. Following a sepa-rate NASA-ASI Implementing Arrangement (already signed by NASA) a microreflector (LaRA, Laser Re-troreflector Array) will be delivered by INFN to JPL in 2019 for deployment on the NASA Mars 2020 Rover. The first opportunities for the deployment of MoonLIGHT-NGR will be from early to late 2018 with commercial missions, followed by opportunities with space agency misions, including the proposed deployment of MoonLIGHT/INRRI on NASA’s Re-source Prospectors and its evolutions. LLR data analysis is carried out since the Apollo days with PEP, the Planetary Ephemeris Program de-veloped and maintained by CfA. New LLR data, will provide useful input to improve the lunar models that PEP needs [7], as already shown by the implementa-tion of data collected by GRAIL into LLR analysis. References: [1] Williams, J. G. et al., Adv. Space Res. 37(1), 67-71 (2006). [2] M. Martini, S. Dell’Agnello, in Springer DOI 10.1007/978-3-319-20224-2_5, R. Peron et al. (eds.) (2016). [3] D. Currie, S. Dell’Agnello, G. Delle Monache, B. Behr, J. Williams, Nucl. Phys. B (Proc Suppl) 243–244 (2013) 218–228. [4] N. Castel-Branco, J. Paramos, R. March, S. Dell’Agnello, in 3rd European Lunar Symposium, Frascati, Italy (2014). [5] S. Dell’Agnello et al., Adv. Space Res. 47, 822–842 (2011). [6] S. Dell’Agnello, et al., J. Adv. in Space Res., 9 (2017) 645–655. [7] R. Reseanberg et al., ar-Xiv:1608.04758v1.