A Manifest of Delivery Missions to Make the Moon Accessible to the World

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A Manifest of Delivery Missions to Make the Moon Accessible to the World FISO Telecon July 15, 2020 Dan Hendrickson, Vice President of Business Development Astrobotic Technology, Inc. July 2020 1 WHY THE MOON Research FUEL DEPOTS EXPLORATION & RESEARCH MINING LIVING OFF THE LAND MANUFACTURING MULTI-PLANET SPECIES 2 ASTROBOTIC PROGRAMS End to End Delivery Services LANDERS ROVERS Peregrine CubeRover Surface payload: 100 kg Surface payload: 5 kg Griffin Polaris Surface payload: 500 kg Surface payload: 90 kg 3 3 ASTROBOTIC PROGRAMS Future Missions and Technology Precision Landing Autonomous Nav 100m precision terrain High-rate, lighting-robust relative nav nav for autonomous ops Mission Simulation Space Computing Render sim for landing Software defined reliability & surface ops for space 4 44 ASTROBOTIC MANIFEST MISSION ONE PEREGRINE 2021 LANDING SITE: LACUS MORTIS 16 customers $79.5M from 6 countries NASA award 5 ASTROBOTIC MANIFEST MISSION TWO MOONRANGER 2022 LANDING SITE: SOUTH POLE Testing autonomy $5.5M on the Moon NASA award 6 ASTROBOTIC MANIFEST MISSION THREE GRIFFIN 2023 LANDING SITE: SOUTH POLE Carrying the $199.5 million NASA VIPER NASA award rover 7 PEREGRINE MISSION ONE DHL PULI TOMMOROW DYMON AEM ASTROSCALE ATLAS ELYSIUM LM1 SPACEBIT MOONARTS DHL MOONBOX ARCH FOUNDATION CANADENSYS CARNEGIE MELLON . ASTROBOTIC NASA 8 8 PEREGRINE UPDATE 60 HOT FIRE TESTS NEW HEADQUARTERS 9 STRUCTURAL TEST MODEL PAYLOAD SIMULATORS LUNAR LOGISTICS HQ Opening in Summer 2020 10 10 LAUNCH VEHICLE SIGNED Contract for Vulcan-Centaur signed with ULA in Aug 2019 11 11 PEREGRINE LANDER One Lander, Any Mission High Reliability, Low Complexity Moon-tested in 2021 12 PEREGRINE LANDER One Lander, Any Mission High Reliability, Low Complexity Moon-tested in 2021 13 SURFACE SERVICE Surface Ops: 8 to 12 Earth Days Comm: 10 kbps per kg Power: 1.0 W per kg Area: 0.5 m2 per deck surface (top & bottom) $1.2 Million / kg to the lunar surface 14 ORBIT SERVICE Astrobotic landers can deliver payloads to lunar orbit as well as the lunar surface. While the trajectory can change from mission to mission, landers typically hold in three distinct Lunar $300k per kg to Orbits (LO’s), and two are available for payload lunar orbit deployment, LO1 and LO2. 15 ROVER SERVICE CubeRovers offer 2 kg of payload capacity within a 4 kg rover Localized Precision: 0.06 mm per meter $4.5M per kg for Nominal Speed: 4 cm/s surface mobility Camera: Front and rear view, 16 megapixel 16 PREPARING YOUR PAYLOAD üCheck your Payload for Compatibility: Payload User’s Guide üDesign with Confidence: Interface Design Document üIntegrate with Peregrine: Use our Peregrine Deck CAD File üGet Personalized Service: Utilize Your Astrobotic Payload Manager 17 17 18.

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Estimation of Lunar Surface Dielectric Constant Using Minirf SAR Data
Estimation of lunar surface dielectric constant using MiniRF SAR data Nidhi Verma, Student Member, IEEE, Pooja Mishra, Member, IEEE, Neetesh Purohit, Member IEEE Abstract—A new model has been developed to estimate dielec- 12), 14163 (Apollo 14), 66041 (Apollo 16) are regolith sam- tric constant () of the lunar surface using Synthetic Aperture ples [15], [16]. Dielectric results from laboratory experiments Radar (SAR) data. Continuous investigation on the dielectric revealed the nature of lunar regolith. Another method in 1998 constant of the lunar surface is a high priority task due to future lunar mission’s goals and possible exploration of human outposts. was given by Chyba et al. in terms of energy loss during For this purpose, derived anisotropy and backscattering coefﬁ- propagation in an absorbing medium [17]. Alan et al. [10] cients of SAR images are used. The SAR images are obtained and Pollack et al. [16] analyzed the relationship between the from Miniature Radio Frequency (MiniRF) radar onboard Lunar dielectric constant and density of large regions using radar Reconnaissance Orbiter (LRO). These images are available in echoes. Campbell gave the formula for estimation of dielectric the form of Stokes parameters, which are used to derive the co- herency matrix. Derived coherency matrix is further represented constant in terms of radar backscattering coefﬁcients. Avik et in terms of particle anisotropy. This coherency matrix’s elements al. [8] gave another method of dielectric constant estimation. compared with Cloud’s coherency matrix, which results in the Hagfor’s observations show a dielectric constant of 2.7 for the new relationship between particle anisotropy and coherency less dense upper regolith [18].
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Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no.
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