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A. Colaprete1, R. Elphic, J. Sanders2, J. Quinn3, B. Larson1, M. Picard4, D. Andrews1, B

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A. Colaprete1, R. Elphic, J. Sanders2, J. Quinn3, B. Larson1, M. Picard4, D. Andrews1, B A. Colaprete1, R. Elphic, J. Sanders2, J. Quinn3, B. Larson1, M. Picard4, D. Andrews1, B. Bussey5 1NASA Ames Research Center, MoffeH Field, CA [email protected] 2NASA Johnson Space Center, Houston TX 3NASA Kennedy Space Center, Cape Canaveral, FL 4Canadian Space Agency, Saint-Hubert QC 5JHU Applied Physics Laboratory, Laurel MD LEAG 10/15/2013 Resource Prospector – Water, water everywhere… A range of forms, distribuXons and concentraons ~0.1-1% ~1-10% ~10-100% 23-30 sec 1.3 Data Model Fit Residual Error H2O(s) H2O(g) OH 1.2 SO2 CH3OH C2H4 O2 CH4 BB (500K) 1.1 1 Brightness 0.9 0.8 0.7 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2 2.1 2.2 2.3 Wavelength (µm) Pieters et al., 2003 Colaprete et al., 2010 Spudis et al., 2010 We know the water (and other H-bearing compounds) are there… Resource Prospector – But exactly where? …and at what concentraons? Forms? • LCROSS + Neutron analysis suggest patchy or buried (or both) distribuXons of hydrogen • Impact gardening will create heterogeneity at lengths scale of ~10-100 m • Several data sets suggest Xme-dependent surface component • In areas of limited sun near sub-surface temperatures are cold enough to retain water Resource Prospector Mission “Big Picture” The Resource Prospector Mission elements include a lunar Mission (RPM) is being jointly lander, a rover, a sampling & developed by NASA and the Canadian Space Agency to analysis payload, and mission prospect for volatiles (water ice) operaons. in the polar regions of the Moon. Utilizing lunar resources to Payload consists of a drill, a small produce oxygen and propellants oven to heat the sample, and a could enable new mission suite of three different architectures for human spectrometers to guide surface exploration. navigaon and characterize the RPM is targeted for launch in volales located in the lunar 2018. regolith. Doc# RPM-PLAN-0006A 4 RPM Mission Goals From LEAG Robo)c Campaign Analysis (2011): Phase I: Lunar Resource Prospec?ng • Defining the composiXon, form, and extent of the resource; • Characterizing the environment in which the resources are found; • Defining the accessibility/extractability of the resources; • QuanXfying the geotechnical properXes of the lunar regolith in the areas where resources are found; • Being able to traverse several kilometers and sample and determine lateral and verXcal distribuXon on meter scales; • IdenXfying resource-rich sites for targeXng future missions Resource Prospector is aligned with the community vision for the next lunar resource mission SKGs and RPM – Address at Least 22 Lunar SKGs RPM Lunar Exploration Strategic Knowledge Gaps Instrument or Activity Relevance I. Understand the Lunar Resource Potential B-1 Regollith 2: Quality/quanity/distribution/form of H species and other volatiles in mare and highlands NSS, NIRVSS, OVEN-LAVA VH D-3 Geotechnicalmaterial characteristics of cold traps NIRVSS, Drill, Rover H D-4 Physiography and accessibility of cold traps Rover-PSR traverses, Drill, Cameras VH D-6 Earth visibility timing and extent Mission Planning VH D-7 Concentration of water and other volatiles species within depth of 1-2 m NSS, NIRVSS, OVEN-LAVA VH D-8 Variability of water concentration on scales of 10's of meters NSS, NIRVSS, OVEN-LAVA VH VH- Volatiles D-9 Mineralogical, elemental, molecular, isotopic, make up of volatiles NIRVSS, OVEN-LAVA L-M-Minerals D-10 Physical nature of volatile species (e.g. pure concentrations, intergranular, globular) NIRVSS, OVEN-LAVA H D-11 Spatial and temporal distribution of OH and H2O at high latitudes NIRVSS, OVEN-LAVA M-H D-13 Monitor and model movement towards and retenion in PSR NIRVSS, OVEN-LAVA M G Lunar ISRU production efficiency 2 Drill, OVEN-ROE, LAVA-WDD M III. Understand how to work and live on the lunar surface A-1 Technology for excavation of lunar resources Drill, Rover M B-2 Lunar Topography Data Planning Products, Cameras M B-3 Autonomous surface navigation Traverse Planning, Rover M-L C-1 Lunar surface trafficability: Modeling & Earth Tests Planning, Earth Testing M C-2 Lunar surface trafficability: In-situ measurements Rover, Drill H D-1 Lunar dust remediation Rover, NIRVSS, OVEN M D-2 Regolith adhesion to human systems and associated mechanical degradation Rover, NIRVSS, OVEN, Cameras M D-3 Descent/ascent engine blast ejecta velocity, departure angle, and entrainment mechanism: Modeling Landing Site Planning, Testing M D-4 Descent/ascent engine blast ejecta velocity, departure angle, and entrainment mechanism Lander, Rover, NIRVSS H F-2 Energy Storage - Polar missions Stretch Goal: Lander, Rover H F-4 Power Generation - Polar missions Rover M VH = Very High, H = High, M = Medium, L = Low Resource Prospector – A Prospector & ISRU Mission A mission to examine polar for the distribution and potential for ISRU Prospec?ng Mission: Ø Characterize the distribuXon of water and other volales at the lunar poles • Map the surface and subsurface distribuXon of hydrogen rich materials • Determine the consXtuents and quanXXes of the volales extracted - QuanXfy important volales: H2, He, CO, CO2, CH4, H2O, N2, NH3, H2S, SO2 • Measure or provide limits on key isotope raos, including D/H, O18/O16, S36/ S34, C13/C12 ISRU Processing Demonstra?on Mission: Ø ExtracXon and capture of nave water • Measure of energy required to extract water (and any other volales) from samples Ø Demonstrate the Hydrogen ReducXon process to extract oxygen from lunar regolith • Demonstrate the hardware (e.g., oven, seals, valves) in lunar seng • Capture, quanXfy, and display the water generated Simplified view of Resource Prospector Mission Get there… Launch Find & Mine Volatiles… Cruise Use the Neutron Spec & Map Near-IR Spec to look for Descent & surface Hydrogen-rich materials Utilize the volatiles… Landing Quick Extract Use the Drill Subsystem to Heat sample to reaction excavate up to 1[m] core Super- temps (150-900degC) using Checkout soil core sample heat soil the OVEN Subsystem Roll-off Flow H through the heated Lander 2 Heat samples (150degC) Make soil to capture oxygen and Heat soil in the OVEN Subsystem water make water using the OVEN Quick Subsystem Checkout Determine type and Begin Determine Show Image and quantify the Surface quantity of volatiles in the me the water created using the Volatiles LAVA Subsystem, (H2, He, LAVA Subsystem Ops CO, CO2, CH4, H2O, N2, water! NH3, H2S, SO2) Doc# RPM-PLAN-0006A 8 Geng there… • Cruise Phase: – 5-day direct Earth to Moon transfer w/DSN S-band – Spin up to 1 rpm using Atude Control System (post-TLI) • No de-spin during TCMs – Perform system checkout Moon Arrival – Perform two TCMs (nom.) (Direct Descent) – Perform two Neutron Spec calibraons (nom.) Neutron • ConXngency / Off nominal Spectrometer – Allows for two (2) addiXonal TCMs Calibraon 2 – Propellant margin for spin / de-spin for thermal anomalies TCM Earth Departure Neutron System Spectrometer Checkout Calibraon 1 TLI TCM Landing there… Cruise Descent & Landing Landed Surface Operaons Payload/rover powered on during descent Landing images TCMs w/Spin stabilized captured during Rover DTE atude perpendicular descent comm. during to Sun surface ops IniXal AlXtude: 16.6 km DTE Comm via omni IniXal Velocity: 2.5 km/s antenna Payload & rover checkout + NS cal, During cruise, comm link IniXal AlXtude: 3 km prior to release & is used for payload IniXal Velocity: 0.105 km/s roll-off of rover. calibraon & bake-out operaons Assume power up post separaon (aer shroud jeson) Touchdown Velocity: <.001 km/s Lander power down upon landing Resource Prospector – The Tool Box Mobility Prospecting Processing & Analysis Rover Neutron Spectrometer System • Mobility system • Cameras (NSS) • Surface interaction • Water-equivalent hydrogen > 0.5 Oxygen & Volatile Extraction wt% down to 1 meter depth Node (OVEN) NIR Volatiles Spectrometer • Volatile Content/Oxygen System (NIRVSS) Extraction by warming • Total sample mass • Surface H2O/OH identification • Near-subsurface sample characterization Lunar Advanced Volatile • Drill site imaging Analysis (LAVA) • Drill site temperatures • Analytical volatile identification and quantification in delivered sample with GC/MS • Measure water content of regolith at 0.5% (weight) or Sampling greater • Characterize volatiles of Auger / Core Drill interest below 70 AMU • Subsurface sample acquisition • Auger for near-surface assay • Core for detailed subsurface assay Prospecng… 1. While roving, prospecting instruments search for enhanced surface H2O/OH, other volatiles and volumetric hydrogen Doc# RPM-PLAN-0006A 12 Prospecng… 1. While roving, prospecting instruments search for enhanced surface H2O/OH and volumetric hydrogen 2. When enhancements are found decision made to either auger or core (sample) Doc# RPM-PLAN-0006A 13 Excavang… 1. While roving, prospecting instruments search for enhanced surface H2O/OH and volumetric hydrogen 2. When enhancements are found decision made to either auger or core (sample) 3. Samples are processed and evolved volatiles measured Doc# RPM-PLAN-0006A 14 Mapping… Mapping of volatiles and samples continues across a variety environments, testing theories of emplacement and retention, and constraining economics of extraction. Doc# RPM-PLAN-0006A 15 Demonstrang… Concluding the primary mission, oxygen extraction from regolith with be demonstrated using hydrogen reduction, thus testing both possible ISRU pathways: local volatiles and water production from “dry” regolith. Doc# RPM-PLAN-0006A 16 Resource Prospector – Landing Site Where to go? Site Selection Criteria § Likely subsurface volales – Sustained low subsurface temperatures
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