National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate.

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Presentation transcript:

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate Mars Exploration Program Analysis Group “MEPAG” Dr. Fuk Li June 16, 2011

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" MEP Overview MRO Mars Express Collaboration Mars Express Collaboration Odyssey MER Operational Phoenix (completed) Phoenix (completed) Mars Science Laboratory MAVEN Aeronomy Orbiter "For Planning and Discussion Purposes Only" & Beyond ESA—NASA ExoMars Trace Gas Orbiter ESA—NASA ExoMars Trace Gas Orbiter NASA/ESA Joint Rover (Exobiology/ Sample Return Cache) NASA/ESA Joint Rover (Exobiology/ Sample Return Cache) NASA-ESA Joint Mars Initiative ESA—EDL Demonstrator 2 All pictures are Artist Conceptions

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" MEP Operation Missions ODY –4 th extended mission on-going –Spacecraft is healthy –THEMIS continues to obtain thermal infrared imagery superior to previous phases of mission; Neutron Spectrometer and HEND still accumulating data on subsurface –Primary relay function for MER –Preparing for support to MSL: EDL coverage and data relay MER –Spirit recovery effort concluded in late May –Opportunity is roving towards the Endeavour crater ~3 km away Had roved ~30 km MRO –1 st extended mission/preparing for MSL relay phase –Spacecraft is healthy –Science payload continues to generate high resolution imagery, hyperspectral information, global and atmospheric monitoring and shallow subsurface radar imaging –Provides critical data for landing site characterization for MSL and other landing missions 3

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" Technical Capabilities Category 1 Risk Class B One Mars Year surface operational lifetime (669 sols/687 days) Discovery Responsive over wide range of latitudes and altitudes Precision Landing via Guided Entry Skycrane Propulsive Landing Long Distance Traverse Capability (20 km) Flexible & Robust Sample Acquisition & Processing Science Focus on Past & Present Habitability of Mars Highly Capable Analytical Laboratory Next Generation Remote Sensing & Contact Investigations Suite of Environmental Monitoring Instruments MSL Project Overview 4 * Artist Conception *

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" MSL in ATLO Process 5

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" Cruise Stage STV Rover System Thermal Testing Rover EMI/EMC Testing Rover Random Vibe MSL Environmental Testing 6

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" MSL Candidate Landing Sites Eberswalde Crater (24°S, 327°E, -1.5 km) contains a clay-bearing delta formed when an ancient river deposited sediment, possibly into a lake. Gale Crater (4.5°S, 137°E, -4.5 km) contains a 5-km sequence of layers that vary from clay-rich materials near the bottom to sulfates at higher elevation. Mawrth Vallis (24°N, 341°E, -2.2 km) exposes layers within Mars’ surface with differing mineralogy, including at least two kinds of clays. Holden Crater (26°S, 325°E, -1.9 km) has alluvial fans, flood deposits, possible lake beds, and clay- rich sediment. 7 "For Planning and Discussion Purposes Only"

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" MAVEN Project Overview Mission Objectives Determine the role that loss of volatiles from the Mars atmosphere to space has played through time, exploring the histories of Mars’ atmosphere and climate, liquid water, and planetary habitability Determine the current state of the upper atmosphere, ionosphere, and interactions with solar wind Determine the current rates of escape of neutrals and ions to space and the processes controlling them Determine the ratios of stable isotopes that will tell Mars’ history of loss through time Mission Approach Obtain detailed measurements of the upper atmosphere, ionosphere, planetary corona, solar wind, solar EUV and SEPs over a 1-year period, to define the interactions between the Sun and Mars Operate 8 instruments for new science results: Particles and Fields Package (6 instruments): SWEA - Solar Wind Electron Analyzer SWIA - Solar Wind Ion Analyzer STATIC - Suprathermal and Thermal Ion Composition SEP - Solar Energetic Particle LPW - Langmuir Probe and Waves MAG - Magnetometer IUVS - Imaging Ultraviolet Spectrometer NGIMS - Neutral Gas and Ion Mass Spectrometer Fly 75°-inclination, 4.5-hour-period, 150-km-periapsis- altitude science orbit Perform five 5-day “deep dip” campaigns to altitudes near 125 km during the 1-year mission Organizations LASP – PI and science team; E/PO; science operations; IUVS and LPW instruments GSFC – project management; mission systems engineering; safety and mission assurance; project scientist; NGIMS and MAG instruments JPL – Navigation; DSN; Mars Program Office SSL – Deputy PI; Particles and Fields Package management; STATIC, SEP, SWIA, and SWEA instruments; LPW probes and booms (IRAP provides the sensor for SWEA) LM – spacecraft; assembly, test and launch operations; mission operations Launch On an Atlas V from KSC between 11/18/13 and 12/7/13 Mars Orbit Insertion on 9/22/14 (for 11/18/13 launch) Website * Artist Conception *

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" 18 Nov 2013 (Open) 7 Dec 2013 (Close) LV: Atlas V 401 Ten Month Ballistic Cruise to Mars Orbit Insertion: 22 Sept 2014 (Open) 26 Sept 2014 (Close) One Year of Science Operations 20-Day Launch Period Type-II Trajectory Early Cruise Late Cruise Northern Approach ~1233 m/s  V Capture Orbit: 35 hour period 550 km P2 75° inclination Mission Architecture 9/22/14 * Artist Conception * * * *

National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California Mars Exploration Directorate "For Planning and Discussion Purposes Only" Current Status and Plans We are executing on the plan laid out in the proposal three years ago –Spacecraft, instrument and ground systems hardware are being built across the partner institutions; contracts are negotiated; launch service has been authorized – MAVEN is now in the midst of a full press for a successful CDR Season The MAVEN Project has been and continues to receive full funding when it’s been needed. Reserves are at acceptable levels in every year between now and launch Schedule is a continuing focus given the 20-day planetary launch window. MAVEN has sufficient schedule margins but we are always looking at opportunities for improvement MAVEN is on track technically, on schedule and on budget