Mars Science Laboratory: Curiosity Rover Curiosity’S Mission: Was Mars Ever Habitable? Acquires Rock, Soil, and Air Samples for Onboard Analysis
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Mars Reconnaissance Orbiter Navigation Strategy for the Exomars Schiaparelli EDM Lander Mission
Jet Propulsion Laboratory California Institute of Technology Mars Reconnaissance Orbiter Navigation Strategy for the ExoMars Schiaparelli EDM Lander Mission Premkumar R. Menon Sean V. Wagner, David C. Jefferson, Eric J. Graat, Kyong J. Lee, and William B. Schulze AAS/AIAA Astrodynamics Specialist Conference San Antonio, Texas February 5–9, 2017 AAS Paper 17-337 © 2017 California Institute of Technology. Government Sponsorship Acknowledged. Mars Reconnaissance Orbiter Project Mars Reconnaissance Orbiter (Mission, Spacecraft and PSO) The Mars Reconnaissance Orbiter mission launched in August 2005 from the Cape Canaveral Air Force Station arriving at Mars in March 2006 started science operations in November 2006. MRO has completed 10 years since launch (50,000 orbits by Mar 2017) and to date has returned nearly 300 Terabytes of data. MRO Primary Science Orbit (PSO): • Sun-synchronous orbit ascending node at 3:00 PM ± 15 minutes Local Mean Solar Time (LMST) (daylight equatorial crossing) • Periapsis is frozen about the Mars South Pole • Near-repeat ground track walk (GTW) every 17-day, 211 orbit (short-term repeat) MRO targeting cycle, exact repeat after 4602 orbits. The nominal GTW is 32.45811 km West each 211 orbit cycle (maintained with periodic maneuvers). MRO Spacecraft: • Spacecraft Bus: 3-axis stabilized ACS system; 3-meter diameter High Gain Antenna; hydrazine propulsion system • Instrument Suite: HiRISE Camera, CRISM Imaging spectrometer, Mars Climate Sounder, Mars Color Imager, Context Camera, Shallow Subsurface Radar, Electra engineering payload (among other instrument payloads) 2/07/17 MRO support of ExoMars Schiaparelli Lander Overflight Relay PRM-3 4. MRO shall have good overflight pass geometry within the first 2 Sols after landing. -
NASA's Curiosity Rover Maximizes Data Sent to Earth by Using International Space Data Communication Standards
Press Release For immediate release NASA's Curiosity Rover Maximizes Data Sent to Earth by Using International Space Data Communication Standards WASHINGTON, 22 August 2012 (CCSDS) – NASA’s Mars Science Laboratory (MSL) mission began its planned 2-year Mars surface exploration mission on August 6 after landing its large, mobile laboratory called Curiosity. The goal of the mission is to assess whether Mars has ever had, or still has, environmental conditions favorable to microbial life. Curiosity, with its one-ton payload carrying capacity carries 10 science instruments that will gather samples of rocks and soil, and process and distribute them to onboard test chambers inside analytical instruments. Some of the rover’s scientific data, including images of the surface of Mars collected by Curiosity’s 17 onboard cameras, are sent directly to and from Earth via NASA’s Deep Space Network (DSN) of large ground antennas. However, once Curiosity becomes fully operational most of the scientific and engineering data will be transferred via relay satellites that are in orbit around Mars. These are primarily the Mars Reconnaissance Orbiter (MRO) and the Mars Odyssey (ODY) spacecraft. The MSL Mars-Earth communications systems are using internationally-agreed space data communications standards to enable reliable transmission of the expected rich data sets to be gathered by Curiosity. These standards were developed by a team of international space data communication specialists collaborating within the Consultative Committee for Space Data Systems (CCSDS). Use of internationally-agreed upon standards reduce cost and risk to space missions, and also offer rich “cross-support” capabilities to collaborate since key data interfaces are inherently interoperable. -
Exomars Schiaparelli Direct-To-Earth Observation Using GMRT
TECHNICAL ExoMars Schiaparelli Direct-to-Earth Observation REPORTS: METHODS 10.1029/2018RS006707 using GMRT S. Esterhuizen1, S. W. Asmar1 ,K.De2, Y. Gupta3, S. N. Katore3, and B. Ajithkumar3 Key Point: • During ExoMars Landing, GMRT 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA, USA, 2Cahill Center for Astrophysics, observed UHF transmissions and California Institute of Technology, Pasadena, CA, USA, 3National Centre for Radio Astrophysics, Pune, India Doppler shift used to identify key events as only real-time aliveness indicator Abstract During the ExoMars Schiaparelli separation event on 16 October 2016 and Entry, Descent, and Landing (EDL) events 3 days later, the Giant Metrewave Radio Telescope (GMRT) near Pune, India, Correspondence to: S. W. Asmar, was used to directly observe UHF transmissions from the Schiaparelli lander as they arrive at Earth. The [email protected] Doppler shift of the carrier frequency was measured and used as a diagnostic to identify key events during EDL. This signal detection at GMRT was the only real-time aliveness indicator to European Space Agency Citation: mission operations during the critical EDL stage of the mission. Esterhuizen, S., Asmar, S. W., De, K., Gupta, Y., Katore, S. N., & Plain Language Summary When planetary missions, such as landers on the surface of Mars, Ajithkumar, B. (2019). ExoMars undergo critical and risky events, communications to ground controllers is very important as close to real Schiaparelli Direct-to-Earth observation using GMRT. time as possible. The Schiaparelli spacecraft attempted landing in 2016 was supported in an innovative way. Radio Science, 54, 314–325. A large radio telescope on Earth was able to eavesdrop on information being sent from the lander to other https://doi.org/10.1029/2018RS006707 spacecraft in orbit around Mars. -
The Rock Abrasion Record at Gale Crater: Mars Science Laboratory
PUBLICATIONS Journal of Geophysical Research: Planets RESEARCH ARTICLE The rock abrasion record at Gale Crater: Mars 10.1002/2013JE004579 Science Laboratory results from Bradbury Special Section: Landing to Rocknest Results from the first 360 Sols of the Mars Science Laboratory N. T. Bridges1, F. J. Calef2, B. Hallet3, K. E. Herkenhoff4, N. L. Lanza5, S. Le Mouélic6, C. E. Newman7, Mission: Bradbury Landing D. L. Blaney2,M.A.dePablo8,G.A.Kocurek9, Y. Langevin10,K.W.Lewis11, N. Mangold6, through Yellowknife Bay S. Maurice12, P.-Y. Meslin12,P.Pinet12,N.O.Renno13,M.S.Rice14, M. E. Richardson7,V.Sautter15, R. S. Sletten3,R.C.Wiens6, and R. A. Yingst16 Key Points: • Ventifacts in Gale Crater 1Applied Physics Laboratory, Laurel, Maryland, USA, 2Jet Propulsion Laboratory, Pasadena, California, USA, 3Department • Maybeformedbypaleowind of Earth and Space Sciences, College of the Environments, University of Washington, Seattle, Washington, USA, 4U.S. • Can see abrasion textures at range 5 6 of scales Geological Survey, Flagstaff, Arizona, USA, Los Alamos National Laboratory, Los Alamos, New Mexico, USA, LPGNantes, UMR 6112, CNRS/Université de Nantes, Nantes, France, 7Ashima Research, Pasadena, California, USA, 8Universidad de Alcala, Madrid, Spain, 9Department of Geological Sciences, Jackson School of Geosciences, University of Texas at Austin, Supporting Information: Austin, Texas, USA, 10Institute d’Astrophysique Spatiale, Université Paris-Sud, Orsay, France, 11Department of • Figure S1 12 fi • Figure S2 Geosciences, Princeton University, Princeton, New Jersey, USA, Centre National de la Recherche Scienti que, Institut 13 • Table S1 de Recherche en Astrophysique et Planétologie, CNRS-Université Toulouse, Toulouse, France, Department of Atmospheric, Oceanic, and Space Science; College of Engineering, University of Michigan, Ann Arbor, Michigan, USA, Correspondence to: 14Division of Geological and Planetary Sciences, California Institute of Technology, Pasadena, California, USA, 15Lab N. -
Mars Reconnaissance Orbiter
Chapter 6 Mars Reconnaissance Orbiter Jim Taylor, Dennis K. Lee, and Shervin Shambayati 6.1 Mission Overview The Mars Reconnaissance Orbiter (MRO) [1, 2] has a suite of instruments making observations at Mars, and it provides data-relay services for Mars landers and rovers. MRO was launched on August 12, 2005. The orbiter successfully went into orbit around Mars on March 10, 2006 and began reducing its orbit altitude and circularizing the orbit in preparation for the science mission. The orbit changing was accomplished through a process called aerobraking, in preparation for the “science mission” starting in November 2006, followed by the “relay mission” starting in November 2008. MRO participated in the Mars Science Laboratory touchdown and surface mission that began in August 2012 (Chapter 7). MRO communications has operated in three different frequency bands: 1) Most telecom in both directions has been with the Deep Space Network (DSN) at X-band (~8 GHz), and this band will continue to provide operational commanding, telemetry transmission, and radiometric tracking. 2) During cruise, the functional characteristics of a separate Ka-band (~32 GHz) downlink system were verified in preparation for an operational demonstration during orbit operations. After a Ka-band hardware anomaly in cruise, the project has elected not to initiate the originally planned operational demonstration (with yet-to-be used redundant Ka-band hardware). 201 202 Chapter 6 3) A new-generation ultra-high frequency (UHF) (~400 MHz) system was verified with the Mars Exploration Rovers in preparation for the successful relay communications with the Phoenix lander in 2008 and the later Mars Science Laboratory relay operations. -
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering Laurel Mossman, Kate Schein, and Amelia Peoples Senior Division Group Documentary Word Count: 499 Our group chose the topic, Donna Shirley and her Mars rover, because of our connections and our interest level in not only science but strong, determined women. One of our group member’s mothers worked for a man under Ms. Shirley when she was developing the Mars rover. This provided us with a connection to Ms. Shirley, which then gave us the amazing opportunity to interview her. In addition, our group is interested in the philosophy of equality and we have continuously created documentaries that revolve around this idea. Every member of our group is a female, so we understand the struggles and discrimination that women face in an everyday setting and wanted to share the story of a female that faced these struggles but overcame them. Thus after conducting a great amount of research, we fell in love with Donna Shirley’s story. Lastly, it was an added benefit that Ms. Shirley is from Oklahoma, making her story important to our state. All of these components made this topic extremely appealing to us. We conducted our research using online articles, Donna Shirley’s autobiography, “Managing Martians”, news coverage from the launch day, and our interview with Donna Shirley. We started our research process by reading Shirley’s autobiography. This gave us insight into her college life, her time working at the Jet Propulsion Laboratory, and what it was like being in charge of such a barrier-breaking mission. -
Chemical Variations in Yellowknife Bay Formation Sedimentary Rocks
PUBLICATIONS Journal of Geophysical Research: Planets RESEARCH ARTICLE Chemical variations in Yellowknife Bay formation 10.1002/2014JE004681 sedimentary rocks analyzed by ChemCam Special Section: on board the Curiosity rover on Mars Results from the first 360 Sols of the Mars Science Laboratory N. Mangold1, O. Forni2, G. Dromart3, K. Stack4, R. C. Wiens5, O. Gasnault2, D. Y. Sumner6, M. Nachon1, Mission: Bradbury Landing P.-Y. Meslin2, R. B. Anderson7, B. Barraclough4, J. F. Bell III8, G. Berger2, D. L. Blaney9, J. C. Bridges10, through Yellowknife Bay F. Calef9, B. Clark11, S. M. Clegg5, A. Cousin5, L. Edgar8, K. Edgett12, B. Ehlmann4, C. Fabre13, M. Fisk14, J. Grotzinger4, S. Gupta15, K. E. Herkenhoff7, J. Hurowitz16, J. R. Johnson17, L. C. Kah18, N. Lanza19, Key Points: 2 1 20 21 12 16 2 • J. Lasue , S. Le Mouélic , R. Léveillé , E. Lewin , M. Malin , S. McLennan , S. Maurice , Fluvial sandstones analyzed by 22 22 23 19 19 24 25 ChemCam display subtle chemical N. Melikechi , A. Mezzacappa , R. Milliken , H. Newsom , A. Ollila , S. K. Rowland , V. Sautter , variations M. Schmidt26, S. Schröder2,C.d’Uston2, D. Vaniman27, and R. Williams27 • Combined analysis of chemistry and texture highlights the role of 1Laboratoire de Planétologie et Géodynamique de Nantes, CNRS, Université de Nantes, Nantes, France, 2Institut de Recherche diagenesis en Astrophysique et Planétologie, CNRS/Université de Toulouse, UPS-OMP, Toulouse, France, 3Laboratoire de Géologie de • Distinct chemistry in upper layers 4 5 suggests distinct setting and/or Lyon, Université de Lyon, Lyon, France, California Institute of Technology, Pasadena, California, USA, Los Alamos National 6 source Laboratory, Los Alamos, New Mexico, USA, Earth and Planetary Sciences, University of California, Davis, California, USA, 7Astrogeology Science Center, U.S. -
Planting and Germination of Sweet Potato, Yam and Radish Plants in the Mars Desert Research Station
Copyright © 2015 by Olenka Jibaja Valderrama. Published by The Mars Society with permission. Planting and Germination of Sweet Potato, Yam and Radish Plants in the Mars Desert Research Station Olenka Jibaja Valderrama Universidad Católica Santo Toribio de Mogrovejo – Chiclayo, Perú [email protected] Abstract: As part of the future exploration of the universe, manned missions to other planets or satellites near Earth will be needed. One of the main objectives of these missions will be to reach Mars because it is at a relatively close distance to our planet and because both planets have some common characteristics. Since the economic investment of these explorations is quite high, the duration of them must be significant; that’s why the missions should aim to be self-sufficient. The search for food sources for crew members is a key factor to be investigated and even more attention should be on food whose production is possible and sustainable in the environment where the mission arises. This work was involved with the planting and germination of radish, yam and sweet potato plants in the greenhouse of the Mars Desert Research Station (MDRS) and the main objective was to investigate the characteristics of growth and development of these plants in Martian conditions to find out whether its production is possible or not. Orange skin and white skin: two types of sweet potatoes were planted. During rotation, it was discovered that yam grew faster under these conditions than the rest of the tubers, although its development was slower as compared to terrestrial conditions. Radish plants in Mars regolith grew in a similar speed than in the fertile Earth soil, and even faster than in drier soil taken from the desert. -
NASA's Mars 2020 Perseverance Rover Gets Balanced 21 April 2020
NASA's Mars 2020 Perseverance rover gets balanced 21 April 2020 minimize friction that could affect the accuracy of the results, the table's surface sits on a spherical air bearing that essentially levitates on a thin layer of nitrogen gas. To determine center of gravity relative to the rover's z-axis (which extends from the bottom of the rover through the top) and y-axis (from the rover's left to right side), the team slowly rotated the vehicle back and forth, calculating the imbalance in its mass distribution. NASA's Perseverance rover is moved during a test of its mass properties at Kennedy Space Center in Florida. The image was taken on April 7, 2020. Credit: NASA/JPL-Caltech With 13 weeks to go before the launch period of NASA's Mars 2020 Perseverance rover opens, final preparations of the spacecraft continue at the Kennedy Space Center in Florida. On April 8, the This image of the Perseverance Mars rover was taken at assembly, test and launch operations team NASA's Kennedy Space Center on April 7, 2020, during a completed a crucial mass properties test of the test of the vehicle's mass properties. Credit: NASA/JPL- rover. Caltech Precision mass properties measurements are essential to a safe landing on Mars because they help ensure that the spacecraft travels accurately Just as an auto mechanic places small weights on throughout its trip to the Red Planet—from launch a car tire's rim to bring it into balance, the through its entry, descent and landing. Perseverance team analyzed the data and then added 13.8 pounds (6.27 kilograms) to the rover's On April 6, the meticulous three-day process chassis. -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
Margie Burns
Gumbo ~ The Grail Connection ~ February 2008 MEMBER GIVING ANALYSIS 2007 The 2007 Member Giving figures are in. Here’s a snapshot of how we ended the year. TOTAL 2007 MEMBER DONATIONS = $ 149,475 Reflects donations to: » The National Office » Grailville » Cornwall » Development Loan forgiveness » “Other” donations/in kind services through National Office Does not include $3,950 from U.S. members in other countries # OF MEMBERS GIVING All member categories = 144 of 242 (59.5%) Active & Wider Grail = 125 of 201 (62%) Emerita donations = $32,283 Development Loan Forgiveness = $ 22,375 Donated Salary / WIST training fees = $ 11,000 $ 33,375 MEMBER DONATIONS TO: National Office = $ 71,855 Grailville = $ 24,030 Cornwall = $ 19,240 A SPECIAL THANK YOU! TO ALL WHO FORGAVE THE LOANS THEY MADE TO THE GRAIL IN THE 1990S FOR THE ESTABLISHMENT OF A DEVELOPMENT OFFICE! 1 GENERAL ASSEMBLY 2008: JUNE 23-29 SCENARIO PLANNING FOR THE FUTURE OF THE GRAIL ~ Judith Blackburn ~ for the Council Preparation for this year’s General Assembly is now underway, and a packet of scenarios depicting the Grail of the future has been distributed to members. All of the scenarios are based on the simple fact that the Grail is not now operating on a sustainable model. Your job is to help discern how we might downsize or re-focus. Times have changed. We no longer recruit women who are able or willing to donate their working lives to the Grail. At the same time we have many ongoing obligations to each other, to our properties, and to the Grail itself. One of our strengths has been how comprehensive our programming has been, but at this juncture we MUST either simplify or scale back our operations. -
Mars 2020 Radiological Contingency Planning
National Aeronautics and Space Administration Mars 2020 Radiological Contingency Planning NASA plans to launch the Mars 2020 rover, produce the rover’s onboard power and to Perseverance, in summer 2020 on a mission warm its internal systems during the frigid to seek signs of habitable conditions in Mars’ Martian night. ancient past and search for signs of past microbial life. The mission will lift off from Cape NASA prepares contingency response plans Canaveral Air Force Station in Florida aboard a for every launch that it conducts. Ensuring the United Launch Alliance Atlas V launch vehicle safety of launch-site workers and the public in between mid-July and August 2020. the communities surrounding the launch area is the primary consideration in this planning. The Mars 2020 rover design is based on NASA’s Curiosity rover, which landed on Mars in 2012 This contingency planning task takes on an and greatly increased our knowledge of the added dimension when the payload being Red Planet. The Mars 2020 rover is equipped launched into space contains nuclear material. to study its landing site in detail and collect and The primary goal of radiological contingency store the most promising samples of rock and planning is to enable an efficient response in soil on the surface of Mars. the event of an accident. This planning is based on the fundamental principles of advance The system that provides electrical power for preparation (including rehearsals of simulated Mars 2020 and its scientific equipment is the launch accident responses), the timely availability same as for the Curiosity rover: a Multi- of technically accurate and reliable information, Mission Radioisotope Thermoelectric Generator and prompt external communication with the (MMRTG).