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Design of Low-Altitude Martian Orbits Using Frequency Analysis A
Design of Low-Altitude Martian Orbits using Frequency Analysis A. Noullez, K. Tsiganis To cite this version: A. Noullez, K. Tsiganis. Design of Low-Altitude Martian Orbits using Frequency Analysis. Advances in Space Research, Elsevier, 2021, 67, pp.477-495. 10.1016/j.asr.2020.10.032. hal-03007909 HAL Id: hal-03007909 https://hal.archives-ouvertes.fr/hal-03007909 Submitted on 16 Nov 2020 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Design of Low-Altitude Martian Orbits using Frequency Analysis A. Noulleza,∗, K. Tsiganisb aUniversit´eC^oted'Azur, Observatoire de la C^oted'Azur, CNRS, Laboratoire Lagrange, bd. de l'Observatoire, C.S. 34229, 06304 Nice Cedex 4, France bSection of Astrophysics Astronomy & Mechanics, Department of Physics, Aristotle University of Thessaloniki, GR 541 24 Thessaloniki, Greece Abstract Nearly-circular Frozen Orbits (FOs) around axisymmetric bodies | or, quasi-circular Periodic Orbits (POs) around non-axisymmetric bodies | are of primary concern in the design of low-altitude survey missions. Here, we study very low-altitude orbits (down to 50 km) in a high-degree and order model of the Martian gravity field. We apply Prony's Frequency Analysis (FA) to characterize the time variation of their orbital elements by computing accurate quasi-periodic decompositions of the eccentricity and inclination vectors. -
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. -
Variability of Mars' North Polar Water Ice Cap I. Analysis of Mariner 9 and Viking Orbiter Imaging Data
Icarus 144, 382–396 (2000) doi:10.1006/icar.1999.6300, available online at http://www.idealibrary.com on Variability of Mars’ North Polar Water Ice Cap I. Analysis of Mariner 9 and Viking Orbiter Imaging Data Deborah S. Bass Instrumentation and Space Research Division, Southwest Research Institute, P.O. Drawer 28510, San Antonio, Texas 78228-0510 E-mail: [email protected] Kenneth E. Herkenhoff U.S. Geological Survey, 2255 North Gemini Drive, Flagstaff, Arizona 86001 and David A. Paige Department of Earth and Space Sciences, University of California, Los Angeles, 405 Hilgard Avenue, Los Angeles, California 90095-1567 Received May 15, 1998; revised November 17, 1999 1. INTRODUCTION Previous studies interpreted differences in ice coverage between Mariner 9 and Viking Orbiter observations of Mars’ north residual Like Earth, Mars has perennial ice caps and an active wa- polar cap as evidence of interannual variability of ice deposition on ter cycle. The Viking Orbiter determined that the surface of the the cap. However,these investigators did not consider the possibility northern residual cap is water ice (Kieffer et al. 1976, Farmer that there could be significant changes in the ice coverage within et al. 1976). At the south residual polar cap, both Mariner 9 the northern residual cap over the course of the summer season. and Viking Orbiter observed carbon dioxide ice throughout the Our more comprehensive analysis of Mariner 9 and Viking Orbiter summer. Many have related observed atmospheric water vapor imaging data shows that the appearance of the residual cap does not abundances to seasonal exchange between reservoirs such as show large-scale variance on an interannual basis. -
Long-Range Rovers for Mars Exploration and Sample Return
2001-01-2138 Long-Range Rovers for Mars Exploration and Sample Return Joe C. Parrish NASA Headquarters ABSTRACT This paper discusses long-range rovers to be flown as part of NASA’s newly reformulated Mars Exploration Program (MEP). These rovers are currently scheduled for launch first in 2007 as part of a joint science and technology mission, and then again in 2011 as part of a planned Mars Sample Return (MSR) mission. These rovers are characterized by substantially longer range capability than their predecessors in the 1997 Mars Pathfinder and 2003 Mars Exploration Rover (MER) missions. Topics addressed in this paper include the rover mission objectives, key design features, and Figure 1: Rover Size Comparison (Mars Pathfinder, Mars Exploration technologies. Rover, ’07 Smart Lander/Mobile Laboratory) INTRODUCTION NASA is leading a multinational program to explore above, below, and on the surface of Mars. A new The first of these rovers, the Smart Lander/Mobile architecture for the Mars Exploration Program has Laboratory (SLML) is scheduled for launch in 2007. The recently been announced [1], and it incorporates a current program baseline is to use this mission as a joint number of missions through the rest of this decade and science and technology mission that will contribute into the next. Among those missions are ambitious plans directly toward sample return missions planned for the to land rovers on the surface of Mars, with several turn of the decade. These sample return missions may purposes: (1) perform scientific explorations of the involve a rover of almost identical architecture to the surface; (2) demonstrate critical technologies for 2007 rover, except for the need to cache samples and collection, caching, and return of samples to Earth; (3) support their delivery into orbit for subsequent return to evaluate the suitability of the planet for potential manned Earth. -
Physical Properties of Martian Meteorites: Porosity and Density Measurements
Meteoritics & Planetary Science 42, Nr 12, 2043–2054 (2007) Abstract available online at http://meteoritics.org Physical properties of Martian meteorites: Porosity and density measurements Ian M. COULSON1, 2*, Martin BEECH3, and Wenshuang NIE3 1Solid Earth Studies Laboratory (SESL), Department of Geology, University of Regina, Regina, Saskatchewan S4S 0A2, Canada 2Institut für Geowissenschaften, Universität Tübingen, 72074 Tübingen, Germany 3Campion College, University of Regina, Regina, Saskatchewan S4S 0A2, Canada *Corresponding author. E-mail: [email protected] (Received 11 September 2006; revision accepted 06 June 2007) Abstract–Martian meteorites are fragments of the Martian crust. These samples represent igneous rocks, much like basalt. As such, many laboratory techniques designed for the study of Earth materials have been applied to these meteorites. Despite numerous studies of Martian meteorites, little data exists on their basic structural characteristics, such as porosity or density, information that is important in interpreting their origin, shock modification, and cosmic ray exposure history. Analysis of these meteorites provides both insight into the various lithologies present as well as the impact history of the planet’s surface. We present new data relating to the physical characteristics of twelve Martian meteorites. Porosity was determined via a combination of scanning electron microscope (SEM) imagery/image analysis and helium pycnometry, coupled with a modified Archimedean method for bulk density measurements. Our results show a range in porosity and density values and that porosity tends to increase toward the edge of the sample. Preliminary interpretation of the data demonstrates good agreement between porosity measured at 100× and 300× magnification for the shergottite group, while others exhibit more variability. -
Volcanism on Mars
Author's personal copy Chapter 41 Volcanism on Mars James R. Zimbelman Center for Earth and Planetary Studies, National Air and Space Museum, Smithsonian Institution, Washington, DC, USA William Brent Garry and Jacob Elvin Bleacher Sciences and Exploration Directorate, Code 600, NASA Goddard Space Flight Center, Greenbelt, MD, USA David A. Crown Planetary Science Institute, Tucson, AZ, USA Chapter Outline 1. Introduction 717 7. Volcanic Plains 724 2. Background 718 8. Medusae Fossae Formation 725 3. Large Central Volcanoes 720 9. Compositional Constraints 726 4. Paterae and Tholi 721 10. Volcanic History of Mars 727 5. Hellas Highland Volcanoes 722 11. Future Studies 728 6. Small Constructs 723 Further Reading 728 GLOSSARY shield volcano A broad volcanic construct consisting of a multitude of individual lava flows. Flank slopes are typically w5, or less AMAZONIAN The youngest geologic time period on Mars identi- than half as steep as the flanks on a typical composite volcano. fied through geologic mapping of superposition relations and the SNC meteorites A group of igneous meteorites that originated on areal density of impact craters. Mars, as indicated by a relatively young age for most of these caldera An irregular collapse feature formed over the evacuated meteorites, but most importantly because gases trapped within magma chamber within a volcano, which includes the potential glassy parts of the meteorite are identical to the atmosphere of for a significant role for explosive volcanism. Mars. The abbreviation is derived from the names of the three central volcano Edifice created by the emplacement of volcanic meteorites that define major subdivisions identified within the materials from a centralized source vent rather than from along a group: S, Shergotty; N, Nakhla; C, Chassigny. -
Resource Utilization and Site Selection for a Self-Sufficient Martian Outpost
NASA/TM-98-206538 Resource Utilization and Site Selection for a Self-Sufficient Martian Outpost G. James, Ph.D. G. Chamitoff, Ph.D. D. Barker, M.S., M.A. April 1998 The NASA STI Program Office... in Profile Since its founding, NASA has been dedicated to CONTRACTOR REPORT. Scientific and the advancement of aeronautics and space technical findings by NASA-sponsored science. The NASA Scientific and Technical contractors and grantees. Information (STI) Program Office plays a key part in helping NASA maintain this important CONFERENCE PUBLICATION. Collected role. papers from scientific and technical confer- ences, symposia, seminars, or other meetings The NASA STI Program Office is operated by sponsored or cosponsored by NASA. Langley Research Center, the lead center for NASA's scientific and technical information. SPECIAL PUBLICATION. Scientific, The NASA STI Program Office provides access technical, or historical information from to the NASA STI Database, the largest NASA programs, projects, and mission, often collection of aeronautical and space science STI concerned with subjects having substantial in the word. The Program Office is also public interest. NASA's institutional mechanism for disseminating the results of its research and • TECHNICAL TRANSLATION. development activities. These results are English-language translations of foreign scientific published by NASA in the NASA STI Report and technical material pertinent to NASA's Series, which includes the following report mission. types: Specialized services that complement the STI TECHNICAL PUBLICATION. Reports of Program Office's diverse offerings include completed research or a major significant creating custom thesauri, building customized phase of research that present the results of databases, organizing and publishing research NASA programs and include extensive results.., even providing videos. -
Navigation Challenges During Exomars Trace Gas Orbiter Aerobraking Campaign
NON-PEER REVIEW Please select category below: Normal Paper Student Paper Young Engineer Paper Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign Gabriele Bellei 1, Francesco Castellini 2, Frank Budnik 3 and Robert Guilanyà Jané 4 1 DEIMOS Space located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 2 Telespazio VEGA located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 3 ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 4 GMV INSYEN located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany Abstract The ExoMars Trace Gas Orbiter satellite spent one year in aerobraking operations at Mars, lowering its orbit period from one sol to about two hours. This delicate phase challenged the operations team and in particular the navigation system due to the highly unpredictable Mars atmosphere, which imposed almost continuous monitoring, navigation and re-planning activities. An aerobraking navigation concept was, for the first time at ESA, designed, implemented and validated on-ground and in-flight, based on radiometric tracking data and complemented by information extracted from spacecraft telemetry. The aerobraking operations were successfully completed, on time and without major difficulties, thanks to the simplicity and robustness of the selected approach. This paper describes the navigation concept, presents a recollection of the main in-flight results and gives a retrospective of the main lessons learnt during this activity. Keywords: ExoMars, Trace Gas Orbiter, aerobraking, navigation, orbit determination, Mars atmosphere, accelerometer Introduction The ExoMars program is a cooperation between the European Space Agency (ESA) and Roscosmos for the robotic exploration of the red planet. -
Initial Maven Observations of Ion Cyclotron Waves and Pickup Protons: a Measurement of Hydrogen Loss in the Upper Martian Exosphere F
46th Lunar and Planetary Science Conference (2015) 2628.pdf INITIAL MAVEN OBSERVATIONS OF ION CYCLOTRON WAVES AND PICKUP PROTONS: A MEASUREMENT OF HYDROGEN LOSS IN THE UPPER MARTIAN EXOSPHERE F. J. Crary1, J. E. P. Connerney2, J. R. Espley3 and J. P. McFadden4, 1Laboratory for Space and Atmospheric Physics, University of Col- orado, Boulder, 1234 Innovation Dr., Boulder, CO, 80303, [email protected] 2Goddard Space Flight Center, Mail Code 695, Greenbelt, MD, 20771, [email protected] 3Goddard Space Flight Center, Mail Code 695, Greenbelt, MD, 20771, [email protected], 4Space Science Laboratory, University of California, Berkeley, 7 Gauss Way, Berkeley, CA 94720-7450, [email protected]. Introduction: Observations by the Mars Global Surveyor, Mars Express and Phobos 2 spacecraft [1],[2],[3] have shown that Mars has a hydrogen exo- sphere which extends as much as ten Martian radii from the planet. These hydrogen atoms ionize and are “picked up” in the solar wind flow. Neither the associ- ated hydrogen loss rate nor the structure of this extend- ed exosphere, have previously been well determined. The resulting pickup protons have a distinctive veloci- ty distribution and generate low frequency electromag- netic waves near the ion cyclotron frequency. Proton pickup ions have been observed by Mars Express [4] and proton cyclotron waves have been observed by Mars Global Surveyor [2]. The MAVEN spacecraft is the first Mars orbiter able to simultane- ously measure both ion cyclotron waves. Data from the spacecraft’s magnetometer [5], providing the vector magnetic field at a rate of 32 samples per second, is Fourier transformed to produce dynamic spectra of right-circularly polarized (whistler mode) and left- circularly polarized (ion cyclotron mode) ultralow fre- quency electromagnetic waves. -
Mineralogy of the Martian Surface
EA42CH14-Ehlmann ARI 30 April 2014 7:21 Mineralogy of the Martian Surface Bethany L. Ehlmann1,2 and Christopher S. Edwards1 1Division of Geological & Planetary Sciences, California Institute of Technology, Pasadena, California 91125; email: [email protected], [email protected] 2Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109 Annu. Rev. Earth Planet. Sci. 2014. 42:291–315 Keywords First published online as a Review in Advance on Mars, composition, mineralogy, infrared spectroscopy, igneous processes, February 21, 2014 aqueous alteration The Annual Review of Earth and Planetary Sciences is online at earth.annualreviews.org Abstract This article’s doi: The past fifteen years of orbital infrared spectroscopy and in situ exploration 10.1146/annurev-earth-060313-055024 have led to a new understanding of the composition and history of Mars. Copyright c 2014 by Annual Reviews. Globally, Mars has a basaltic upper crust with regionally variable quanti- by California Institute of Technology on 06/09/14. For personal use only. All rights reserved ties of plagioclase, pyroxene, and olivine associated with distinctive terrains. Enrichments in olivine (>20%) are found around the largest basins and Annu. Rev. Earth Planet. Sci. 2014.42:291-315. Downloaded from www.annualreviews.org within late Noachian–early Hesperian lavas. Alkali volcanics are also locally present, pointing to regional differences in igneous processes. Many ma- terials from ancient Mars bear the mineralogic fingerprints of interaction with water. Clay minerals, found in exposures of Noachian crust across the globe, preserve widespread evidence for early weathering, hydrothermal, and diagenetic aqueous environments. Noachian and Hesperian sediments include paleolake deposits with clays, carbonates, sulfates, and chlorides that are more localized in extent. -
Planetary Science
Mission Directorate: Science Theme: Planetary Science Theme Overview Planetary Science is a grand human enterprise that seeks to discover the nature and origin of the celestial bodies among which we live, and to explore whether life exists beyond Earth. The scientific imperative for Planetary Science, the quest to understand our origins, is universal. How did we get here? Are we alone? What does the future hold? These overarching questions lead to more focused, fundamental science questions about our solar system: How did the Sun's family of planets, satellites, and minor bodies originate and evolve? What are the characteristics of the solar system that lead to habitable environments? How and where could life begin and evolve in the solar system? What are the characteristics of small bodies and planetary environments and what potential hazards or resources do they hold? To address these science questions, NASA relies on various flight missions, research and analysis (R&A) and technology development. There are seven programs within the Planetary Science Theme: R&A, Lunar Quest, Discovery, New Frontiers, Mars Exploration, Outer Planets, and Technology. R&A supports two operating missions with international partners (Rosetta and Hayabusa), as well as sample curation, data archiving, dissemination and analysis, and Near Earth Object Observations. The Lunar Quest Program consists of small robotic spacecraft missions, Missions of Opportunity, Lunar Science Institute, and R&A. Discovery has two spacecraft in prime mission operations (MESSENGER and Dawn), an instrument operating on an ESA Mars Express mission (ASPERA-3), a mission in its development phase (GRAIL), three Missions of Opportunities (M3, Strofio, and LaRa), and three investigations using re-purposed spacecraft: EPOCh and DIXI hosted on the Deep Impact spacecraft and NExT hosted on the Stardust spacecraft. -
OVERVIEW of the PHOENIX MARS LANDER MISSION. P. H. Smith1, 1Lunar and Planetary Lab, University of Arizona, Tucson, AZ 85721, [email protected]
Martian Sulfates as Recorders of Atmospheric-Fluid-Rock Interactions (2006) 7069.pdf OVERVIEW OF THE PHOENIX MARS LANDER MISSION. P. H. Smith1, 1Lunar and Planetary Lab, University of Arizona, Tucson, AZ 85721, [email protected]. Introduction: The Phoenix lander is ples of this biological paydirt and test for the next mission to study the surface of signatures related to biology. Mars in situ. By studying the active water Baseline Mission: After the initial as- cycles in the polar region, it complements sessment of the landing site by the science the Mars Exploration Rovers that look at team, the primary science phase of the the ancient history of Mars contained in mission begins with the collection of sur- the solid rocks. Lacking mobility, Phoenix face samples. Two major science instru- explores the subsurface to the north of the ments receive and analyze the samples. lander, studying the mineralogy and The first is the thermal evolved gas ana- chemistry of the soils and ice. lyzer (TEGA). A sample is delivered to a Scientific Objectives, Phoenix Follows hopper that feeds a small amount of soil the Water: The Phoenix mission targets into a tiny oven, which is sealed and the northern plains between 65 and 72 N. heated slowly to temperatures approaching High-resolution images from the Mars Or- 1000 C. The heater power profile neces- biter Camera on the Mars Global Surveyor sary to maintain a constant temperature spacecraft show a “basketball-like” texture gradient contains peaks and valleys that on the surface with low hummocks spaced indicate phase transitions. For instance, 10’s of meters apart; polygonal terrain, or ice will show a feature at its melting point patterned ground, is also common.