45. Space Robots and Systems
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NASA Mars Helicopter Team Striving for a “Kitty Hawk” Moment
NASA Mars Helicopter Team Striving for a “Kitty Hawk” Moment NASA’s next Mars exploration ground vehicle, Mars 2020 Rover, will carry along what could become the first aircraft to fly on another planet. By Richard Whittle he world altitude record for a helicopter was set on June 12, 1972, when Aérospatiale chief test pilot Jean Boulet coaxed T his company’s first SA 315 Lama to a hair-raising 12,442 m (40,820 ft) above sea level at Aérodrome d’Istres, northwest of Marseille, France. Roughly a year from now, NASA hopes to fly an electric helicopter at altitudes equivalent to two and a half times Boulet’s enduring record. But NASA’s small, unmanned machine actually will fly only about five meters above the surface where it is to take off and land — the planet Mars. Members of NASA’s Mars Helicopter team prepare the flight model (the actual vehicle going to Mars) for a test in the JPL The NASA Mars Helicopter is to make a seven-month trip to its Space Simulator on Jan. 18, 2019. (NASA photo) destination folded up and attached to the underbelly of the Mars 2020 Rover, “Perseverance,” a 10-foot-long (3 m), 9-foot-wide (2.7 The atmosphere of Mars — 95% carbon dioxide — is about one m), 7-foot-tall (2.13 m), 2,260-lb (1,025-kg) ground exploration percent as dense as the atmosphere of Earth. That makes flying at vehicle. The Rover is scheduled for launch from Cape Canaveral five meters on Mars “equal to about 100,000 feet [30,480 m] above this July on a United Launch Alliance Atlas V rocket and targeted sea level here on Earth,” noted Balaram. -
Mars Science Laboratory Entry Capsule Aerothermodynamics and Thermal Protection System
Mars Science Laboratory Entry Capsule Aerothermodynamics and Thermal Protection System Karl T. Edquist ([email protected], 757-864-4566) Brian R. Hollis ([email protected], 757-864-5247) NASA Langley Research Center, Hampton, VA 23681 Artem A. Dyakonov ([email protected], 757-864-4121) National Institute of Aerospace, Hampton, VA 23666 Bernard Laub ([email protected], 650-604-5017) Michael J. Wright ([email protected], 650-604-4210) NASA Ames Research Center, Moffett Field, CA 94035 Tomasso P. Rivellini ([email protected], 818-354-5919) Eric M. Slimko ([email protected], 818-354-5940) Jet Propulsion Laboratory, Pasadena, CA 91109 William H. Willcockson ([email protected], 303-977-5094) Lockheed Martin Space Systems Company, Littleton, CO 80125 Abstract—The Mars Science Laboratory (MSL) spacecraft TABLE OF CONTENTS is being designed to carry a large rover (> 800 kg) to the 1. INTRODUCTION ..................................................... 1 surface of Mars using a blunt-body entry capsule as the 2. COMPUTATIONAL RESULTS ................................. 2 primary decelerator. The spacecraft is being designed for 3. EXPERIMENTAL RESULTS .................................... 5 launch in 2009 and arrival at Mars in 2010. The 4. TPS TESTING AND MODEL DEVELOPMENT.......... 7 combination of large mass and diameter with non-zero 5. SUMMARY ........................................................... 11 angle-of-attack for MSL will result in unprecedented REFERENCES........................................................... 11 convective heating environments caused by turbulence prior BIOGRAPHY ............................................................ 12 to peak heating. Navier-Stokes computations predict a large turbulent heating augmentation for which there are no supporting flight data1 and little ground data for validation. -
Planetary Exploration Using Biomimetics an Entomopter for Flight on Mars Phase II Project NAS5-98051
Planetary Exploration Using Biomimetics An Entomopter for Flight On Mars Phase II Project NAS5-98051 NIAC Fellows Conference June 11-12, 2002 Lunar and Planetary Institute Houston Texas Anthony Colozza Northland Scientific / Ohio Aerospace Institute Cleveland, Ohio Planetary Exploration Using Biomimetics Team Members • Mr. Anthony Colozza / Northland Scientific Inc. • Prof. Robert Michelson / Georgia Tech Research Institute • Mr. Teryn Dalbello / University of Toledo ICOMP • Dr.Carol Kory / Northland Scientific Inc. • Dr. K.M. Isaac / University of Missouri-Rolla • Mr. Frank Porath / OAI • Mr. Curtis Smith / OAI Mars Exploration Mars has been the primary object of planetary exploration for the past 25 years To date all exploration vehicles have been landers orbiters and a rover The next method of exploration that makes sense for mars is a flight vehicle Mars Exploration Odyssey Orbiter Viking I & II Lander & Orbiter Global Surveyor Pathfinder Lander & Rover Mars Environment Mars Earth Temp Range -143°C to 27°C -62°C to 50°C & Mean -43°C 15°C Surface 650 Pa 103300 Pa Pressure Gravity 3.75 m/s2 9.81 m/s2 Day Length 24.6 hrs 23.94 hrs Year Length 686 days 365.26 days Diameter 6794 km 12756 km Atmosphere CO2 N2, O2 Composition History of Mars Aircraft Concepts Inflatable Solar Aircraft Concept Hydrazine Power Aircraft Concept MiniSniffer Aircraft Long Endurance Solar Aircraft Concept Key Challenges to Flight On Mars • Atmospheric Conditions (Aerodynamics) • Deployment • Communications • Mission Duration Environment: Atmosphere • Very low atmospheric -
Rtg Impact Response to Hard Landing During Mars Environmental Survey (Mesur) Mission
RTG IMPACT RESPONSE TO HARD LANDING DURING MARS ENVIRONMENTAL SURVEY (MESUR) MISSION A. Schock M. Mukunda Space ABSTRACT Since the simultaneous operation of large number of landers over a long period of time is required, the landers The National Aeronautics and Space Administration must be capable of long life. They must be simple so that (NASA) is studying a seven-year robotic mission (MESUR, a large number can be sent at affordable cost, and yet Mars Environmental Survey) for the seismic, meteorological, rugged and robust In order to survive a wide range of and geochemical exploration of the Martian surface by means landing and environmental conditions, of a network of -16 small, inexpensive landers spread from pole to pole. To permit operation at high Martian latitudes, NASA has basellned the use of Radioisotope NASA has tentatively decided to power the landers with small Thermoelectric Generators (RTGs) to power the probe, RTGs (Radioisotope Thermoelectric Generators). To support lander, and scientific Instruments. Considerations favoring the NASA mission study, the Department of Energy's Office of the use of RTGs are their applicability at both low and high Special Applications commissioned Fairchild to perform Martian latitudes, their ability to operate during and after specialized RTG design studies. Those studies indicated that Martian sandstorms, and their ability to withstand Martian the cost and complexity of the mission could be significantly ground impacts at high velocities and g-loads. reduced if the RTGs had sufficient impact resistance to survive ground impact of the landers without retrorockets. High Impact resistance of the RTGs can be of critical Fairchild designs of RTGs configured for high impact importance In reducing the complexity and cost of the resistance were reported previously. -
Sojourner on Mars and Lessons Learned for Future Planetary Missions
981695 Sojourneron M arsand Lessons Learned forFuturePlanetary Rovers Brian W ilcox and Tam Nguyen NASA's JetPropulsion Laboratory C opyright© 1997 SocietyofAutom otive Engineers,Inc. ABSTRACT The sitelocations w ere designated by a hum an operator using engineering datacollected during previous On July 4, 1997, the M arsPathfinder spacecraft traversals and end-of-solstereo im ages captured by the successfullylanded on M arsinthe Ares Vallislanding lander IMP (Im ager for M arsPathfinder) cam eras. site and deployed an 11.5-kilogram m icrorover nam ed During the traversalsthe rover autonom ouslyavoided Sojourner.Thismicrorover accom plished itsprimary rock,drop-off,and slope hazards. Itchanged its course mission objectives inthe first 7 days, and continued to toavoidthese hazards and turned back tow ardits goals operatefora totalof83 sols(1 sol= M ars day = 1 Earth w henever the hazards w erenolonger inits w ay. The day + ~24 m ins)untilthe landerlostcom m unication w ith rover used "dead reckoning" counting w heel turns and Earth, probably due tolander batteryfailure. The using on-boardrate sensorsestimate position. Although microrover navigated to m any sites surrounding the the rover telem etryrecorded itsresponses to hum an lander, and conducted various science and technology driver com m ands in detail,the vehicle'sactualpositions experim entsusing itson-boardinstrum ents. were not know n untilexamination of the lander stereo im ages at the end of the sol.Acollection of stereo Inthis paper,the rover navigation perform ance is im ages containing rover tracks allow s reconstruction of analyzed on the basisofreceived rovertelem etry, rover the rover physicaltraversalpaththoughoutthe m ission. uplink com m ands and stereo im ages captured by the Since the primary purpose for a robotic vehicleon lander cam eras. -
Scientific Exploration of Mars
Chapter 5 Scientific Exploration of Mars UNDERSTANDING MARS successfully inserted Mariner 9 into an orbit about Mars8 on November 13, 1971. It was the The planets have fascinated humankind ever first spacecraft to orbit another planet (box 5-A). since observers first recognized that they had For the first 2 months of the spacecraft’s stay in characteristic motions different from the stars. Mars’ orbit, the most severe Martian dust storms Astronomers in the ancient Mediterranean called ever recorded obscured Mars surface features. them the wanderers because they appear to wan- After the storms subsided and the atmosphere der among the background of the stars. Because cleared up, Mariner 9 was able to map the entire of its reddish color as seen by the naked eye, Mars Martian surface with a surface resolution of 1 9 drew attention. It has been the subject of scientif- kilometer. ic and fictiona13 interest for centuries.4 In recent Images from Mariner 9 revealed surface fea- years, planetary scientists have developed in- tures far beyond what investigators had expected creased interest in Mars, because Mars is the from the earlier flybys. The earlier spacecraft had most Earthlike of the planets. “The study of Mars by chance photographed the heavily cratered is [therefore] an essential basis for our under- southern hemisphere of the planet, which looks standing of the evolution of the Earth and the more like the Moon than like Earth. These first inner solar system.”5 closeup images of Mars gave scientists the false Planetary exploration has been one of the Na- impression that Mars was a geologically “dead” tional Aeronautics and Space Administration’s planet, in which asteroid impacts provided the (NASA) primary goals ever since the U.S. -
Moon-Miners-Manifesto-Mars.Pdf
http://www.moonsociety.org/mars/ Let’s make the right choice - Mars and the Moon! Advantages of a low profile for shielding Mars looks like Arizona but feels like Antarctica Rover Opportunity at edge of Endeavor Crater Designing railroads and trains for Mars Designing planes that can fly in Mars’ thin air Breeding plants to be “Mars-hardy” Outposts between dunes, pulling sand over them These are just a few of the Mars-related topics covered in the past 25+ years. Read on for much more! Why Mars? The lunar and Martian frontiers will thrive much better as trading partners than either could on it own. Mars has little to trade to Earth, but a lot it can trade with the Moon. Both can/will thrive together! CHRONOLOGICAL INDEX MMM THEMES: MARS MMM #6 - "M" is for Missing Volatiles: Methane and 'Mmonia; Mars, PHOBOS, Deimos; Mars as I see it; MMM #16 Frontiers Have Rough Edges MMM #18 Importance of the M.U.S.-c.l.e.Plan for the Opening of Mars; Pavonis Mons MMM #19 Seizing the Reins of the Mars Bandwagon; Mars: Option to Stay; Mars Calendar MMM #30 NIMF: Nuclear rocket using Indigenous Martian Fuel; Wanted: Split personality types for Mars Expedition; Mars Calendar Postscript; Are there Meteor Showers on Mars? MMM #41 Imagineering Mars Rovers; Rethink Mars Sample Return; Lunar Development & Mars; Temptations to Eco-carelessness; The Romantic Touch of Old Barsoom MMM #42 Igloos: Atmosphere-derived shielding for lo-rem Martian Shelters MMM #54 Mars of Lore vs. Mars of Yore; vendors wanted for wheeled and walking Mars Rovers; Transforming Mars; Xities -
Comparative Study of Aerial Platforms for Mars Exploration
Comparative Study of Aerial Platforms for Mars Exploration Thesis by Nasreen Dhanji Department of Mechanical Engineering McGill University Montreal, Canada October 2007 A Thesis submitted to McGill University in partial fulfillment of the requirements for the degree of Master of Engineering © Nasreen Dhanji, 2007 Library and Bibliotheque et 1*1 Archives Canada Archives Canada Published Heritage Direction du Branch Patrimoine de I'edition 395 Wellington Street 395, rue Wellington Ottawa ON K1A0N4 Ottawa ON K1A0N4 Canada Canada Your file Votre reference ISBN: 978-0-494-51455-9 Our file Notre reference ISBN: 978-0-494-51455-9 NOTICE: AVIS: The author has granted a non L'auteur a accorde une licence non exclusive exclusive license allowing Library permettant a la Bibliotheque et Archives and Archives Canada to reproduce, Canada de reproduire, publier, archiver, publish, archive, preserve, conserve, sauvegarder, conserver, transmettre au public communicate to the public by par telecommunication ou par Plntemet, prefer, telecommunication or on the Internet, distribuer et vendre des theses partout dans loan, distribute and sell theses le monde, a des fins commerciales ou autres, worldwide, for commercial or non sur support microforme, papier, electronique commercial purposes, in microform, et/ou autres formats. paper, electronic and/or any other formats. The author retains copyright L'auteur conserve la propriete du droit d'auteur ownership and moral rights in et des droits moraux qui protege cette these. this thesis. Neither the thesis Ni la these ni des extraits substantiels de nor substantial extracts from it celle-ci ne doivent etre imprimes ou autrement may be printed or otherwise reproduits sans son autorisation. -
2016 Publication Year 2020-06-03T14:13:16Z Acceptance
Publication Year 2016 Acceptance in OA@INAF 2020-06-03T14:13:16Z Title Small Mars satellite: a low-cost system for Mars exploration Authors Pasolini, Pietro; Aurigemma, Renato; Causa, Flavia; Dell'Aversana, Pasquale; de la Torre Sangrà, David; et al. Handle http://hdl.handle.net/20.500.12386/25908 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016. Copyright ©2016 by the International Astronautical Federation (IAF). All rights reserved. IAC-16-A3.3A.6 SMALL MARS SATELLITE: A LOW-COST SYSTEM FOR MARS EXPLORATION Pasolini P.*a, Aurigemma R.b, Causa F.a, Cimminiello N.b, de la Torre Sangrà D.c, Dell’Aversana P.d, Esposito F.e, Fantino E.c, Gramiccia L.f, Grassi M.a, Lanzante G.a, Molfese C.e, Punzo F.d, Roma I.g, Savino R.a, Zuppardi G.a a University of Naples “Federico II”, Naples (Italy) b Eurosoft srl, Naples (Italy) c Space Studies Institute of Catalonia (IEEC), Barcelona (Spain) d ALI S.c.a.r.l., Naples (Italy) e INAF - Astronomical Observatory of Capodimonte, Naples (Italy) f SRS E.D., Naples (Italy) g ESA European Space Agency, Nordwijk (The Netherlands) * Corresponding Author Abstract The Small Mars Satellite (SMS) is a low-cost mission to Mars, currently under feasibility study funded by the European Space Agency (ESA). The mission, whose estimated cost is within 120 MEuro, aims at delivering a small Lander to Mars using an innovative deployable (umbrella-like) heat shield concept, known as IRENE (Italian ReEntry NacellE), developed and patented by ALI S.c.a.r.l., which is also the project's prime contractor. -
§130.417. Scientific Research and Design TEKS Overview 2020 Texas High School Aerospace Scholars Online Curriculum
§130.417. Scientific Research and Design TEKS Overview 2020 Texas High School Aerospace Scholars Online Curriculum # of Activities Standard # Standa rd Aligned (c)(2) The student, for at least 40% of instructional time, conducts laboratory and field investigations using safe, environmentally appropriate, and ethical practices. The student is expected to: 130.417.c2A (2A) demonstrate safe practices during laboratory and field investigations; and 18 (2B) demonstrate an understanding of the use and conservation of resources and the proper disposal 130.417.c2B or recycling of materials. 18 (c)(3) The student uses scientific methods and equipment during laboratory and field investigations. The student is expected to: (3A) know the definition of science and understand that it has limitations, as specified in subsection 130.417.c3A (b)(4)* of this section; 29 (3B) know that scientific hypotheses are tentative and testable statements that must be capable of being supported or not supported by observational evidence. Hypotheses of durable explanatory power 130.417.c3B which have been tested over a wide variety of conditions are incorporated into theories; 29 (3C) know that scientific theories are based on natural and physical phenomena and are capable of being tested by multiple independent researchers. Unlike hypotheses, scientific theories are well- established and highly-reliable explanations, but may be subject to change as new areas of science and 130.417.c3C new technologies are developed; 10 130.417.c3D (3D) distinguish between scientific -
Abstract - MESUR Pathfinder Mission Operations Concepts $
.$’ Abstract - MESUR Pathfinder Mission Operations Concepts $. The Mars Environmental Survey (MESUR) Pathfinder Project plans a December 1996 launch of a single spacecraft. The 7-month cruise includes up to four trajectory correction maneuvers (TCMS) and two checkouts of the complete flight system, one just after launch and one just before arrival at Mars. After jettisoning a cruise stage, an entry body containing a lander and microrover will directly enter the Mars atmosphere and parachute to a hard landing near the sub-solar latitude of 15 degrees North in July 1997. Primary surface operations last for 30 days, As a Discovery mission, MESUR Pathfinder costs are capped. Cost estimates for Pathfinder ground systems development and operations are not only lower in absolute dollars, but also are a lower percentage of total project costs than in past planetary missions. Operations teams will be smaller and fewer than typical flight projects. All experiment functions, including rover technology experiments, are collected in one Experiment Team. All engineering functions (exclusive of multimission services) are collected into a single Engineering Team. Operations with two small teams is made possible by the following characteristics: Acceptance of more risk as a Class C mission. Rover operations using simple high-level behavior commands. A simple spin-stabilized flight system. Telemetry collection of engineering and experiment data packets by demand into solid state memory. ● Direct-to-Earth telemetry driven only by downlink data rate and independent of collection rate. Prioritized packet downlink determined by ground command parameters. Onboard management of computer memory. No complex navigation data types. No cruise science and limited surface experiments. -
The Origins of the Discovery Program, 1989-1993
Space Policy 30 (2014) 5e12 Contents lists available at ScienceDirect Space Policy journal homepage: www.elsevier.com/locate/spacepol Transforming solar system exploration: The origins of the Discovery Program, 1989e1993 Michael J. Neufeld National Air and Space Museum, Smithsonian Institution, United States article info abstract Article history: The Discovery Program is a rarity in the history of NASA solar system exploration: a reform program that Received 18 October 2013 has survived and continued to be influential. This article examines its emergence between 1989 and Accepted 18 October 2013 1993, largely as the result of the intervention of two people: Stamatios “Tom” Krimigis of the Johns Available online 19 April 2014 Hopkins University Applied Physics Laboratory (APL), and Wesley Huntress of NASA, who was Division Director of Solar System Exploration 1990e92 and the Associate Administrator for Space Science 1992 Keywords: e98. Krimigis drew on his leadership experience in the space physics community and his knowledge of Space history its Explorer program to propose that it was possible to create new missions to the inner solar system for a NASA Space programme organization fraction of the existing costs. He continued to push that idea for the next two years, but it took the influence of Huntress at NASA Headquarters to push it on to the agenda. Huntress explicitly decided to use APL to force change on the Jet Propulsion Laboratory and the planetary science community. He succeeded in moving the JPL Mars Pathfinder and APL Near Earth Asteroid Rendezvous (NEAR) mission proposals forward as the opening missions for Discovery. But it took Krimigis’s political skill and access to Sen.