AN ANIMATED OVERVIEW of PLANETARY ROBOTICS: Past, Present and Future

Total Page:16

File Type:pdf, Size:1020Kb

AN ANIMATED OVERVIEW of PLANETARY ROBOTICS: Past, Present and Future 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) AN ANIMATED OVERVIEW OF PLANETARY ROBOTICS: Past, Present and Future Michel Van Winnendael*, Francesco Grassini*, James Garry**, Gianfranco Visentin* *European Space Agency, Automation and Robotics Section **Planetary and Space Sciences Research Institute, Open University, Milton Keynes, UK ASTRA 2002 19-21 November 2002 Issue 2 ESTEC, Noordwijk, The Netherlands Automation and Robotics Section (TOS-MMA) Introduction The subject of this slide show is planetary robotics, defined as “systems which provide manipulation and/or mobility functions, which moreover have a certain flexibility to perform a variety of tasks, and which are designed to operate on or near the surface of celestial bodies”. Typically these functions consist of moving around on celestial bodies (on, above or under the surface), transporting, loading/ unloading and positioning items on the surface of a planet, moon, asteroid or comet nucleus. We have made a (necessarily subjective) selection of missions and developments which we consider most relevant in the frame of planetary robotics. ASTRA 2002 19-21 November 2002 ESTEC, Noordwijk, The Netherlands 1 1 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Rover Categories For classification of planetary rovers we use the following definitions: • “large rovers” from few 100s kg to ~1000 kg • “mini rovers” from few 10s kg to ~100 kg • “micro rovers” from a few kg to ~10 kg e.g Marsokhod, Russia 1990’s e.g. MUSES-CN, NASA/JPL R&D • “nano rovers” from 10s of g e.g. Nanokhod (ESA R&D 1999) to ~1 kg e.g. Lunokhods, Russia 1970 e.g. Sojourner NASA/JPL 1997 ASTRA 2002 19-21 November 2002 ESTEC, Noordwijk, The Netherlands Automation and Robotics Section (TOS-MMA) Past Activities and Missions under Development ASTRA 2002 19-21 November 2002 ESTEC, Noordwijk, The Netherlands 2 2 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Luna 16, 20, 24 Russia (1970-1976) Luna 16, Luna 20, Luna 24: Lunar Sample Return, returned Lunar soil sample to Earth (100g on Luna 16 in 1970, 30 g on Luna 20 in 1972, 170 g on Luna 24 in 1976)) Luna 16 lander with arm and drilling rig (Credit: NPO Lavochkin / NASA NSSDC) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Luna 16, 20, 24 Russia (1970-1976) Luna 16, Luna 20, Luna 24: Lunar Sample Return, returned Lunar soil sample to Earth (100g on Luna 16 in 1970, 30 g on Luna 20 in 1972, 170 g on Luna 24 in 1976) Luna 16 sample return (Credit:CD 'Soviets in Space‘ by “Compact Book Publishing Co, Moscow”) 1970 1980 1990 2000 2010 2020 2030 3 3 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Luna 16, 20 & 24 Russia (1970-1976) Luna 16, Luna 20, Luna 24: Lunar Sample Return, returned Lunar soil sample to Earth (100g on Luna 16 in 1970, 30 g on Luna 20 in 1972, 170 g on Luna 24 in 1976) Luna24 sample return 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Luna 17 & 21 Russia (1970-1973) Luna 17: carried the Lunokhod 1 rover, the first rover on another world, which traveled 10 km on the Lunar Surface (Nov. 1970- Oct. 1971) Luna 21: carried the Lunokhod 2 rover, which covered 37 km of terrain (Jan 1973-Jun 1973) Lunokhod 1 on lander before deployment (Credit: NPO Lavochkin) 1970 1980 1990 2000 2010 2020 2030 4 4 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Luna 17 & 21 Russia (1970-1973) Luna 17: carried the Lunokhod 1 rover, the first rover on another world, which traveled 10 km on the Lunar Surface (Nov. 1970- Oct. 1971) Luna 21: carried the Lunokhod 2 rover, which covered 37 km of terrain (Jan 1973-Jun 1973) Lunokhod mobility system testing (Credit: VNII Transmash) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Luna 17 & 21 Russia (1970-1973) Luna 17: carried the Lunokhod 1 rover, the first rover on another world, which traveled 10 km on the Lunar Surface (Nov. 1970- Oct. 1971) Luna 21: carried the Lunokhod 2 rover, which covered 37 km of terrain (Jan 1973-Jun 1973) Lunokhod Operation (Credit:CD 'Soviets in Space‘ by “Compact Book Publishing Co, Moscow”) 1970 1980 1990 2000 2010 2020 2030 5 5 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Luna 17 & 21 Russia (1970-1973) Luna 17: carried the Lunokhod 1 rover, the first rover on another world, which traveled 10 km on the Lunar Surface (Nov. 1970- Oct. 1971) Luna 21: carried the Lunokhod 2 rover, which covered 37 km of terrain (Jan 1973-Jun 1973) Lunokhod Control Station (Credit: NPO Lavochkin / The Planetary Society) Lunokhod 2 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) LRV APOLLO USA (1971-1972) Lunar Roving Vehicle, a foldable 208 kg rover, designed to transport 2 astronauts, scientific equipment and lunar samples LRV-1 on Apollo 15 (1971) LRV-2 on Apollo 16 (1972) LRV-3 on Apollo 17 (1972) The various LRV parts LRV-1 onLRV Apollo-1 on 15,Apollo with 15 astronaut (Credit: (Credit:NASA) NASA) LRV with astronaut (Credit: NASA) LRV wheel (Credit: NASA) LRV Control Console (Credit: NASA) 1970 1980 1990 2000 2010 2020 2030 6 6 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Mars2, Mars 3 ProP-M Russia (1971) The Mars2 and Mars3 landers both carried a ski-walking microrover called ProP-M, which was attached to the lander by means of a tether cable. They both arrived during a big martian dust storm. Mars2 crashed. The Mars3 landing succeeded but after 20 s the communication was lost. ProP-M microrover (Credit: VNII Transmash) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Mars2, Mars 3 ProP-M Russia (1971) The Mars2 and Mars3 landers both carried a ski-walking microrover called ProP-M, which was attached to the lander by means of a tether cable. They both arrived during a big martian dust storm. Mars2 crashed. The Mars3 landing succeeded but after 20 s the communication was lost. ProP-M deployment simulation (Credit:CD 'Soviets in Space‘ by “Compact Book Publishing Co, Moscow”) 1970 1980 1990 2000 2010 2020 2030 7 7 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Viking USA (1975-1982) First successful soft landings at two locations on the Martian surface. Both landershad a furlable boom with a soil scoop to collect surface samples. Viking Orbiters (Credit: NASA/JPL) Vikingimage Lander of trench with made stowed by the furlable soil scoopboom (Credit: (Credit: NASA/JPL) NASA/JPL) Viking Lander withsoil deployed scoop (Credit: furlable NASA/JPL)boom (Credit: NASA/JPL) Viking 1 in cleanroom(Credit: NASA/JPL) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Phobos2 Phobos Hopper Russia (1988-1989) The Phobos2 spacecraft carried a small “hopper” lander, called ProP-F, designed to land on Phobos (one of the moons of Mars). Contact with the spacecraft was lost shortly before release of the hopper and another lander. ProP-F (Credit: VNII Transmash) 1970 1980 1990 2000 2010 2020 2030 8 8 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) Phobos2 Phobos Hopper Russia (1988-1989) The Phobos2 spacecraft carried a small “hopper” lander, called ProP-F, designed to land on Phobos (one of the moons of Mars). Contact with the spacecraft was lost shortly before release of the hopper and another lander. ProP-F in operation (simulation) (Credit: James Garry) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) M94-M96 Marsokhod Russia (1990-1995) In view of a planned ambitious mission the Russians developed a minirover for Mars surface operations, called Marsokhod. The mission was repeatedly postponed and finally cancelled. Marsokhod testing in USA, 1996 (Credit: NASA) Marsokhod testing in USA, 1996 (Credit: NASA) The M94 Marsokhod (Credit: VNII Transmash) 1970 1980 1990 2000 2010 2020 2030 9 9 7th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2002' ESTEC, Noordwijk, The Netherlands, November 19 - 21, 2002 Automation and Robotics Section (TOS-MMA) M94-M96 Marsokhod Russia (1990-1995) In view of a planned ambitious mission the Russians developed a minirover for Mars surface operations, called Marsokhod. The mission was repeatedly postponed and finally cancelled. Marsokhod testing in Kamchatka, Russia (Credit: VNII Transmash) 1970 1980 1990 2000 2010 2020 2030 Automation and Robotics Section (TOS-MMA) Mars Pathfinder Sojourner Rover USA (1996-1997) Mars lander using airbag technology. The first successful Mars landing since Viking. Deployed a micro-rover called “Sojourner”.
Recommended publications
  • 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.
    [Show full text]
  • On Orbital Debris JEFF FOUST, COLLEGE PARK, Md
    NOVEMBER 24, 2014 SPOTLIGHT Clyde Space See page 12 www.spacenews.com VOLUME 25 ISSUE 46 $4.95 ($7.50 Non-U.S.) PROFILE/22> YVONNE PENDLETON DIRECTOR, SOLAR SYSTEM EXPLORATION RESEARCH VIRTUAL INSTITUTE INSIDE THIS ISSUE LAUNCH INDUSTRY Swift Development of Ariane 6 Urged Applauding the end of a French-German impasse over the Ariane 6 rocket, the European Satellite Operators Association said the vehicle needs to be in service as quickly as possible. See story, page 8 ATK Hints at Antares Engine Selection Alliant Techsystems Chief Executive Mark DeYoung said there are no near-term liquid- propulsion alternatives to Russian engines for U.S. rockets. See story, page 6 ESA PHOTO Virginia May Seek Federal Funds for Wallops > “We have found a compromise that is OK for both countries, for the other participating states and also for industry,” Brigitte Zypries (above), Germany’s Virginia’s two U.S. senators said they may seek federal funds to cover $20 million in repairs to the space minister, said of an agreement under which Germany and France will back the Ariane 6 rocket and scrap the Ariane 5 Midlife Evolution. Wallops Island launch pad damaged when Orbital Sciences’ Antares exploded. See story, page 6 MILITARY SPACE Protected Tactical Waveform Taking Shape German-French Compromise The U.S. Air Force is expected to demonstrate its protected tactical waveform in new modems and reworked terminals as early as 2018. See story, page 11 U.S. To Grant Indirect Access to Space Fence Paves Direct Path to Ariane 6 The Pentagon’s international space surveillance partners will have indirect access to data from the Air Force’s next-generation Space Fence tracking system.
    [Show full text]
  • 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.
    [Show full text]
  • Autonomous Navigation and the Sojourner Microrover
    rtRR.31. lYYf3 5: 4“(7-TI 5L1FLNCE RRIWROD NO. >y~ 1-’.1313 m TI-113PATNFINDERIVWSIONmhf.ms tbas@iweofMarostthetime the d F ; Iandar completed sun-finding and identifi 3 the cliraetion of mrirtiannorth on 90! 1. Int$ 4 Autonomous Navigation and the madkfe wqqmints (ss needed) were also de- tined by the driver if them was a preferent$l : Sojourner Microrover path toward the fml dcstindors (such ss a 7 . route to avoid obvious hazsrds along t$e 8 path). If the rover was not slreody faoing e 9 J. Matijevic next waypoinL it was carunandsd to 10 toward tbe god until it facd the destination+ 11 These oommnds (W30to Waypointfl tuqs, 12 and a command to update the position of e TtM Mars ex@xation program has as an ing, the rover used teobniques for aukmo- rover in the x and y coordinate tie) w e i: ovmamhingtheme tho mamh for md under- mous control which were (among sewed sent to tho rovor as part of a single c d stnnding of life, climate, and resou.moson technologies)tkst damonstrate$in flight on sequence. 4 15 16 this fascinating planet. The abfiity to move this mission. One such technique for Upon exeoution of tha “Go to Waypo”mt” 17 aboutthe surfiiof Mars is key to makb autonomow navigation and hszad avoidance cunmand the rover drove an appmxirrde 18 measuremcmtsand the gathuirtg of tha straight lina, ac@9& - its ps data which address this therm (J). In Oc- when it datacted drifi off ils co c ;: tober 1992, the NASA Office of Spaea or enoountoreda tid condili 21 Access and kbno]o~ fdod an ex- king cxooutionof a “Go to Wai - 22 periment to d~nsti~ the mobile vti- point” eomrnsnd,the rover updstdd 23 ck technologiesneeded for a Msrs surl%oc its position relntive to the lander {o 24 mission (2), lllat exporimlmh the Micro- dexarmine(at a mioirnurn) if it ~d rover Flight Expmimcnt (MJ?EX) or reaohed the objeotivc of the trsy- : “So@mer;’ flew on tbe Mars Pathfinder erse.
    [Show full text]
  • 350 International Atlas of Lunar Exploration 8 January 1973
    :UP/3-PAGINATION/IAW-PROOFS/3B2/978«52181«5(M.3D 350 [7428] 19.8.20073:28PM 350 International Atlas of Lunar Exploration 8 January 1973: Luna 21 and Lunokhod 2 (Soviet Union) The 4850 kg Luna 21 spacecraft was launched from Baikonur at 06:56 UT on a Proton booster, placed in a low Earth parking orbit and then put on a lunar trajec­ tory. Power problems required that the Lunokhod solar panel be opened in flight to augment power, and stowed again for the trajectory correction and orbit insertion burns and for landing. On 12 January Luna 21 entered a 90 km by 100 km lunar orbit inclined 60° to the equator. After a day in orbit the low point was reduced to 16 km, and on 15 January after 40 orbits the vehicle braked and dropped to just 750 m above the surface. Then the main thrusters slowed the descent, and at :UP/3-PAGINATION/IAW-PROOFS/3B2/978«52181«5(M.3D 351 [7428] 19.8.20073:28PM Chronological sequence of missions and events 351 22 m a set of secondary thrusters took over until the After landing, Lunokhod 2 surveyed its surround­ spacecraft was only 1.5 meters high, when the thrusters ings. A rock partly blocked the west-facing ramp so the were shut off. Landing time was 23:35 UT. rover was driven east across a shallow crater, leaving the The site was in Le Monnier crater on the eastern edge lander at 01:14 UT on 16 January. It rested 30 m from of Mare Serenitatis, 180 km north of the Apollo 17 land­ the descent stage to recharge its batteries until 18 ing site, at 25.85° N, 30.45° E (Figure 327A).
    [Show full text]
  • MT Aerospace (Germany)
    https://ntrs.nasa.gov/search.jsp?R=20080014278 2019-08-30T04:19:50+00:00Z European Directions for Hypersonic Thermal Protection Systems and Hot Structures 31st Annual Conference on Composites Materials and Structures Daytona Beach, FL January 22, 2007 David E. Glass NASA Langley Research Center, Hampton, VA 23681 Approved for Public Release, Distribution Unlimited Agenda ♦ Background • Comments on prior ESA workshop • X-38 • Hopper ♦ Flight Vehicle Based Technology Development • IXV (ESA) • EXPERT (ESA) • USV (Italy) • SHEFEX (Germany) • SHyFE (UK) • LEA (France) • Foton (Russia) ♦ Non-Vehicle Specific Technology ♦ Concluding Remarks 2 European TPS and Hot Structures Research and Development ♦TPS and hot structures research and development critical for future space vehicles ♦Developing next generation TPS and hot structures technology (not Space Shuttle derived technology) ♦Long-term funding based on technology needs ♦Wide industry support and commitment to X-38 program ♦Test facilities developed for TPS and hot structures development • Thermal/structural test chamber • Arc-jet tunnels developed in recent years ♦Technology development has broad base • Fabrication • Testing • Large components • Fasteners • Bearings • Oxidation protection • Damage repair • Life cycle Wayne Sawyer comments from previous ESA TPS & Hot Structures Workshop 3 European TPS and Hot Structures Research and Development ♦ Proposing numerous experimental launch vehicles dedicated to or with TPS and hot structures research of prime consideration ♦ Committing significant
    [Show full text]
  • Mission Analysis and Preliminary Re-Entry Trajectory Design of the DLR Reusability Flight Experiment Refex
    8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Mission Analysis and Preliminary Re-entry Trajectory Design of the DLR Reusability Flight Experiment ReFEx Sven Stappert*, Peter Rickmers*, Waldemar Bauer*, Martin Sippel* *German Aerospace Center (DLR), Institute of Space Systems, Robert-Hooke-Straße 7, 28359 Bremen [email protected], [email protected], [email protected], [email protected] Abstract Driven by the recently increased demand for investigating reusable launchers, the German Aerospace Center (DLR) is currently developing the Reusability Flight Experiment (ReFEx). The goal is to demonstrate the capability of performing an atmospheric re-entry, representative of a possible future winged reusable stage, and to develop and test key technologies for such reusable stages. The flight demonstrator ReFEx shall perform a controlled and autonomous re-entry from hypersonic velocity of approximately Mach 5 down to subsonic velocity after separation from the VSB-30 booster. The focus of this paper is the re-entry trajectory design for the ReFEx mission. Abbreviations AoA Angle of Attack AVS Avionics BC Ballistic Coefficient BoGC Begin of Guided Control CALLISTO Cooperative Action Leading to Launcher Innovation in Stage Tossback Operation DOF Degree of Freedom ELV Expendable Launch Vehicle EoE End Of Experiment GNC Guidance, Navigation and Control L/D Lift-to-Drag Ratio FPA Flight Path Angle LFBB Liquid Fly-Back Booster MECO Main Engine Cut-Off RCS Reaction Control System RLV Reusable Launch Vehicle TOSCA Trajectory Optimization and Simulation of Conventional and Advanced Spacecraft VTHL Vertical Takeoff, Horizontal Landing VTVL Vertical Takeoff, Vertical Landing 1. Introduction The recent successes of the emerging private space companies SpaceX and Blue Origin in landing, recovering and relaunching reusable first stages have demonstrated the possibility of building reliable and competitive reusable first stages.
    [Show full text]
  • Three Women Who Dared Rabbi Van Lanckton Temple B’Nai Shalom Braintree, Massachusetts March 4, 2017
    Three Women Who Dared Rabbi Van Lanckton Temple B’nai Shalom Braintree, Massachusetts March 4, 2017 Be happy, it’s Adar! The new month of Adar began last Monday. Next weekend, we celebrate Purim. Spring is finally almost here. In addition to sending sh’lach manot and eating hamentaschen and dressing up in costumes, the central celebration of Purim is the public reading of the Book of Esther, Megillat Esther. Esther is the prime example of a woman who dared. She dared to speak up to King Achashverosh. She dared to enter his throne room without his permission, risking death. She accused Haman, powerful counselor to the king, of plotting to kill the Jews. In doing so, she revealed to the king that she, herself, was Jewish. If she had failed, she would have shared in the fate of all the Jews of Persia in being killed by Haman and his followers. Before these exploits, Esther was unsure what to do. Her uncle Mordecai urged her to use her position as queen to save the Jews. We need to back up a little in the story to understand the exchange between Mordecai and Esther and the key line in that exchange that still speaks to us today. Megillat Esther tells us that the king had promoted Haman and seated him higher than any of his fellow officials. All the king’s courtiers knelt and bowed low to Haman according to the king’s order, but Mordecai would not kneel or bow low. He refused to do so, he said, because he was a Jew.
    [Show full text]
  • Dr. Sergei Fedorovich Teselkin Lavochkin Association, Russian Federation, [email protected]
    69th International Astronautical Congress 2018 Paper ID: 44581 oral IAF SPACE EXPLORATION SYMPOSIUM (A3) Solar System Exploration (5) Author: Dr. Sergei Fedorovich Teselkin Lavochkin Association, Russian Federation, [email protected] \TO VENUS TOGETHER": RUSSIAN-AMERICAN JOINT ENCORE OF VENUS RESEARCHES WITH ORBITER, LANDER AND ATMOSPHERIC PROBES IN THE PROJECT \VENUS-D" Abstract S. Lemeshevskii, Candidate of Economics, [email protected] O. Grafodatskiy, Doctor of Engineering Sci- ence,[email protected] Kh.Karchaev, Candidate of Economics, [email protected] S. Teselkin, Candi- date of PhysicsMathematics,[email protected] V. Vorontsov, Doctor of Engineering Science, [email protected] Lavochkin Association, Russia Mission "Venera-D" by Lavochkin Association implies a long-term study of Venus. International pay- load is to be installed on orbiter, lander and long-living station on Venus surface. The project is a basis for further large-scale international missions to Venus, previously carried out in 1960-80s and early 1990s by Soviet and American spacecraft. A large amount of data on structure, soil composition, atmosphere, cloud layers, wind speed on the surface were accumulated. Soviet Venus research program was completed in 1986 by landing of \VEGA" (Venus-Halley's comet), one of the most successful projects in Lavochkin history. Since 1994 (mapping with the NASA Magellan mission) Venus was studied by two spacecraft: \Venus Express" (ESA, 2005-2014) and \Akatsuki" (JAXA, launch - 2010, start of operation - 2015). The first steps of \Venera-D" appeared in the early 2000s with the idea to provide operations on the planet's surface for several hours and possibly days. With the latest developments, unification of design solutions and new technical tools used in-house Lavochkin experts consider the mission \VEGA" as a prototype for the next automatic interplanetary station destined to Venus.
    [Show full text]
  • L. Summerera,∗, A. Galvezb, D. Izzoa, F
    64nd International Astronautical Congress, Beijing, China. Copyright 2013 by ESA. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-13.E.6.1.6 COMPETITIONS, GAMES AND PRIZES - MEANS FOR ADVANCED SPACE RESEARCH? L. Summerera,∗, A. Galvezb, D. Izzoa, F. Salzgeberc, A. de Clercqc, P. Manesc aESA Advanced Concepts Team, Keplerlaan 1, 2201 Noordwijk, The Netherlands bESA General Studies Programme, rue Mario Nikis, 75015 Paris, France cESA Technology Transfer Programme, Keplerlaan 1, 2201 Noordwijk, The Netherlands Abstract The traditional main mechanisms to advance science and technology in the space sector have recently been complemented by the use of competitions, prizes and games. Historically competitions and ex-ante prizes have played an important role among the tools of governments to stimulate innovation and advance science and technologies. Triggered by the success of the Ansari X-Prize in late 1990s / early 2000, these mechanisms have steadily gained grounds and supporters, also among governments. Scholarly literature on the effectiveness, advantages and disadvantages of these methods is emerging but still scarce. Most of the available scholarly literature assesses their impact based on US case studies and examples. The present paper provides a first analysis of these mechanisms and tools within the European Space Agency (ESA), based on three different areas: scientific research within its Advanced Concepts Team, business and innovation oriented competitions and prizes within the technology transfer programme and system level studies within the General Studies Programme. The ESA Advanced Concepts Team has experimented and used new ways of engaging with the larger scientific community via the use of scientific competitions, online games and scientific crowdsourcing experiments.
    [Show full text]
  • 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.
    [Show full text]
  • Jacques Tiziou Space Collection
    Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through
    [Show full text]