China's Touch on the Moon
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Ice& Stone 2020
Ice & Stone 2020 WEEK 34: AUGUST 16-22 Presented by The Earthrise Institute # 34 Authored by Alan Hale This week in history AUGUST 16 17 18 19 20 21 22 AUGUST 16, 1898: DeLisle Stewart at Harvard College Observatory’s Boyden Station in Arequipa, Peru, takes photographs on which Saturn’s outer moon Phoebe is discovered, although the images of Phoebe were not noticed until the following March by William Pickering. Phoebe was the first planetary moon to be discovered via photography, and it and other small planetary moons are discussed in last week’s “Special Topics” presentation. AUGUST 16, 2009: A team of scientists led by Jamie Elsila of the Goddard Space Flight Center in Maryland announces that they have detected the presence of the amino acid glycine in coma samples of Comet 81P/ Wild 2 that were returned to Earth by the Stardust mission 3½ years earlier. Glycine is utilized by life here on Earth, and the presence of it and other organic substances in the solar system’s “small bodies” is discussed in this week’s “Special Topics” presentation. AUGUST 16 17 18 19 20 21 22 AUGUST 17, 1877: Asaph Hall at the U.S. Naval Observatory in Washington, D.C. discovers Mars’ larger, inner moon, Phobos. Mars’ two moons, and the various small moons of the outer planets, are the subject of last week’s “Special Topics” presentation. AUGUST 17, 1989: In its monthly batch of Minor Planet Circulars (MPCs), the IAU’s Minor Planet Center issues MPC 14938, which formally numbers asteroid (4151), later named “Alanhale.” I have used this asteroid as an illustrative example throughout “Ice and Stone 2020” “Special Topics” presentations. -
Exploration of the Moon
Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms. -
Contributions of a Lunar Geoscience Observer (Lgo) Mission to Fundamental Questions in Lunar Science
CONTRIBUTIONS OF A LUNAR GEOSCIENCE OBSERVER (LGO) MISSION TO FUNDAMENTAL QUESTIONS IN LUNAR SCIENCE by LGO SCIENCE WORKSHOP MEMBERS Contributions Lunar Geoscience Observer Mission Frontispiece: Earth-rise over the lunar highlands. Contributions of a Lunar Geoscience Observer Mission to Fundaments Questions in Lunar Science LGO Science Workshop Members March LGO Science Workshop Members Roger Phillips (Chair), Southern Methodist University Merton Davies, Rand Coworation Michael Drake, University of Arizona Michael Duke, Johnson Space Center Larry Haskin. Washington University James Head, Brown University Eon Mood, University of Arizona Robert Lin, University of California, Berkeley Duane Muhleman, California Institute of Technology Doug Nash (Study Scientist), Jet Propulsion Laboratory Carle Pieters, Brown University Bill Sjogren, Jet Propulsion Laboratory Paul Spudis, U .S. Geological Survey Jeff Taylor, University of New Mexico Jacob Trombka, Goddard Space Flight Center This report was compiled and prepared in the Department of Geological Sciences and the AnthroGraphics Laboratory of Southern Methodist University. Material in this document may be copied without restraint for library, abstract service, educational or personal research purposes. Republication of any portion should be accompanied by the appropriate acknowledgment of this document. For further information, contact: Dr. Roger Phillips Department of Geological Sciences Southern Methodist University Dallas, TX 75275 Executive Summary THE IMPORTANCE OF LUNAR SCIENCE STATUS OF LUNAR SCIENCE DATA AND THEORY The Moon is the keystone in the interlinked knowledge that forms the foundation of our understanding of the silicate Unlike other solar system bodies beyond Earth, the Moon bodies of the solar system. The Moon is remarkable in that it has been intensely studied by telescope, unmanned space- remains the only other planet for which we have samples of crafi and manned missions. -
To the Moon and Beyond! Article
3/12/2020 Achieve3000: Lesson Printed by: Jessica Christian Printed on: March 12, 2020 To the Moon and Beyond! Article PART 1 NEW DELHI, India. Both India and China are moving ahead in space exploration. Both countries launched space missions in 2013. India's Mars Orbiter Mission (MOM) was sent to Mars in November. China's Chang'e 3 spaceship blasted off on its way to the moon in December. India India launched its first spacecraft bound for Mars on November 5, 2013. The craft spent almost a month in Earth's orbit. Then, on November 30, 2013, the orbiter went on its way to the Red Planet. "The Earth orbiting phase of the spacecraft ended. The spacecraft is now on a course to reach Mars after a journey of about 10 months around the sun," the Indian Space Research Organisation (ISRO) said in early December. The 3,000-pound (1,350-kilogram) orbiter is called Mangalyaan. That means "Mars craft" in Hindi. It must travel 485 million miles (780 million Photo credit and all related images: kilometers) to reach an orbit around Mars. It will take about 300 days. It is Arun Sankar K/AP expected to do this by September 2014. This is the Satish Dhawan Space Center in southern India. India sent its first spaceship to Mars in The orbiter will gather images and data. They will help in determining how November 2013. Martian weather systems work. India is also looking to MOM to figure out what happened to the large quantities of water that are believed to have once existed on Mars. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
The Moon Is a Harsh Chromatogram: the Most Strategic Knowledge Gap (Skg) at the Lunar Surface E
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 2766.pdf THE MOON IS A HARSH CHROMATOGRAM: THE MOST STRATEGIC KNOWLEDGE GAP (SKG) AT THE LUNAR SURFACE E. Patrick, R. Blase, M. Libardoni, Southwest Research Institute®, 6220 Culebra Rd., San Antonio, TX 78238 ([email protected]) Introduction: Data from analytical instruments de- a gas chromatograph mass spectrometer (GCMS) and ployed during multiple lunar missions, combined with revealed 97% of the composition in that mass channel laboratory results[1], suggest the regolith surface of the to be N2. Henderson et al.[5] also identified amino ac- Moon traps more volatiles in gas-surface interactions ids which were attributed to contamination, but results than is currently understood. We assert that the lunar from recent more sensitive LCMS and GCMS experi- surface behaves as a giant 3-D surface chromatogram, ments by Elsila et al.[1] found some amino acid and separating gas molecules by species as each wafts other organic signatures to be extraterrestrial in origin. across the regolith according to its mobility and ad- While these and other investigations suggest contami- sorption characteristics before eventually becoming nation from the Apollo spacecraft as a likely source for trapped. Herein we present supporting evicence for this a number of observed signatures[1,2,4,5], what is not claim. explained is the nature of the trapping mechanism for In gas chromatography (GC), components of a the N2 feature in 10086, and demonstrates gas retention sample are separated within a column according to from a gas that, under most circumstances, exhibits no their individual partitioning coefficients and by such retention at temperatures around 300 K[3]. -
Thermal Design, Analysis and Test Validation of Turksat-3Usat Satellite
Journal of Thermal Engineering, Vol. 7, No. 3, pp. 468-482, March, 2021 Yildiz Technical University Press, Istanbul, Turkey THERMAL DESIGN, ANALYSIS AND TEST VALIDATION OF TURKSAT-3USAT SATELLITE Murat Bulut1,*, Nedim Sözbir2 ABSTRACT When CubeSat projects are a useful means by which universities can engage their students in space-related activities. TURKSAT-3USAT is a three-unit amateur radio CubeSat jointly developed by the Space Systems Design and Test Laboratory and the Radio Frequency Electronics Laboratory of Istanbul Technical University (ITU), in collaboration with TURKSAT, A.S. company as well as the Turkish Amateur Technology Organization. It was launched on April 26, 2013 as a secondary payload on a CZ-2D rocket from China’s Jiuquan Space Center to an altitude of approximately 680 km. The mission of the satellite has two primary goals: (1) to voice communication at Low Earth Orbit (LEO) and (2) to educate students by providing hands-on experience. TURKSAT-3USAT was designed to sustain a circular, near sun-synchronous LEO, and has dimensions of 10 x 10 x 34 cm3. Within the course of this paper, TURKSAT-3USAT’s thermal control will be addressed. TURKSAT-3USAT’s thermal control model was developed using ThermXL and ESATAN-TMS software. Using this model, temperature distributions of the CubeSat when subjected to various experimental conditions of interest were computed. Using a thermal vacuum chamber (TVAC), thermal cycling and bake-out testing were carried out on the flight model to verify the thermal design performance and check the mathematical model. Based on thermal analysis results, the temperature of equipment was within the allowable temperature range except for the batteries that were between 42.56 oC and -20.31 oC. -
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T. Crofton Department of Aerospace & Ocean Engineering TEAM LEAD Allison Quinn STUDENT MEMBERS Ethan LeBoeuf Brian McLemore Peter Bradley Smith Amanda Swanson Michael Valosin III Vidya Vishwanathan FACULTY SUPERVISOR AIAA 2018 Undergraduate Spacecraft Design Dr. Kevin Shinpaugh Competition Submission i AIAA Member Numbers and Signatures Ethan LeBoeuf Brian McLemore Member Number: 918782 Member Number: 908372 Allison Quinn Peter Bradley Smith Member Number: 920552 Member Number: 530342 Amanda Swanson Michael Valosin III Member Number: 920793 Member Number: 908465 Vidya Vishwanathan Dr. Kevin Shinpaugh Member Number: 608701 Member Number: 25807 ii Table of Contents List of Figures ................................................................................................................................................................ v List of Tables ................................................................................................................................................................vi List of Symbols ........................................................................................................................................................... vii I. Team Structure ........................................................................................................................................................... 1 II. Introduction .............................................................................................................................................................. -
Comparisions of Ground Penetrating Radar Results at Chang’E-3 and Chang’E-4 Landing Sites
51st Lunar and Planetary Science Conference (2020) 1125.pdf COMPARISIONS OF GROUND PENETRATING RADAR RESULTS AT CHANG’E-3 AND CHANG’E-4 LANDING SITES. J. L. Lai1, Y. Xu1, X. P. Zhang1, L. Xiao1,2, Q. Yan1, X. Meng1, B. Zhou3, Z. H. Dong3, and D. Zhao3 1State Key Laboratory of Lunar and Planetary Sciences, Macau University of Science and Technology, Macau ([email protected]) , 2Planetary Science Institute, School of Earth Sciences, China University of Geosciences, Wu- han, China, 3Key Laboratory of Electromagnetic Radiation and Detection Technology, Institute of Electronics, Chinese Acade- my of Science, Beijing, China. Introduction: On 14 December 2013, Chang’e-3 (CE-3) landed at 340.49°E, 44.12°N in northern Mare Imbrium and released the Yutu rover. On 3 January 2019, Chang’e-4 (CE-4) landed at 177.588° E, 45.457° S (Statio Tianhe) in the Von Kármán crater of the SPA basin and released the Yutu-2 rover. The two rovers both equipped with ground-penetrating radars (hereaf- ter referred to as Lunar Penetrating Radar, LPR) pro- vide unique data sets of in situ measurements of the lunar regolith [1]. The aim of this work is to report the first five lunar days of CE-4 LPR results at 500 MHz and compare the results between the two sites. Chang’e-3 and Chang’e-4 Landing sites CE-3 probe landed in the Imbrium basin on bas- alts inferred as Eratosthenian in age. These represent some of the youngest units on the Moon at about 2.35- Figure 1 (a) The CE-3 landing site on TiO2 map 2.5 billion years (Gy) old[2], for instance compared derived from Lunar Reconnaissance Orbiter Camera with samples returned by the Apollo and Luna mis- (LROC) Wide-Angle Camera (WAC) images (Sato et sions. -
MODELING and SIMULATION of the CHANDRAYAAN-I HYSI DATA for MINERAL MIXING ANALYSIS. S.B. Sayyad and Mohammed Zeeshan R, (Departm
4th Planetary Data Workshop 2019 (LPI Contrib. No. 2151) 7074.pdf MODELING AND SIMULATION OF THE CHANDRAYAAN-I HYSI DATA FOR MINERAL MIXING ANALYSIS. S.B. Sayyad and Mohammed Zeeshan R, (Department of Physics, Milliya College Arts Science and Management Science College Beed Maharashtra India. [email protected], [email protected] ) Introduction: The space weathering is the primary process involved on the lunar surface which has the strong influence on the reflectance properties because of the accumulation of small submicroscopic iron [1- 2]. Long time exposure to the environment complicates the understanding of the surface composition [3-6] Theoretical model can be employed to understand the effect of space weathering and to study the composition of the lunar regolith. From the studies done on the lu- nar samples from the Apollo mission it was clear that there are the significant differences between the optical properties of spectra pulverized in the laboratory and spectra obtained from the lunar soil [7-9]. The lunar Fig. 1. Site Location of Mare Crisium and data subset of soil spectra shows systematic influence of space weath- Mare Crisium. ering which is reduction in overall reflectance red- dened -slope continuum and attenuated absorption bands. To model the measured reflectance spectra of Chandrayaan-1 hyperspectral Imager (HySI) we have obtained an artificial reflectance spectrum using Bi- directional reflectance function (BRDF) based on the equation of radiative transfer proposed by Bruce Hap- ke and published in the series of papers [10-14]. The effect of space weathering, particle size, single particle phase function, porosity can be easily accommodated and it is con- sidered to be most efficient for modeling asteroids and plane- tary surfaces Modeling the Chandrayaan-1 HySI dataset: The Band to band registered level-4 HySI image was Fig.2. -
Surveyor 1 Space- Craft on June 2, 1966 As Seen by the Narrow Angle Camera of the Lunar Re- Connaissance Orbiter Taken on July 17, 2009 (Also See Fig
i “Project Surveyor, in particular, removed any doubt that it was possible for Americans to land on the Moon and explore its surface.” — Harrison H. Schmitt, Apollo 17 Scientist-Astronaut ii Frontispiece: Landing site of the Surveyor 1 space- craft on June 2, 1966 as seen by the narrow angle camera of the Lunar Re- connaissance Orbiter taken on July 17, 2009 (also see Fig. 13). The white square in the upper photo outlines the area of the enlarged view below. The spacecraft is ca. 3.3 m tall and is casting a 15 m shadow to the East. (NASA/LROC/ ASU/GSFC photos) iii iv Surveyor I: America’s First Moon Landing by William F. Mellberg v © 2014, 2015 William F. Mellberg vi About the author: William Mellberg was a marketing and public relations representative with Fokker Aircraft. He is also an aerospace historian, having published many articles on both the development of airplanes and space vehicles in various magazines. He is the author of Famous Airliners and Moon Missions. He also serves as co-Editor of Harrison H. Schmitt’s website: http://americasuncommonsense.com Acknowledgments: The support and recollections of Frank Mellberg, Harrison Schmitt, Justin Rennilson, Alexander Gurshstein, Paul Spudis, Ronald Wells, Colin Mackellar and Dwight Steven- Boniecki is gratefully acknowledged. vii Surveyor I: America’s First Moon Landing by William F. Mellberg A Journey of 250,000 Miles . December 14, 2013. China’s Chang’e 3 spacecraft successfully touched down on the Moon at 1311 GMT (2111 Beijing Time). The landing site was in Mare Imbrium, the Sea of Rains, about 25 miles (40 km) south of the small crater, Laplace F, and roughly 100 miles (160 km) east of its original target in Sinus Iridum, the Bay of Rainbows. -
In-Flight Validation of Akatsuki X-Band Deep Space Telecommunication Technologies
Trans. JSASS Aerospace Tech. Japan Vol. 10, No. ists28, pp. To_3_7-To_3_12, 2012 Topics In-FlightIn-Flight Validation Validation of Akatsuki of Akatsuki X-Band X-Band Deep SpaceDeep SpaceTelecommu- Telecommunicationnication Technologies Technologies By Tomoaki TODA and Nobuaki ISHII Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, Sagamihara, Japan (Received June 24th, 2011) Akatsuki is the Japanese first Venus exploration program. The spacecraft was successfully launched in May 21st 2010 from Tanegashima Space Center via H II-A vehicle. One of her missions is a flight demonstration of her telecommunication system developed for supporting Japanese future deep space missions. During her half-year cruising phase heading for Venus, we had conducted checkouts of the system. The key technologies are a deep space transponder, a set of onboard antennas, and power amplifiers. They all were newly introduced into Akatsuki. Their performances had been tested through the half-year operations and been investigated by using collective data obtained in the experiments. Our regenerative ranging was also demonstrated in these activities. We proved that the newly introduced telecommunication system worked exactly as we had designed and that the system performances were the same as evaluated on the ground. In this paper, we will summarize these in-flight validations for the Akatsuki telecommunication system. Key Words: Akatsuki, PLANET-C, Deep Space Telecommunications, Regenerative Ranging 1. Introduction block diagram of Akatsuki. The redundancy is given to TRPs and 10 W solid-state power amplifiers (SSPAs). The TWTA is Akatsuki is the Venus exploration program of Japan Aero- provided for the increase of scientific data acquisition.