Moon Mapping Project Results on Solar Wind Ion Flux and Composition †
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A Quantitative Human Spacecraft Design Evaluation Model For
A QUANTITATIVE HUMAN SPACECRAFT DESIGN EVALUATION MODEL FOR ASSESSING CREW ACCOMMODATION AND UTILIZATION by CHRISTINE FANCHIANG B.S., Massachusetts Institute of Technology, 2007 M.S., University of Colorado Boulder, 2010 A thesis submitted to the Faculty of the Graduate School of the University of Colorado in partial fulfillment of the requirement for the degree of Doctor of Philosophy Department of Aerospace Engineering Sciences 2017 i This thesis entitled: A Quantitative Human Spacecraft Design Evaluation Model for Assessing Crew Accommodation and Utilization written by Christine Fanchiang has been approved for the Department of Aerospace Engineering Sciences Dr. David M. Klaus Dr. Jessica J. Marquez Dr. Nisar R. Ahmed Dr. Daniel J. Szafir Dr. Jennifer A. Mindock Dr. James A. Nabity Date: 13 March 2017 The final copy of this thesis has been examined by the signatories, and we find that both the content and the form meet acceptable presentation standards of scholarly work in the above mentioned discipline. ii Fanchiang, Christine (Ph.D., Aerospace Engineering Sciences) A Quantitative Human Spacecraft Design Evaluation Model for Assessing Crew Accommodation and Utilization Thesis directed by Professor David M. Klaus Crew performance, including both accommodation and utilization factors, is an integral part of every human spaceflight mission from commercial space tourism, to the demanding journey to Mars and beyond. Spacecraft were historically built by engineers and technologists trying to adapt the vehicle into cutting edge rocketry with the assumption that the astronauts could be trained and will adapt to the design. By and large, that is still the current state of the art. It is recognized, however, that poor human-machine design integration can lead to catastrophic and deadly mishaps. -
AAS Worldwide Telescope: Seamless, Cross-Platform Data Visualization Engine for Astronomy Research, Education, and Democratizing Data
AAS WorldWide Telescope: Seamless, Cross-Platform Data Visualization Engine for Astronomy Research, Education, and Democratizing Data The Harvard community has made this article openly available. Please share how this access benefits you. Your story matters Citation Rosenfield, Philip, Jonathan Fay, Ronald K Gilchrist, Chenzhou Cui, A. David Weigel, Thomas Robitaille, Oderah Justin Otor, and Alyssa Goodman. 2018. AAS WorldWide Telescope: Seamless, Cross-Platform Data Visualization Engine for Astronomy Research, Education, and Democratizing Data. The Astrophysical Journal: Supplement Series 236, no. 1. Published Version https://iopscience-iop-org.ezp-prod1.hul.harvard.edu/ article/10.3847/1538-4365/aab776 Citable link http://nrs.harvard.edu/urn-3:HUL.InstRepos:41504669 Terms of Use This article was downloaded from Harvard University’s DASH repository, and is made available under the terms and conditions applicable to Open Access Policy Articles, as set forth at http:// nrs.harvard.edu/urn-3:HUL.InstRepos:dash.current.terms-of- use#OAP Draft version January 30, 2018 Typeset using LATEX twocolumn style in AASTeX62 AAS WorldWide Telescope: Seamless, Cross-Platform Data Visualization Engine for Astronomy Research, Education, and Democratizing Data Philip Rosenfield,1 Jonathan Fay,1 Ronald K Gilchrist,1 Chenzhou Cui,2 A. David Weigel,3 Thomas Robitaille,4 Oderah Justin Otor,1 and Alyssa Goodman5 1American Astronomical Society 1667 K St NW Suite 800 Washington, DC 20006, USA 2National Astronomical Observatories, Chinese Academy of Sciences 20A Datun Road, Chaoyang District Beijing, 100012, China 3Christenberry Planetarium, Samford University 800 Lakeshore Drive Birmingham, AL 35229, USA 4Aperio Software Ltd. Headingley Enterprise and Arts Centre, Bennett Road Leeds, LS6 3HN, United Kingdom 5Harvard Smithsonian Center for Astrophysics 60 Garden St. -
Arxiv:2006.00776V1 [Physics.Space-Ph] 1 Jun 2020
manuscript submitted to Geophysical Research Letters Dust impact voltage signatures on Parker Solar Probe: influence of spacecraft floating potential S. D. Bale1,2, K. Goetz3, J. W. Bonnell1, A. W. Case4, C. H. K. Chen5,T. Dudok de Wit6, L. C. Gasque1,2, P. R. Harvey1, J. C. Kasper 7,4, P. J. Kellogg3, R. J. MacDowall8, M. Maksimovic9, D. M. Malaspina10, B. F. Page1,2, M. Pulupa1, M. L. Stevens4, J. R. Szalay11, A. Zaslavsky9 1Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450, USA 2Physics Department, University of California, Berkeley, CA 94720-7300, USA 3School of Physics and Astronomy, University of Minnesota, Minneapolis, 55455, USA 4Smithsonian Astrophysical Observatory, Cambridge, MA 02138 USA 5School of Physics and Astronomy, Queen Mary University of London, London E1 4NS, UK 6LPC2E, CNRS and University of Orleans,´ Orleans,´ France 7Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, MI 48109, USA 8Solar System Exploration Division, NASA/Goddard Space Flight Center, Greenbelt, MD, 20771 9LESIA, Observatoire de Paris, Universit PSL, CNRS, Sorbonne Universit, Universit de Paris, 5 place Jules Janssen, 92195 Meudon, France 10Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO, 80303, USA 11Department of Astrophysical Sciences, Princeton University, Princeton, NJ, 08544, USA Key Points: • The Parker Solar Probe (PSP) FIELDS instrument measures millisecond volt- ages impulses associated with dust impacts • The sign of the largest monopole voltage response is a function of the spacecraft floating potential • These measurements are consistent with models of dynamic charge balance following dust impacts Submitted : June 2, 2020 arXiv:2006.00776v1 [physics.space-ph] 1 Jun 2020 Corresponding author: Stuart D. -
Chandrayaan-2 Completes a Year Around the Moon
One-year completion of Chandrayaan-2 Lunar orbit insertion (August 20, 2019) Chandrayaan-2 completes a year around the Moon The Moon provides the best linkage to understand Earth’s early history and offers an undisturbed record of the inner Solar system environment. It could also be a base for future human space exploration of the solar system and a unique laboratory, unlike any on Earth, for fundamental physics investigations. In spite of several missions to the Moon, there remains several unanswered questions. Continued high resolution studies of its surface, sub-surface/interior and its low-density exosphere, are essential to address diversities in lunar surface composition and to trace back the origin and evolution of the Moon. The clear evidence from India’s first mission to the Moon, Chandrayaan-1, on the extensive presence of surface water and the indication for sub- surface polar water-ice deposits, argues for more focused studies on the extent of water on the surface, below the surface and in the tenuous lunar exosphere, to address the true origin and availability of water on Moon. With the goal of expanding the lunar scientific knowledge through detailed studies of topography, mineralogy, surface chemical composition, thermo-physical characteristics and the lunar exosphere, Chandrayaan-2 was launched on 22nd July 2019 and inserted into the lunar orbit on 20th August 2019, exactly one year ago. Though the soft-landing attempt was not successful, the orbiter, which was equipped with eight scientific instruments, was successfully placed in the lunar orbit. The orbiter completed more than 4400 orbits around the Moon and all the instruments are currently performing well. -
Science: Planetary Science Outyears Are Notional
Science: Planetary Science Outyears are notional ($M) 2019 2020 2021 2022 2023 Planetary Science $2,235 $2,200 $2,181 $2,162 $2,143 Ø Creates a robotic Lunar Discovery and Exploration program, that supports commercial partnerships and innovative approaches to achieving human and science exploration goals. Ø Continues development of Mars 2020 and Europa Clipper. Ø Establishes a Planetary Defense program, including the Double Asteroid Redirection Test (DART) and Near-Earth Object Observations. Ø Studies a potential Mars Sample Return mission incorporating commercial partnerships. Ø Formulates the Lucy and Psyche missions. Ø Selects the next New Frontiers mission. Ø Invests in CubeSats/SmallSats that can achieve entirely new science at lower cost. Ø Operates 10 Planetary missions. § OSIRIS-REx will map asteroid Bennu. § New Horizons will fly by its Kuiper belt target. Dawn Image of Ceres on January 13, 2015 20 Science: Astrophysics Outyears are notional ($M) 2019 2020 2021 2022 2023 Astrophysics $1,185 $1,185 $1,185 $1,185 $1,185 Ø Launches the James Webb Space Telescope. Ø Moves Webb into the Cosmic Origins Program within the Astrophysics Account. Ø Terminates WFIRST due to its significant cost and higher priorities elsewhere within NASA. Increases funding for future competed missions and research. Ø Supports the TESS exoplanet mission following launch by June 2018. Ø Formulates or develops, IXPE, GUSTO, XARM, Euclid, and a new MIDEX mission to be selected in FY 2019. Ø Operates ten missions and the balloon project. Ø Invests in CubeSats/SmallSats that can achieve entirely new science at lower cost. Ø All Astrophysics missions beyond prime operations (including SOFIA) will be subject to senior review in 2019. -
Transmittal of Geotail Prelaunch Mission Operation Report
National Aeronautics and Space Administration Washington, D.C. 20546 ss Reply to Attn of: TO: DISTRIBUTION FROM: S/Associate Administrator for Space Science and Applications SUBJECT: Transmittal of Geotail Prelaunch Mission Operation Report I am pleased to forward with this memorandum the Prelaunch Mission Operation Report for Geotail, a joint project of the Institute of Space and Astronautical Science (ISAS) of Japan and NASA to investigate the geomagnetic tail region of the magnetosphere. The satellite was designed and developed by ISAS and will carry two ISAS, two NASA, and three joint ISAS/NASA instruments. The launch, on a Delta II expendable launch vehicle (ELV), will take place no earlier than July 14, 1992, from Cape Canaveral Air Force Station. This launch is the first under NASA’s Medium ELV launch service contract with the McDonnell Douglas Corporation. Geotail is an element in the International Solar Terrestrial Physics (ISTP) Program. The overall goal of the ISTP Program is to employ simultaneous and closely coordinated remote observations of the sun and in situ observations both in the undisturbed heliosphere near Earth and in Earth’s magnetosphere to measure, model, and quantitatively assess the processes in the sun/Earth interaction chain. In the early phase of the Program, simultaneous measurements in the key regions of geospace from Geotail and the two U.S. satellites of the Global Geospace Science (GGS) Program, Wind and Polar, along with equatorial measurements, will be used to characterize global energy transfer. The current schedule includes, in addition to the July launch of Geotail, launches of Wind in August 1993 and Polar in May 1994. -
A New Polarimeter to Study the Curl Component of the Cosmic Microwave Background Polarization
UNIVERSITA` DEGLI STUDI DI ROMA \LA SAPIENZA" Facolt`adi Scienze Matematiche Fisiche e Naturali A new polarimeter to study the curl component of the Cosmic Microwave Background polarization Tesi di Laurea Specialistica in Astronomia ed Astro¯sica Anno Accademico 2005/2006 Author Supervisor Lorenzo Moncelsi Prof. Paolo de Bernardis Register: 1071681 Co-supervisor Dott. Federico Nati Contents Introduzione 6 Introduction 10 1 The Hot Big Bang Model and the Inflation add-on 11 1.1 Introduction . 11 1.2 The Standard Cosmological Model . 11 1.3 The Unsolved Problems . 17 1.3.1 The flatness problem . 17 1.3.2 The horizons problem . 18 1.3.3 The absence of magnetic monopoles . 19 1.4 The Solution: Inflation . 20 1.5 The Physics of Inflation . 22 1.5.1 Scalar Fields . 22 1.5.2 Slow-Roll Approximation . 25 1.5.3 Exact Solutions . 26 1.5.4 Hamilton-Jacobi Formulation . 28 1.5.5 Reheating . 29 1.5.6 Scalar Fluctuations . 30 1.5.7 Tensor Fluctuations . 34 2 The Cosmic Microwave Background 37 2.1 Introduction . 37 2.2 Earth's Absolute Motion: The Dipole Anisotropy . 39 2.3 The Last Scattering Surface . 42 2.4 The Temperature Power Spectrum . 44 2.4.1 Physical E®ects at Recombination . 44 2.4.2 Statistical Treatment . 47 2.4.3 The Shape of the Spectrum . 49 2.5 Polarization . 54 2.5.1 Thomson Scattering at Recombination . 54 2.5.2 Statistical Treatment . 56 2.5.3 Quadrupole Anisotropy From Scalar Perturbations . 65 I 2.5.4 Quadrupole Anisotropy From Tensor Perturbations . -
On Parker Solar Probe, NASA Leaves the Driving to Aerojet Rocketdyne
On Parker Solar Probe, NASA Leaves the Driving to Aerojet Rocketdyne August 12, 2018 KENNEDY SPACE CENTER, Fla., Aug. 12, 2018 (GLOBE NEWSWIRE) -- With a big assist from Aerojet Rocketdyne, NASA’s Parker Solar Probe is now on its way to humankind’s closest encounter ever with a star – in this case our solar system’s sun. Parker Solar Probe NASA image Aerojet Rocketdyne provided the full propulsion system on NASA’s Parker Solar Probe, which will venture eight times closer to the Sun than the previous record holderCredit: NASA/Johns Hopkins APL In addition to the RS-68A main engines for the United Launch Alliance Delta IV Heavy rocket that launched the Parker Probe into space, Aerojet Rocketdyne also supplied the RL10B-2 second stage engine and 12 MR-106 reaction control thrusters on the Delta Cryogenic Second Stage, as well as the full propulsion system on the Parker Solar Probe. The nearly 7-year journey will bring the probe to within 6.2 million kilometers of the Sun’s surface. That’s well within the orbit of the Sun’s nearest planet, Mercury, and eight times closer than the previous record holder, the U.S.-German Helios B probe, which made its closest approach in 1976. “Surviving a years-long journey to the corona of the Sun while operating in autonomous mode requires an incredibly high level of reliability,” said Aerojet Rocketdyne CEO and President Eileen Drake. “Aerojet Rocketdyne propulsion plays a critical role in all aspects of the Parker Solar Probe mission, from launch on the Delta IV, to the probe’s safe cruise through space and approach of the Sun’s atmosphere.” The Parker Solar Probe ultimately will dip into the Sun’s corona, carrying instruments to observe and measure the movement and interaction of phenomena including electric and magnetic fields, energetic particles and solar wind. -
Collision Avoidance Operations in a Multi-Mission Environment
AIAA 2014-1745 SpaceOps Conferences 5-9 May 2014, Pasadena, CA Proceedings of the 2014 SpaceOps Conference, SpaceOps 2014 Conference Pasadena, CA, USA, May 5-9, 2014, Paper DRAFT ONLY AIAA 2014-1745. Collision Avoidance Operations in a Multi-Mission Environment Manfred Bester,1 Bryce Roberts,2 Mark Lewis,3 Jeremy Thorsness,4 Gregory Picard,5 Sabine Frey,6 Daniel Cosgrove,7 Jeffrey Marchese,8 Aaron Burgart,9 and William Craig10 Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450 With the increasing number of manmade object orbiting Earth, the probability for close encounters or on-orbit collisions is of great concern to spacecraft operators. The presence of debris clouds from various disintegration events amplifies these concerns, especially in low- Earth orbits. The University of California, Berkeley currently operates seven NASA spacecraft in various orbit regimes around the Earth and the Moon, and actively participates in collision avoidance operations. NASA Goddard Space Flight Center and the Jet Propulsion Laboratory provide conjunction analyses. In two cases, collision avoidance operations were executed to reduce the risks of on-orbit collisions. With one of the Earth orbiting THEMIS spacecraft, a small thrust maneuver was executed to increase the miss distance for a predicted close conjunction. For the NuSTAR observatory, an attitude maneuver was executed to minimize the cross section with respect to a particular conjunction geometry. Operations for these two events are presented as case studies. A number of experiences and lessons learned are included. Nomenclature dLong = geographic longitude increment ΔV = change in velocity dZgeo = geostationary orbit crossing distance increment i = inclination Pc = probability of collision R = geostationary radius RE = Earth radius σ = standard deviation Zgeo = geostationary orbit crossing distance I. -
The Active Region Source of a Type III Radio Storm Observed by Parker Solar Probe During Encounter 2 Log-Spaced Chunks, Each of 2.56 Mhz Wide
Astronomy & Astrophysics manuscript no. ISSI_E2_Hinode-final ©ESO 2021 February 10, 2021 The active region source of a type III radio storm observed by Parker Solar Probe during Encounter 2 L. Harra1, 2, D. H. Brooks3, S. D. Bale4, C. H. Mandrini5, 6, K. Barczynski1, 2, R. Sharma7, S. T. Badman4, S. Vargas Domínguez8, and M. Pulupa4 1 PMOD/WRC, Dorfstrasse 33 CH-7260 Davos Dorf, Switzerland e-mail: [email protected] e-mail: [email protected] 2 ETH-Zurich, Hönggerberg campus, HIT building, Zürich, Switzerland 3 College of Science, George Mason University, 4400 University Drive, Fairfax, VA 22030 USA e-mail: [email protected] 4 Physics Department and Space Sciences Laboratory, University of California, Berkeley, USA. 94720-7450 e-mail: [email protected] 5 Instituto de Astronomía y Física del Espacio (IAFE), CONICET-UBA, Buenos Aires, Argentina 6 Facultad de Ciencias Exactas y Naturales (FCEN), UBA, Buenos Aires, Argentina e-mail: [email protected] 7 Fachhochschule Nordwestschweiz (FHNW), Bahnhofstrasse 6, 5210 Windisch, Switzerland e-mail: [email protected] 8 Universidad Nacional de Colombia, Observatorio Astronómico Nacional, Bogotá, Colombia e-mail: [email protected] Received September 2020 ABSTRACT Context. To investigate the source of a type III radio burst storm during encounter 2 of NASA’s Parker Solar Probe (PSP) mission. Aims. It was observed that in encounter 2 of NASA’s Parker Solar Probe mission there was a large amount of radio activity, and in particular a noise storm of frequent, small type III bursts from 31st March to 6th April 2019. Our aim is to investigate the source of these small and frequent bursts. -
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. -
FACTORS" with Multiple Compact Satellites for the Space-Earth Coupling Mechanisms
PCG21-05 Japan Geoscience Union Meeting 2018 Science Objectives and Mission Plan of "FACTORS" with Multiple Compact Satellites for the Space-Earth Coupling Mechanisms *Masafumi Hirahara1, Yoshifumi Saito2, Hirotsugu Kojima3, Naritoshi Kitamura2, Kazushi Asamura 2, Ayako Matsuoka2, Takeshi Sakanoi4, Yoshizumi Miyoshi1, Shin-ichiro Oyama1, Masatoshi Yamauchi5, Yuichi Tsuda2, Nobutaka Bando2 1. Institute of Space-Earth Environmental Research, Nagoya University, 2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3. Research Institute for Sustainable Humanosphere, Kyoto University, 4. Planetary Plasma and Atmospheric Research Center, Graduate School of Science, Tohoku University, 5. Swedish Institute of Space Physics After the successful launch and the recent observational progresses of the ERG(Arase) satellite mission, we have been leading the next community exploration mission in the Japanese space physics research. In the ERG mission, we are focusing on the unique space plasma mechanisms and conditions causing the terrestrial radiation belt through the wave-particle interaction analyses and the triangle-type research system consisting the satellite and ground-based observations and the data analyses/modelings/simulations. Our next exploration target is the space-Earth connection processes/mechanisms responsible for the formation and coupling of the terrestrial magnetosphere/ionoshere/thermosphere and the acceleration and transportation of the space plasma and neutral atmospheric particles, which could be