International Cooperation in Space
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XXIX Congress Report XXIX Planetary Congress • Austria • 2016 Photos: OEWF
XXIX Congress Report XXIX Planetary Congress • Austria • 2016 Photos: OEWF 1 John-David Bartoe, 2 Alexander Ivanchenkov, 3 Ulrich Walter, 4 Gerhard Thiele, 5 Georgi Iva- nov, 6 Yuri Gidzenko, 7 Bertalan Farkas, 8 Kevin Ford, 9 Pavel Vinogradov, 10 Charlie Walker, 11 Kimiya Yui, 12 Anatoli Artsebarskii, 13 Shannon Lucid, 14 Reinhold Ewald, 15 Claudie Haigneré, 16 Joe Acaba, 17 Ernst Messerschmid, 18 Jan Davis, 19 Franz Viehbock, 20 Loren Shriver, 21 Miroslaw Hermaszewski. 22 Sultan bin Salman al-Saud, 23 Yang Liwei, 24 Richard Garriott, 25 Mark Brown, 26 Carl Walz, 27 Bill McArthur, 28 Owen Garriott, 29 Anna Fisher, 30 George Zam- ka, 31 Rick Hieb, 32 Jerry Ross, 33 Alexander Volkov, 34 André Kuipers, 35 Jean-Pierre Haign- eré, 36 Toktar Aubakirov, 37 Kay Hire, 38 Michael Fincke, 39 John Fabian, 40 Pedro Duque, 41 Michael Foreman, 42 Sergei Avdeev, 43 Vladimir Kovolyonok, 44 Alexandar Aleksandrov, 45 Alexander Alexandrov, 46 Drew Feustel, 47 Dumitru Prunariu, 48 Alexei Leonov, 49 Rusty Sch- weickart, 50 Klaus-Dietrich Flade, 51 Anton Shkaplerov, 52 Alexander Samokutyaev, 53 Sergei Krikalev, 54 Viktor Savinykh, 55 Soichi Noguchi, 56 Bonnie Dunbar, 57 Vladimir Aksyonov, 58 Scott Altman, 59 Yuri Baturin, 60 Susan Helms, 61 Ulf Merbold, 62 Stephanie Wilson, 63 Chiaki Mukai, 64 Charlie Camarda, 65 Julie Payette, 66 Dick Richards, 67 Yuri Usachev, 68 Michael Lo- pez-Alegria, 69 Jim Voss, 70 Rex Walheim, 71 Oleg Atkov, 72 Bobby Satcher, 73 Valeri Tokarev, 74 Sandy Magnus, 75 Bo Bobko, 76 Helen Sharman, 77 Susan Kilrain, 78 Pam Melroy, 79 Janet Kavandi, 80 Tony Antonelli, 81 Sergei Zalyotin, 82 Frank De Winne, 83 Alexander Balandin, 84 Sheikh Muszaphar, 85 Christer Fuglesang, 86 Nikolai Budarin, 87 Salizhan Sharipov, 88 Vladimir Titov, 89 Bill Readdy, 90 Bruce McCandless II, 91 Vyacheslav Zudov, 92 Brian Duffy, 93 Randy Bresnik, 94 Oleg Artemiev XXIX Planetary Congress • Austria • 2016 One hundred and four astronauts and cosmonauts from 21 nations gathered Oc- tober 3-7, 2016 in Vienna, Austria for the XXIX Planetary Congress of the Associa- tion of Space Explorers. -
NASA's STEREO Mission
NASA’s STEREO Mission J.B. Gurman STEREO Project Scientist W.T. Thompson STEREO Chief Observer Solar Physics Laboratory, Helophysics Division NASA Goddard Space Flight Center 1 The STEREO Mission • Science and technology definition team report, 1997 December: • Understand the origin and consequences of coronal mass ejections (CMEs) • Two spacecraft in earth-leading and -lagging orbits near 1 AU (Solar Terrestrial Probe line) • “Beacon” mode for near-realtime warning of potentially geoeffective events 2 Level 1 Requirements • Understand the causes and mechanisms of CME initiation • Characterize the propagation of CMEs through the heliosphere • Discover the mechanisms and sites of energetic particle acceleration in the low corona and the interplanetary medium • Develop a 3D, time-dependent model of the magnetic topology, temperature, density, and velocity structure of the ambient solar wind 3 Implementation • Two nearly identical spacecraft launched by a single ELV • Bottom spacecraft in stack has adapter ring, some strengthening • Spacecraft built at Johns Hopkins University APL • Four science investigations 4 Scientific Instruments • S/WAVES - broad frequency response RF detection of Type II, III bursts • PLASTIC - solar wind plasma and suprathermal ion composition measurements • IMPACT - energetic electrons and ions, magnetic field • SECCHI - EUV, coronagraphs and heliospheric imagers (surface to 1.5 AU) 5 Instrument Hardware • PLASTIC IMPACT boom IMPACT boom SECCHI SCIP SECCHI HI S/WAVES 6 Orbit Design • Science team selected a separation -
Nustar Observatory Guide
NuSTAR Guest Observer Program NuSTAR Observatory Guide Version 3.2 (June 2016) NuSTAR Science Operations Center, California Institute of Technology, Pasadena, CA NASA Goddard Spaceflight Center, Greenbelt, MD nustar.caltech.edu heasarc.gsfc.nasa.gov/docs/nustar/index.html i Revision History Revision Date Editor Comments D1,2,3 2014-08-01 NuSTAR SOC Initial draft 1.0 2014-08-15 NuSTAR GOF Release for AO-1 Addition of more information about CZT 2.0 2014-10-30 NuSTAR SOC detectors in section 3. 3.0 2015-09-24 NuSTAR SOC Update to section 4 for release of AO-2 Update for NuSTARDAS v1.6.0 release 3.1 2016-05-10 NuSTAR SOC (nusplitsc, Section 5) 3.2 2016-06-15 NuSTAR SOC Adjustment to section 9 ii Table of Contents Revision History ......................................................................................................................................................... ii 1. INTRODUCTION ................................................................................................................................................... 1 1.1 NuSTAR Program Organization ..................................................................................................................................................................................... 1 2. The NuSTAR observatory .................................................................................................................................... 2 2.1 NuSTAR Performance ........................................................................................................................................................................................................ -
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. -
Expedition 8 MISSION OVERVIEW
Expedition 8 MISSION OVERVIEW To Improve Life Here, Science Comes to the Forefront To Extend Life to There, To Find Life Beyond. Experiments from earlier expeditions will Education Payload Operations (EPO) remain aboard the International Space include three educational activities that That is NASAs vision. Station (ISS), continuing to benefit from will focus on demonstrating science, long-term exposure to microgavity, and mathematics, technology, engineering or Michael Foale, additional studies in the life and physical geography principles. Expedition 8 Commander, NASA ISS sciences and space technology development Group Activation Packs -- YEAST will Science Officer: will be added. evaluate the role of individual genes in the When we look back fifty years to this time, we Most of the research complement for response of yeast to space flight conditions. wont remember the experiments that were Expedition 8 will be carried out with The results of this research could help performed, we wont remember the assembly scientific research facilities and samples clarify how mammalian cells grow under that was done, we may barely remember any already on board the Space Station. microgravity conditions and determine if individuals. What we will know was that countries Additional experiments are being evaluated genes are altered. came together to do the first joint international and prepared to take advantage of the Synchronized Position Hold, Engage, project, and we will know that that was the seed limited cargo space on the Soyuz or Reorient, Experimental Satellites that started us off to the moon and Mars. Progress vehicles. The research agenda for (SPHERES) will allow scientists to study the expedition remains flexible. -
The Deep Space Network - a Technology Case Study and What Improvements to the Deep Space Network Are Needed to Support Crewed Missions to Mars?
The Deep Space Network - A Technology Case Study and What Improvements to the Deep Space Network are Needed to Support Crewed Missions to Mars? A Master’s Thesis Presented to Department of Telecommunications State University of New York Polytechnic Institute Utica, New York In Partial Fulfillment of the Requirements for the Master of Science Degree By Prasad Falke May 2017 Abstract The purpose of this thesis research is to find out what experts and interested people think about Deep Space Network (DSN) technology for the crewed Mars mission in the future. The research document also addresses possible limitations which need to be fix before any critical missions. The paper discusses issues such as: data rate, hardware upgrade and new install requirement and a budget required for that, propagation delay, need of dedicated antenna support for the mission and security constraints. The Technology Case Study (TCS) and focused discussion help to know the possible solutions and what everyone things about the DSN technology. The public platforms like Quora, Reddit, StackExchange, and Facebook Mars Society group assisted in gathering technical answers from the experts and individuals interested in this research. iv Acknowledgements As the thesis research was challenging and based on the output of the experts and interested people in this field, I would like to express my gratitude and appreciation to all the participants. A special thanks go to Dr. Larry Hash for his guidance, encouragement, and support during the whole time. Additionally, I also want to thank my mother, Mrs. Mangala Falke for inspiring me always. Last but not the least, I appreciate the support from Maricopa County Emergency Communications Group (MCECG) and Arizona Near Space Research (ANSR) Organization for helping me to find the experts in space and communications field. -
'Cervantes'mission
CERVANTES 2/26/04 2:43 PM Page 44 Human Spaceflight The ‘Cervantes’ Mission - Another European Astronaut at the ISS 44 esa bulletin 117 - february 2004 www.esa.int CERVANTES 2/26/04 2:43 PM Page 45 The Cervantes Mission Pedro Duque ESA Astronaut, European Astronaut Centre (EAC), ESA Directorate of Human Spaceflight, Cologne, Germany Astronauts from NASA, NASDA and ESA in front of the Columbus module during the European part of their Space Station training How It Came to Pass When Spain expressed interest in sponsoring a Soyuz to the International Space Station (ISS), I was informed that I might be assigned to such a mission. At the time I was a member of the Columbus Project team, where I had been working since 1999 in the areas of crew interfaces, maintainability, EVA/robotics interfaces and also to some extent NASA interfaces. In addition, I was one of a group of ESA astronauts training to operate the systems of the Training in the US Lab simulator Space Station, with the four of us being candidates for the first Permanent Crews with ESA participation. Several months passed between the initial flight idea and the official announcement by the Spanish Government, during which it became increasingly probable that I would have to train in Russia to operate the Soyuz TMA as Flight Engineer, learn how to execute experiments in the (as yet undefined) ESA Utilisation Programme, and therefore also hand over my Columbus duties. Our Training Division and the Gagarin Centre considered one year a reasonable time to devote to this, based on their experience with previous such projects (Cassiopée, Marco Polo and Odissea). -
Complete List of Contents
Complete List of Contents Volume 1 Cape Canaveral and the Kennedy Space Center ......213 Publisher’s Note ......................................................... vii Chandra X-Ray Observatory ....................................223 Introduction ................................................................. ix Clementine Mission to the Moon .............................229 Preface to the Third Edition ..................................... xiii Commercial Crewed vehicles ..................................235 Contributors ............................................................. xvii Compton Gamma Ray Observatory .........................240 List of Abbreviations ................................................. xxi Cooperation in Space: U.S. and Russian .................247 Complete List of Contents .................................... xxxiii Dawn Mission ..........................................................254 Deep Impact .............................................................259 Air Traffic Control Satellites ........................................1 Deep Space Network ................................................264 Amateur Radio Satellites .............................................6 Delta Launch Vehicles .............................................271 Ames Research Center ...............................................12 Dynamics Explorers .................................................279 Ansari X Prize ............................................................19 Early-Warning Satellites ..........................................284 -
The Deep Space Network: a Functional Description
Chapter 2 The Deep Space Network: A Functional Description Jim Taylor All deep-space missions—defined as those operating at or beyond the orbit of the Earth’s Moon—require some form of telecommunications network with a ground system to transmit to and receive data from the spacecraft. The Deep Space Network or DSN is one of the largest and most sophisticated of such networks. NASA missions in low Earth orbit communicate through either the Near Earth Network (NEN) or the SN (Space Network), with the SN, both operated by the NASA Goddard Space Flight Center (GSFC). The SN has of a number of Tracking and Data Relay Satellites (TDRS) in geosynchronous orbits. In addition, the European Space Agency operates a number of ground stations that may be used to track NASA deep space missions during the hours after launch. In addition, commercial companies operate ground stations that can communicate with NASA missions. The remainder of this book describes only the Deep Space Network operated for NASA by JPL. The lessons and techniques of the DSN replicate many comparable issues of the other networks. The lessons from the missions described in the following chapters are widely applicable to all deep space telecommunications systems. This includes post-launch support that was negotiated and planned using stations belonging to networks other than the DSN. The description and performance summary of the DSN in this chapter come from the DSN Telecommunications Link Design Handbook, widely known 15 16 Chapter 2 within NASA as the 810-5 document [1]. This modular handbook has been approved by the DSN Project Office, and its modules are updated to define current DSN capabilities. -
July Roundup WORKING
volume number 43/9 NASA White Sands Test Facility celebrates 40th anniversary by Cheerie R. Patneaude Roundup SPACE CENTER ROUNDUP Lyndon B. Johnson Space Center small test facility nestled in the San Augustine Mountains in southern New AMexico celebrated 40 years of continuous contribution to the nation’s space program on Saturday, Sept. 18. The first rocket engine was tested at the White Sands Test Facility (WSTF) on Sept. 22, 1964. Five years later, on July 20, 1969, Neil Armstrong and Buzz Aldrin landed on the Moon using the propulsion systems tested and qualified for human spaceflight at WSTF. On July 6, 1962, WSTF was chosen as the site for the Johnson Space Center Propulsion Systems Development Facility. This site was chosen for NASA S-64-17543 Ralph Rocha, technician, unpacks the first Service Propulsion System engine to be its isolated location and topography, which tested at WSTF in 1964. minimized the inherent hazards of aerospace propulsion testing to the general population. More than 310 engines have been tested to date, for a total number of firings exceeding 2.1 million. Although originally built to support propulsion tests, WSTF soon expanded to test materials to verify their suitability for use in spacecraft construction. WSTF currently does extensive testing for other NASA centers; for other government agencies including Army, Air Force, Navy, Department of Energy and Department of Transportation; and for aerospace-related commercial industries on a reimbursable basis. NASA WSTF0871-2014 A chemical steam generator provides long-duration vacuum environment for rocket engine firings at three test stands. Pat Rawlings/SAIC Space Center Roundup PRSRT STD U.S. -
The Orion Spacecraft As a Key Element in a Deep Space Gateway
The Orion Spacecraft as a Key Element in a Deep Space Gateway A Technical Paper Presented by: Timothy Cichan Lockheed Martin Space [email protected] Kerry Timmons Lockheed Martin Space [email protected] Kathleen Coderre Lockheed Martin Space [email protected] Willian D. Pratt Lockheed Martin Space [email protected] July 2017 © 2014 Lockheed Martin Corporation Abstract With the Orion exploration vehicle and Space Launch System (SLS) approaching operational status, NASA and the international community are developing the next generation of habitats to serve as a deep space platform that will be the first of its kind, a cislunar Deep Space Gateway (DSG). The DSG is evolvable, flexible, and modular. It would be positioned in the vicinity of the Moon and allow astronauts to demonstrate they can operate for months at a time well beyond Low Earth Orbit. Orion is the next generation human exploration spacecraft being developed by NASA. It is designed to perform deep space exploration missions, and is capable of carrying a crew of 4 astronauts on independent free-flight missions up to 21 days, limited only by consumables. Because Orion meets the strict requirements for deep space flight environments (reentry conditions, deep-space communications, safety, radiation, and life support for example) it is a key element in a DSG and is more than just a transportation system. Orion has the capability to act as the command deck of any deep space piloted vehicle. To increase affordability and reduce the complexity and number of subsystem functions the early DSG must be responsible for, the DSG can leverage these unique deep space qualifications of Orion. -
The Cassini-Huygens Mission Overview
SpaceOps 2006 Conference AIAA 2006-5502 The Cassini-Huygens Mission Overview N. Vandermey and B. G. Paczkowski Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 The Cassini-Huygens Program is an international science mission to the Saturnian system. Three space agencies and seventeen nations contributed to building the Cassini spacecraft and Huygens probe. The Cassini orbiter is managed and operated by NASA's Jet Propulsion Laboratory. The Huygens probe was built and operated by the European Space Agency. The mission design for Cassini-Huygens calls for a four-year orbital survey of Saturn, its rings, magnetosphere, and satellites, and the descent into Titan’s atmosphere of the Huygens probe. The Cassini orbiter tour consists of 76 orbits around Saturn with 45 close Titan flybys and 8 targeted icy satellite flybys. The Cassini orbiter spacecraft carries twelve scientific instruments that are performing a wide range of observations on a multitude of designated targets. The Huygens probe carried six additional instruments that provided in-situ sampling of the atmosphere and surface of Titan. The multi-national nature of this mission poses significant challenges in the area of flight operations. This paper will provide an overview of the mission, spacecraft, organization and flight operations environment used for the Cassini-Huygens Mission. It will address the operational complexities of the spacecraft and the science instruments and the approach used by Cassini- Huygens to address these issues. I. The Mission Saturn has fascinated observers for over 300 years. The only planet whose rings were visible from Earth with primitive telescopes, it was not until the age of robotic spacecraft that questions about the Saturnian system’s composition could be answered.