IMTEC-89-46FS Space Operations: Listing of NASA Scientific Missions
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The Contribution of Global Ocean Observation of Continuity of HY-2
CGMS-XXXVI-CNSA-WP-04 Prepared by CNSA Agenda Item: III/3&4 The contribution of global ocean observation of continuity of HY-2 satellite HY-2 satellite, an ocean dynamic environment observation satellite, mainly ` objective is monitoring and detecting the parameters of ocean dynamic environment. These parameters include sea surface wind fields, sea surface height, wave height, gravity field, ocean circulation and sea surface temperature etc. The contribution of global ocean observation of continuity of HY-2 satellite 1. Introduction HY-2 satellite scatterometer provides sea surface wind fields, which can offset the observation gap of the plan of global scatterometer. At the same time, HY-2 satellite altimeter provides sea surface height, significant wave height, sea surface wind speed and polar ice sheet elevation, which can offset the observation gap of the plan of global altimeter around 2012, and can offset the observation gap of JASON-1&2 at polar area. More details as follows. 2. Observation of sea surface wind fields The analysis accuracy of wind field for ocean-atmosphere can improve 10-20% by using the satellite scatterometer data, by which can improve greatly the quality of initial wind field of numerical atmospheric forecast model in coastal ocean. Satellite scatterometer data has play important role on study of large-scale ocean phenomenon, such as sea-air interactions, ocean circulation, EI Nino etc. The figure 1 shows that QuikSCAT scatterometer has operational application in 1999, but it has not the following plan. ERS-2 scatterometer mission has transferred to METOP ASCAT in 2006. GCOM-B1 will launch in 2008, one of its payloads is an ocean vector wind measurement (OVWM) instruments, and it also called AlphaScat. -
In Brief Modified to Increase Engine Reliability
r bulletin 102 — may 2000 3rd Space Station ESA, together with a European industrial Element to be Launched consortium headed by DaimlerChrysler (D) and including Belgian, Dutch and French NASA and the Russian Aviation and partners, was responsible for the design, Space Agency (Rosaviakosmos) plan that development and delivery of the core data the next component of the International management system, which provides Space Station (ISS) – the Zvezda service Zvezda’s main computer. module – will be launched on 12 July from the Baikonur Cosmodrome in Kazakhstan. ESA also has a contract with Rosaviakosmos and RSC-Energia for Following a Joint Programme Review and performing system and interface a General Designers’ Review in Moscow, it integration tasks required for docking with was agreed that Zvezda (Russian for Zvezda by ESA’s Automated Transfer ‘star’) will be launched by a Proton rocket Vehicle (ATV), which will be used for ISS with the second and third stage engines re-boost and logistics support missions In Brief modified to increase engine reliability. from 2003 onwards. Through its ATV industrial consortium led by Aerospatiale Zvezda will provide the early living quarters Matra Lanceurs (F), ESA is also procuring for ISS crew, together with the life sup- some Russian hardware and software for port, electrical power distribution, data use with the ATV. management, flight control, and propul- sion systems for the ISS. On the scientific side, ESA has concluded contracts with Rosaviakosmos and RSC- Energia for the conduct of scientific experiments on Zvezda, including the Global Timing System (GTS) and a radiobiology experiment (called Matroshka) to monitor and analyse radiation doses in ISS crew. -
Using Earth Observation Data to Improve Health in the United States Accomplishments and Future Challenges
a report of the csis technology and public policy program Using Earth Observation Data to Improve Health in the United States accomplishments and future challenges 1800 K Street, NW | Washington, DC 20006 Tel: (202) 887-0200 | Fax: (202) 775-3199 Author E-mail: [email protected] | Web: www.csis.org Lyn D. Wigbels September 2011 ISBN 978-0-89206-668-1 Ë|xHSKITCy066681zv*:+:!:+:! a report of the csis technology and public policy program Using Earth Observation Data to Improve Health in the United States accomplishments and future challenges Author Lyn D. Wigbels September 2011 About CSIS At a time of new global opportunities and challenges, the Center for Strategic and International Studies (CSIS) provides strategic insights and bipartisan policy solutions to decisionmakers in government, international institutions, the private sector, and civil society. A bipartisan, nonprofit organization headquartered in Washington, D.C., CSIS conducts research and analysis and devel- ops policy initiatives that look into the future and anticipate change. Founded by David M. Abshire and Admiral Arleigh Burke at the height of the Cold War, CSIS was dedicated to finding ways for America to sustain its prominence and prosperity as a force for good in the world. Since 1962, CSIS has grown to become one of the world’s preeminent international policy institutions, with more than 220 full-time staff and a large network of affiliated scholars focused on defense and security, regional stability, and transnational challenges ranging from energy and climate to global development and economic integration. Former U.S. senator Sam Nunn became chairman of the CSIS Board of Trustees in 1999, and John J. -
University of Iowa Instruments in Space
University of Iowa Instruments in Space A-D13-089-5 Wind Van Allen Probes Cluster Mercury Earth Venus Mars Express HaloSat MMS Geotail Mars Voyager 2 Neptune Uranus Juno Pluto Jupiter Saturn Voyager 1 Spaceflight instruments designed and built at the University of Iowa in the Department of Physics & Astronomy (1958-2019) Explorer 1 1958 Feb. 1 OGO 4 1967 July 28 Juno * 2011 Aug. 5 Launch Date Launch Date Launch Date Spacecraft Spacecraft Spacecraft Explorer 3 (U1T9)58 Mar. 26 Injun 5 1(U9T68) Aug. 8 (UT) ExpEloxrpelro r1e r 4 1915985 8F eJbu.l y1 26 OEGxOpl o4rer 41 (IMP-5) 19697 Juunlye 2 281 Juno * 2011 Aug. 5 Explorer 2 (launch failure) 1958 Mar. 5 OGO 5 1968 Mar. 4 Van Allen Probe A * 2012 Aug. 30 ExpPloiorenre 3er 1 1915985 8M Oarc. t2. 611 InEjuxnp lo5rer 45 (SSS) 197618 NAouvg.. 186 Van Allen Probe B * 2012 Aug. 30 ExpPloiorenre 4er 2 1915985 8Ju Nlyo 2v.6 8 EUxpKlo 4r e(rA 4ri1el -(4IM) P-5) 197619 DJuenc.e 1 211 Magnetospheric Multiscale Mission / 1 * 2015 Mar. 12 ExpPloiorenre 5e r 3 (launch failure) 1915985 8A uDge.c 2. 46 EPxpiolonreeerr 4130 (IMP- 6) 19721 Maarr.. 313 HMEaRgCnIe CtousbpeShaetr i(cF oMxu-1ltDis scaatelell itMe)i ssion / 2 * 2021081 J5a nM. a1r2. 12 PionPeioenr e1er 4 1915985 9O cMt.a 1r.1 3 EExpxlpolorerer r4 457 ( S(IMSSP)-7) 19721 SNeopvt.. 1263 HMaalogSnaett oCsupbhee Sriact eMlluitlet i*scale Mission / 3 * 2021081 M5a My a2r1. 12 Pioneer 2 1958 Nov. 8 UK 4 (Ariel-4) 1971 Dec. 11 Magnetospheric Multiscale Mission / 4 * 2015 Mar. -
Wide-Field Infrared Survey Explorer Launch Press
PRess KIT/DECEMBER 2009 Wide-field Infrared Survey Explorer Launch Contents Media Services Information ................................................................................................................. 3 Quick Facts ............................................................................................................................................. 4 Mission Overview .................................................................................................................................. 5 Why Infrared? ....................................................................................................................................... 10 Science Goals and Objectives ......................................................................................................... 12 Spacecraft ............................................................................................................................................. 16 Science Instrument ............................................................................................................................. 19 Infrared Missions: Past and Present ............................................................................................... 23 NASA’s Explorer Program ................................................................................................................. 25 Program/Project Management .......................................................................................................... 27 Media Contacts J.D. Harrington -
Measurement of the Earth Radiation Budget at the Top of the Atmosphere—A Review
Review Measurement of the Earth Radiation Budget at the Top of the Atmosphere—A Review Steven Dewitte * and Nicolas Clerbaux Observations Division, Royal Meteorological Institute of Belgium, 1180 Brussels, Belgium; [email protected] * Correspondence: [email protected]; Tel.: +32-2-3730624 Received: 25 September 2017; Accepted: 1 November 2017; Published: 7 November 2017 Abstract: The Earth Radiation Budget at the top of the atmosphere quantifies how the Earth gains energy from the Sun and loses energy to space. It is of fundamental importance for climate and climate change. In this paper, the current state-of-the-art of the satellite measurements of the Earth Radiation Budget is reviewed. Combining all available measurements, the most likely value of the Total Solar Irradiance at a solar minimum is 1362 W/m2, the most likely Earth albedo is 29.8%, and the most likely annual mean Outgoing Longwave Radiation is 238 W/m2. We highlight the link between long-term changes of the Outgoing Longwave Radiation, the strengthening of El Nino in the period 1985–1997 and the strengthening of La Nina in the period 2000–2009. Keywords: Earth Radiation Budget; Total Solar irradiance; Satellite remote sensing 1. Introduction The Earth Radiation Budget (ERB) at the top of the atmosphere describes how the Earth gains energy from the sun, and loses energy to space through reflection of solar radiation and the emission of thermal radiation. The ERB is of fundamental importance for climate since: (1) The global climate, as quantified e.g., by the global average temperature, is determined by this energy exchange. -
Developments in Observations and Theory for Solar Cycle 22 Laurel, Maryland, 8-9 June 1989
MA Workshop #2: Developments in Observations and Theory for Solar Cycle 22 Laurel, Maryland, 8-9 June 1989 {i<?',.., '- i _'-_'? ; ._,/ , _t MAX Workshop #2: Developments in Observations and Theory for Solar Cycle 22 Laurel, Maryland, 8-9 June 1989 Edited by Robert M. Winglee University of Colorado Boulder, Colorado Brian R. Dennis NASA Goddard Space Flight Center Greenbelt, Maryland Cover An eruptive prominence associated with the X1.6 3B flare of June 20, 1989. This event and its coronal mass ejection were well observed during the first Max '91 Campaign. This digital H-alpha image was obtained at 15:04 UT ( 4 minutes before the peak of the event in soft X-rays) by the Holloman Solar Observatory of the USAF SOON system. TABLE OF CONTENTS Preface ......................... vii Group Summaries High Energy Flare Physics Group Summary .......... ld] J. M. Ryan and J. D. Kurfess Magnetograph Group Summary ............... 17d_ H. P. Jones Theory and Modeling Group ................ 27_ G. D. Holman Summary of Observations of AR 5395 • . ° • . , , . ° , . 31c_z?:? j /I D. M. Zarro and R. M. Winglee Invited Reviews Scientific Objectives of Solar Gamma-Ray Observations ..... 33_;_/ R. E. Lingenfelter The Gamma-Ray Observatory: An Overview ......... D. A. Kniffen When and Where to Look to Observe Major Solar Flares .... 46_ T. Bai Access to MAX'91 Information via Computer Networks .... 6_. A. L. Kiplinger -7 High Energy Flare Physics Capabilities of GRO/OSSE for Observing Solar Flares . J. D. Kurfess, W. N. Johnson, G. H. Share, S. M. Matz and R. J. Murphy The Solar Gamma Ray and Neutron Capabilities of COMPTEL on the Gamma Ray Observatory ............ -
A Comparison Study on Thermal Control Techniques for a Nanosatellite Carrying Infrared Science Instrument
ICES-2020-15 A comparison study on thermal control techniques for a nanosatellite carrying infrared science instrument Shanmugasundaram Selvadurai1, Amal Chandran2, Sunil C Joshi3 and Teo Hang Tong Edwin 4 Nanyang Technological University, Singapore, 639798 David Valentini5 Thales Alenia Space, Cannes, 06150, France Friedhelm Olschewski6 University of Wuppertal, 42119 Wuppertal, Germany Based on current technological advancements and forecasts, nanosatellites will be used for both scientific and defense applications leveraging advantages on both development cost and development lifecycle. As nanosatellites become more capable, there is an increase in demand for high power applications which makes the missions complex from implementing a proper thermal control system (TCS) to dissipate the huge waste heat generated. One of the applications for nanosatellites is advanced infrared imaging for both scientific and military applications. ARCADE (Atmospheric coupling and Dynamics Explorer), a 27U satellite is being developed by Satellite Research Centre (SaRC) at Nanyang Technological University (NTU) for scientific objectives. The main payload AtmoLITE needs a detector cool down at -30°C and to meet this requirement, an appropriate classical TCS is chosen and described in this paper. Nanosatellites carrying infrared, cryogenic or other scientific instruments that need active cooling, should be equipped with a proper TCS within the highly constrained available volume. Another objective of this study is to compare the existing TCS for nanosatellites and adopt a suitable and efficient TCS for a scientific nanosatellite mission carrying a generic science instrument that needs an active cooling of up to 95K. TCS using Heat pipes (HP), single-phase mechanically pumped fluid loop (SMPFL), and two-phase mechanically pumped fluid loop systems (2ΦMPFL) have been extensively used only by larger satellites. -
GST Responses to “Questions to Inform Development of the National Plan”
GST Responses to “Questions to Inform Development of the National Plan” Name (optional): Dr. Darrel Williams Position (optional): Chief Scientist, (240) 542-1106; [email protected] Institution (optional): Global Science & Technology, Inc. Greenbelt, Maryland 20770 Global Science & Technology, Inc. (GST) is pleased to provide the following answers as a contribution towards OSTP’s effort to develop a national plan for civil Earth observations. In our response we provide information to support three main themes: 1. There is strong science need for high temporal resolution of moderate spatial resolution satellite earth observation that can be achieved with cost effective, innovative new approaches. 2. Operational programs need to be designed to obtain sustained climate data records. Continuity of Earth observations can be achieved through more efficient and economical means. 3. We need programs to address the integration of remotely sensed data with in situ data. GST has carefully considered these important national Earth observation issues over the past few years and has submitted the following RFI responses: The USGS RFI on Landsat Data Continuity Concepts (April 2012), NASA’s Sustainable Land Imaging Architecture RFI (September 2013), and This USGEO RFI (November 2013) relative to OSTP’s efforts to develop a national plan for civil Earth observations. In addition to the above RFI responses, GST led the development of a mature, fully compliant flight mission concept in response to NASA’s Earth Venture-2 RFP in September 2011. Our capacity to address these critical national issues resides in GST’s considerable bench strength in Earth science understanding (Drs. Darrel Williams, DeWayne Cecil, Samuel Goward, and Dixon Butler) and in NASA systems engineering and senior management oversight (Drs. -
Spacecraft System Failures and Anomalies Attributed to the Natural Space Environment
NASA Reference Publication 1390 - j Spacecraft System Failures and Anomalies Attributed to the Natural Space Environment K.L. Bedingfield, R.D. Leach, and M.B. Alexander, Editor August 1996 NASA Reference Publication 1390 Spacecraft System Failures and Anomalies Attributed to the Natural Space Environment K.L. Bedingfield Universities Space Research Association • Huntsville, Alabama R.D. Leach Computer Sciences Corporation • Huntsville, Alabama M.B. Alexander, Editor Marshall Space Flight Center • MSFC, Alabama National Aeronautics and Space Administration Marshall Space Flight Center ° MSFC, Alabama 35812 August 1996 PREFACE The effects of the natural space environment on spacecraft design, development, and operation are the topic of a series of NASA Reference Publications currently being developed by the Electromagnetics and Aerospace Environments Branch, Systems Analysis and Integration Laboratory, Marshall Space Flight Center. This primer provides an overview of seven major areas of the natural space environment including brief definitions, related programmatic issues, and effects on various spacecraft subsystems. The primary focus is to present more than 100 case histories of spacecraft failures and anomalies documented from 1974 through 1994 attributed to the natural space environment. A better understanding of the natural space environment and its effects will enable spacecraft designers and managers to more effectively minimize program risks and costs, optimize design quality, and achieve mission objectives. .o° 111 TABLE OF CONTENTS -
Proceedings of Spie
PROCEEDINGS OF SPIE SPIEDigitalLibrary.org/conference-proceedings-of-spie Ground calibration of the spatial response and quantum efficiency of the CdZnTe hard x-ray detectors for NuSTAR Brian W. Grefenstette, Varun Bhalerao, W. Rick Cook, Fiona A. Harrison, Takao Kitaguchi, et al. Brian W. Grefenstette, Varun Bhalerao, W. Rick Cook, Fiona A. Harrison, Takao Kitaguchi, Kristin K. Madsen, Peter H. Mao, Hiromasa Miyasaka, Vikram Rana, "Ground calibration of the spatial response and quantum efficiency of the CdZnTe hard x-ray detectors for NuSTAR," Proc. SPIE 10392, Hard X-Ray, Gamma-Ray, and Neutron Detector Physics XIX, 1039207 (29 August 2017); doi: 10.1117/12.2271365 Event: SPIE Optical Engineering + Applications, 2017, San Diego, California, United States Downloaded From: https://www.spiedigitallibrary.org/conference-proceedings-of-spie on 1/5/2018 Terms of Use: https://www.spiedigitallibrary.org/terms-of-use Ground Calibration of the Spatial Response and Quantum Efficiency of the CdZnTe Hard X-ray Detectors for NuSTAR Brian W. Grefenstette1, Varun Bhalerao2, W. Rick Cook1, Fiona A. Harrison1, Takao Kitaguchi3, Kristin K. Madsen1, Peter H. Mao1, Hiromasa Miyasaka1, Vikram Rana1 1Space Radiation Lab, California Institute of Technology (Caltech), Pasadena, CA 2Department of Physics, Indian Institute of Technology Bombay, Powai, Mumbai, India 3RIKEN Nishina Center, 2-1 Hirosawa, Wako, Saitama 351-0198, Japan ABSTRACT Pixelated Cadmium Zinc Telluride (CdZnTe) detectors are currently flying on the Nuclear Spectroscopic Tele- scope ARray (NuSTAR) NASA Astrophysics Small Explorer. While the pixel pitch of the detectors is ≈ 605 µm, we can leverage the detector readout architecture to determine the interaction location of an individual photon to much higher spatial accuracy. -
Cubesat-Based Science Missions for Geospace and Atmospheric Research
National Aeronautics and Space Administration NATIONAL SCIENCE FOUNDATION (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH annual report October 2013 www.nasa.gov www.nsf.gov LETTERS OF SUPPORT 3 CONTACTS 5 NSF PROGRAM OBJECTIVES 6 GSFC WFF OBJECTIVES 8 2013 AND PRIOR PROJECTS 11 Radio Aurora Explorer (RAX) 12 Project Description 12 Scientific Accomplishments 14 Technology 14 Education 14 Publications 15 Contents Colorado Student Space Weather Experiment (CSSWE) 17 Project Description 17 Scientific Accomplishments 17 Technology 18 Education 18 Publications 19 Data Archive 19 Dynamic Ionosphere CubeSat Experiment (DICE) 20 Project Description 20 Scientific Accomplishments 20 Technology 21 Education 22 Publications 23 Data Archive 24 Firefly and FireStation 26 Project Description 26 Scientific Accomplishments 26 Technology 27 Education 28 Student Profiles 30 Publications 31 Cubesat for Ions, Neutrals, Electrons and MAgnetic fields (CINEMA) 32 Project Description 32 Scientific Accomplishments 32 Technology 33 Education 33 Focused Investigations of Relativistic Electron Burst, Intensity, Range, and Dynamics (FIREBIRD) 34 Project Description 34 Scientific Accomplishments 34 Education 34 2014 PROJECTS 35 Oxygen Photometry of the Atmospheric Limb (OPAL) 36 Project Description 36 Planned Scientific Accomplishments 36 Planned Technology 36 Planned Education 37 (NSF) CUBESAT-BASED SCIENCE MISSIONS FOR GEOSPACE AND ATMOSPHERIC RESEARCH [ 1 QB50/QBUS 38 Project Description 38 Planned Scientific Accomplishments 38 Planned