Space and Ground Segment Performance and Lessons Learned of the FORMOSAT-3/COSMIC Mission: Four Years in Orbit
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Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments
applied sciences Article Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments Jie Ren 1,2, Hui Liu 3,* , Xiaotong Lu 1,2 and Hong Chang 1,2,* 1 CAS Key Laboratory of Time and Frequency Primary Standards, National Time Service Center, Xi’an 710600, China; [email protected] (J.R.); [email protected] (X.L.) 2 School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China 3 State Key Laboratory of Photoelectric Technology and Functional Materials, International Collaborative Center on Photoelectric Technology and Nano Functional Materials, Institute of Photonics & Photon-Technology, Northwest University, Xi’an 710069, China * Correspondence: [email protected] (H.L.); [email protected] (H.C.) Received: 7 June 2020; Accepted: 15 July 2020; Published: 17 July 2020 Abstract: Obtaining ultracold alkaline earth(-like) atoms in space encounters the problem of performing narrow-line laser cooling in microgravity environments (µ-gEs). This paper reports an analysis of the magneto-optical trap (MOT) based on the narrow-line transition in 88Sr, while paying special attention to the role of the gravity. This analysis suggests the MOTs based on narrow-line transitions cannot be cold and dense enough in a µ-gE. We thus propose a strategy: that one can use a dual-frequency MOT to realize a low-temperature, high density, and high transfer efficiency, narrow-line red MOT in µ-gEs. Keywords: lasering cooling and trapping; microgravity; Monte Carlo simulation; optical lattice clocks; in space 1. Introduction Great efforts have been made in recent decades to push cold atoms into microgravity environments [1]. -
TRACKING and DATA ACQUISITION/ SPACE OPERATIONS **DB Chap 4(297-321) 1/17/02 12:29 PM Page 299
**DB Chap 4(297-321) 1/17/02 12:29 PM Page 297 CHAPTER FOUR TRACKING AND DATA ACQUISITION/ SPACE OPERATIONS **DB Chap 4(297-321) 1/17/02 12:29 PM Page 299 CHAPTER FOUR TRACKING AND DATA ACQUISITION/ SPACE OPERATIONS Introduction NASA’s tracking and data acquisition program provided vital support for all NASA flight projects. NASA also supported, on a reimbursable basis, projects of the Department of Defense, other government agencies, commercial firms, and other countries and international organizations engaged in space research activities. The tracking and data acquisition program supported sounding rock- ets and balloons, research aircraft, Earth orbital and suborbital missions, planetary spacecraft, and deep space probes. The support included: • Tracking to determine the position and trajectory of vehicles in space • Acquisition of scientific and Earth applications data from on-board experiments and sensors • Acquisition of engineering data on the performance of spacecraft and launch vehicle systems • Transmission of commands from ground stations to spacecraft • Communication with astronauts • Communication of information among the various ground facilities and central control centers • Processing of data acquired from launch vehicles and spacecraft • Reception of television transmission from space vehicles NASA established three types of support capabilities: • The Spaceflight Tracking and Data Network (STDN) supported low- Earth orbital missions. • The Deep Space Network (DSN) supported planetary and interplane- tary flight missions. It also supported geosynchronous and highly elliptical missions and those in low-Earth orbit not compatible with the Tracking and Data Relay Satellite System (TDRSS). • The TDRSS provided low-Earth orbital mission support and reduced NASA’s need for an extensive network of ground stations. -
Accuracy, Precision, and Performance of Satellite Telemetry for Monitoring Wolf Movements Within Each Category
Accuracy, Precision, and Pedormance of Satellite Telemetry for Monitoring Wolf Movements • Warren B. Ballard, Daniel J. Reed, Steven G. Fancy, and Paul R. Krausman We placed 23 satellite platform transmitter terminals (1.08-I.22 kg) on wolves in northwest Alaska during I987 through I99I. Male and female wolves aged I 0 months to eight years were monitored with no apparent adverse effects on them. We obtained 3 ,80I relocations from the 23 transmitters, an average of 29 relocations/month from each. Transmitters were programmed to operate four to six hours every two days and had a mean life span (including days before and after use on a wolf) of253 days (range= 67-482 days). Average life span while attached to wolves was I8I days (range= 50-366 days). Accuracy of I ,885 relocations at seven known sites varied among transmitters and averaged 336 and 728 mfor best and low quality relocations, respectively. The estimated locations from several transmitters were biased toward south and west directions. Costs (I992) per satellite relocation averaged about $44 U.S., in comparison to about $I66 with conventional telemetry methods using fixed-wing aircraft. Satellite telemetry has great potential for providing improved data sets for evaluation ofwolfterritory sizes and movements, but currently lacks accuracy and precision for detailed habitat or landscape use assessments. Introduction three reports provided evaluations of the systems after 1987 when Service Argos made improvements in calculating lo Satellite telemetry has become a widely accepted tool for cations and quality indices (Keating et al. 1991). Ofthe latter studying movements oflarge mammals and birds (Fancy et three studies, only Keating et al. -
7. Operations
7. Operations 7.1 Ground Operations The Exploration Systems Architecture Study (ESAS) team addressed the launch site integra- tion of the exploration systems. The team was fortunate to draw on expertise from members with historical and contemporary human space flight program experience including the Mercury, Gemini, Apollo, Skylab, Apollo Soyuz Test Project, Shuttle, and International Space Station (ISS) programs, as well as from members with ground operations experience reaching back to the Redstone, Jupiter, Pershing, and Titan launch vehicle programs. The team had a wealth of experience in both management and technical responsibilities and was able to draw on recent ground system concepts and other engineering products from the Orbital Space Plane (OSP) and Space Launch Initiative (SLI) programs, diverse X-vehicle projects, and leadership in NASA/Industry/Academia groups such as the Space Propulsion Synergy Team (SPST) and the Advanced Spaceport Technology Working Group (ASTWG). 7.1.1 Ground Operations Summary The physical and functional integration of the proposed exploration architecture elements will occur at the primary launch site at the NASA Kennedy Space Center (KSC). In order to support the ESAS recommendation of the use of a Shuttle-derived Cargo Launch Vehicle (CaLV) and a separate Crew Launch Vehicle (CLV) for lunar missions and the use of a CLV for ISS missions, KSC’s Launch Complex 39 facilities and ground equipment were selected for conversion. Ground-up replacement of the pads, assembly, refurbishment, and/or process- ing facilities was determined to be too costly and time-consuming to design, build, outfit, activate, and certify in a timely manner to support initial test flights leading to an operational CEV/CLV system by 2011. -
Metop Second Generation Payload
MetOp Second Generation Payload Marc Loiselet, Ville Kangas, Ilias Manolis, Franco Fois, Salvatore d’Addio European Space Agency, ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands E-mail: [email protected] MetOp-Second Generation Satellite Instruments Instrument Provider The ESA MetOp Second Generation (MetOp-SG) Programme was approved at the ESA Council Meeting at Ministerial level in Naples in Sat-A METimage DLR via EUMETSAT November 2012. IASI-NG CNES via EUMETSAT MetOp-SG is a follow-on to the current, first generation series of MetOp satellites, which is now established as a cornerstone of the global MWS ESA – MetOp-SG network of meteorological satellites. RO ESA – MetOp-SG The MetOp-SG programme is being implemented in collaboration with EUMETSAT. 3MI ESA – MetOp-SG ESA will develop the prototype MetOp-SG satellites (including associated instruments) and procure, on behalf of EUMETSAT, the recurrent Sentinel-5 ESA – GMES satellites (and associated instruments). The overall MetOp-SG space segment architecture consists of two series of satellites (Sat-A, Sat-B), each carrying different suites of instruments and operating in LEO polar orbit. The planned launches of the first of each series of satellites Sat-B SCA ESA – MetOp-SG are at the beginning of 2021 and at end 2022, respectively. MWI ESA – MetOp-SG RO ESA – MetOp-SG More information can be found in the “MetOp Second Generation – Overview” presentation from Graeme Mason, Hubert Barré, Maurizio ICI ESA – MetOp-SG Betto, ESA-ESTEC, The Netherlands. Argos-4 CNES via EUMETSAT Payload ESA is responsible for instrument design of six instruments, namely the MicroWave Sounder (MWS), Scatterometer (SCA), the Radio Occultation (RO), the MicroWave Imaging (MWI), the Ice Cloud Imager (ICI), and the Multi-viewing, Multi-channel, Multi-polarisation imager (3MI). -
Radio Telemetry and Bird Movements
95 Chapter 7 Radio telemetry and bird movements RADIO TELEMETRY Understanding the role that wildlife play in the ecology of AI viruses requires knowledge of the detailed movements of wild birds over varying spatial scales. On the one hand, con- currence between the migratory patterns of some Palearctic breeding waterbirds and the spread of the H5N1 HPAI virus across Asia and Europe in the northern fall and winter of 2005/06 illustrates the importance of studies designed to identify specific migratory routes, stopover points and non-breeding areas that may span entire continents. On the other hand, studies documenting the local movements of wild birds between poultry farms and nearby wetlands may be invaluable to establish viable pathways of H5N1 HPAI transmission from poultry to wildlife (or vice versa). Radio telemetry is a technique for determining bird movements over areas ranging in size from the restricted breeding territories of resident bird species to the movement pat- terns of international migratory species (reviewed in Fuller et al. 2005). Radio telemetry has important applications in the investigation of infectious diseases of migratory species, including H5N1 AI virus ecology. Specific objectives for AI-related telemetry studies have already been identified during the FAO-OIE International Scientific Conference on Avian Influenza and Wild Birds in May 200610. In fact, telemetry projects tracking the local move- ments and migration routes of wild birds identified as potential virus hosts are already under way11. The basic concept of a radio telemetry study sounds simple; attach a radio transmitter to an animal and track the signal to determine the animal’s movements. -
Demonstration of Satellite/GPS Telemetry for Monitoring Fine- Scale Movements of Lesser Prairie-Chickens
United States Department of Agriculture Forest Service National Technology & Demonstration of Development Program Inventory and Monitoring 1219 1813—SDTDC Satellite/GPS Telemetry December 2012 for Monitoring Fine- Scale Movements of Lesser Prairie-Chickens Demonstration of Satellite/GPS Telemetry for Monitoring Fine-Scale Movements of Lesser Prairie-Chickens Rey Farve, Project Leader Forest Service San Dimas Technology & Development Center December 2012 The information contained in this publication has been developed for the guidance of employees of the Forest Service, U.S. Department of Agriculture, its contractors, and cooperating Federal and State agencies. The Forest Service assumes no responsibility for the interpretation or use of this information by other than its own employees. The use of trade, firm, or corporation names is for the information and convenience of the reader. Such use does not constitute an official evaluation, conclusion, recommendation, endorsement, or approval of any product or service to the exclusion of others that may be suitable. The U.S. Department of Agriculture (USDA) prohibits discrimination in all its programs and activities on the basis of race, color, national origin, age, disability, and where applicable, sex, marital status, familial status, parental status, religion, sexual orientation, genetic information, political beliefs, reprisal, or because all or part of an individual’s income is derived from any public assistance program. (Not all prohibited bases apply to all programs.) Persons with disabilities who require alternative means for communication of program information (Braille, large print, audiotape, etc.) should contact USDA’s TARGET Center at (202) 720-2600 (voice and TDD). To file a complaint of discrimination, write USDA, Director, Office of Civil Rights, 1400 Independence Avenue, S.W., Washington, D.C. -
Development and Testing of Metop-Sg Solar Array Drive Mechaism
DEVELOPMENT AND TESTING OF METOP-SG SOLAR ARRAY DRIVE MECHAISM Aksel Elkjaer (1) (2), Lars Helge Surdal (1) (1) Kongsberg Defence & Aerospace (KDA), PO1003, N-3601 Kongsberg, NORWAY (2) Norwegian University of Science and Technology (NTNU), NO-7491 Trondheim, NORWAY, Email: [email protected] ABSTRACT The following sections are grouped into two chapters; §2 Design Drivers presents specific technical This paper presents the development process of the requirements and the design developments that occurred KARMA5-SG Solar Array Drive Mechanism (SADM) during preliminary and critical design reviews. The for delivery to MetOp-SG satellites. The mechanism second chapter, §3 Test Results, details test setups, development is recounted with respect to key design results and non-conformances. drivers and experiences from their subsequent test verification are shared. Design drivers relating to structural, thermal and driveline performance are detailed in the context of a flight program development. Practical experiences from testing are reported and specific challenges from non-conformances are highlighted. A description of test setups and results for functional, vibration and thermal requirements are presented. The purpose of the paper is to share practices and offer lessons learned. 1 INTRODUCTION Delivery to flight programs entails demanding programmatic constraints. As such technology maturity Figure 1. KARMA5-SG MetOp-SG SADM is prioritised to assure schedule constraints. Nevertheless, system development leads to eventual 2 DESIGN DRIVERS changes that impact design decisions and success rests The purpose of the SADM is to provide precise and on the collaboration of all stakeholders. This paper smooth positioning of the solar array whilst transferring provides experiences from the development of MetOp- the electrical power it generates into the satellite. -
→ Space for Europe European Space Agency
number 149 | February 2012 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams → by elaborating and implementing a long-term European space policy, by Director General: J.-J. Dordain recommending space objectives to the Member States, and by concerting the policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States. -
Esa Broch Envisat 2.Xpr Ir 36
ENVISAT-1 Mission & System Summary ENVISAT-1 ENVISAT-1 Mission & System Summary Issue 2 Table of contents Table Table of contents 1 Introduction 3 Mission 4 System 8 Satellite 16 Payload Instruments 26 Products & Simulations 62 FOS 66 PDS 68 Overall Development and Verification Programme 74 Industrial Organization 78 Introduction Introduction 3 The impacts of mankind’s activities on the Earth’s environment is one of the major challenges facing the The -1 mission constists of three main elements: human race at the start of the third millennium. • the Polar Platform (); • the -1 Payload; The ecological consequences of human activities is of • the -1 Ground Segment. major concern, affecting all parts of the globe. Within less than a century, induced climate changes The development was initiated in 1989 as may be bigger than what those faced by humanity over a multimission platform; the -1 payload the last 10000 years. The ‘greenhouse effect’, acid rain, complement was approved in 1992 with the final the hole in the ozone layer, the systematic destruction decision concerning the industrial consortium being of forests are all triggering passionate debates. taken in March 1994. The -1 Ground Concept was approved in September 1994. This new awareness of the environmental and climatic changes that may be affecting our entire planet has These decisions resulted in three parallel industrial considerably increased scientific and political awareness developments, together producing the overall -1 of the need to analyse and understand the complex system. interactions between the Earth’s atmosphere, oceans, polar and land surfaces. The development, integration and test of the various elements are proceeding leading to a launch of the The perspective being able to make global observations -1 satellite planned for the end of this decade. -
Space-Based Telemetry and Range Safety Project Ku-Band and Ka-Band Phased Array Antenna
NASA/TM-2005-212872 Space-Based Telemetry and Range Safety Project Ku-Band and Ka-Band Phased Array Antenna Donald E. Whiteman NASA Dryden Flight Research Center Edwards, California Lisa M. Valencia NASA John F. Kennedy Space Center Kennedy Space Center, Florida Richard B. Birr ASRC Aerospace Corporation NASA John F. Kennedy Space Center Kennedy Space Center, Florida July 2005 The NASA STI Program Office…in Profile Since its founding, NASA has been dedicated •CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA Scientific and Technical technical conferences, symposia, seminars, Information (STI) Program Office plays a key or other meetings sponsored or co-sponsored part in helping NASA maintain this by NASA. important role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program Office is operated by technical, or historical information from Langley Research Center, the lead center for NASA programs, projects, and missions, NASA’s scientific and technical information. often concerned with subjects having The NASA STI Program Office provides access substantial public interest. to the NASA STI Database, the largest collection of aeronautical and space science STI in the • TECHNICAL TRANSLATION. English- world. The Program Office is also NASA’s language translations of foreign scientific institutional mechanism for disseminating the and technical material pertinent to results of its research and development activities. NASA’s mission. These results are published by NASA in the NASA STI Report Series, which includes the Specialized services that complement the STI following report types: Program Office’s diverse offerings include creating custom thesauri, building customized databases, organizing and publishing research • TECHNICAL PUBLICATION. -
The EUMETSAT Polar System 13+ Successful Years of Global Observations for Operational Weather Prediction and Climate Monitoring K
Article The EUMETSAT Polar System 13+ Successful Years of Global Observations for Operational Weather Prediction and Climate Monitoring K. Dieter Klaes, Jörg Ackermann, Craig Anderson, Yago Andres, Thomas August, Régis Borde, Bojan Bojkov, Leonid Butenko, Alessandra Cacciari, Dorothée Coppens, Marc Crapeau, Stephanie Guedj, Olivier Hautecoeur, Tim Hultberg, Rüdiger Lang, Stefanie Linow, Christian Marquardt, Rosemarie Munro, Carlo Pettirossi, Gabriele Poli, Francesca Ticconi, Olivier Vandermarcq, Mayte Vasquez, and Margarita Vazquez-Navarro ABSTRACT: After successful launch in November 2018 and successful commissioning of Metop-C, all three satellites of the EUMETSAT Polar System (EPS) are in orbit together and operational. EPS is part of the Initial Joint Polar System (IJPS) with the United States (NOAA) and provides the service in the midmorning orbit. The Metop satellites carry a mission payload of sounding and imaging instruments, which allow provision of support to operational meteorology and climate monitoring, which are the main mission objectives for EPS. Applications include numerical weather prediction, atmospheric composition monitoring, and marine meteorology. Climate monitoring is supported through the generation of long time series through the program duration of 20+ years. The payload was developed and contributed by partners, including NOAA, CNES, and ESA. EUMETSAT and ESA developed the space segment in cooperation. The system has proven its value since the first satellite Metop-A, with enhanced products at high reliability