Aquarius to Scrutinize Ocean Salinity
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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. - 
											
The Rovers' Tale
Vol 436|11 August 2005 BOOKS & ARTS The rovers’ tale How NASA scientists overcame the odds to find signs of water on Mars. Roving Mars: Spirit, Opportunity, and the Exploration of the Red Planet by Steve Squyres JPL/NASA Hyperion: 2005. 432 pp. $25.95 Gregory Benford Roving Marsis a deftly and dramatically writ- ten history of the Mars rovers, Spirit and Opportunity. It is also a primer on how to do exotic geology at a distance of 100 million miles using robots. Steve Squyres knows how to render scenes and intricate technical detail to build tension, without losing sight of the thrill and grind of the groundbreaking work. “Eleven years had passed since I had started trying to send hardware to Mars, and in all that time I hadn’t seen a single plan for Mars explo- ration survive for more than about eighteen months before there was some sort of cata- clysm,” writes Squyres. Chief among these was the loss of the 1999 Mars Climate Orbiter: “The Mars program had become so screwed up that nobody had caught a high-school mis- take like mixing up English and metric units.” NASA doesn’t escape criticism over the rover mission either. According to Squyres, NASA’s On a roll: during testing for manoeuvrability in the lab, the rovers overcame a series of obstacles. rules meant that “cutting corners and taking chances” were the Jet Propulsion Laboratory’s The team had to trim experiments and patch signs of ancient surface water and found it, only management tools. After the losses of the problems right up to the launch date. - 
												
												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. - 
												
												Planetary Report Report
The PLANETARYPLANETARY REPORT REPORT Volume XXIX Number 1 January/February 2009 Beyond The Moon From The Editor he Internet has transformed the way science is On the Cover: Tdone—even in the realm of “rocket science”— The United States has the opportunity to unify and inspire the and now anyone can make a real contribution, as world’s spacefaring nations to create a future brightened by long as you have the will to give your best. new goals, such as the human exploration of Mars and near- In this issue, you’ll read about a group of amateurs Earth asteroids. Inset: American astronaut Peggy A. Whitson who are helping professional researchers explore and Russian cosmonaut Yuri I. Malenchenko try out training Mars online, encouraged by Mars Exploration versions of Russian Orlan spacesuits. Background: The High Rovers Project Scientist Steve Squyres and Plane- Resolution Camera on Mars Express took this snapshot of tary Society President Jim Bell (who is also head Candor Chasma, a valley in the northern part of Valles of the rovers’ Pancam team.) Marineris, on July 6, 2006. Images: Gagarin Cosmonaut Training This new Internet-enabled fun is not the first, Center. Background: ESA nor will it be the only, way people can participate in planetary exploration. The Planetary Society has been encouraging our members to contribute Background: their minds and energy to science since 1984, A dust storm blurs the sky above a volcanic caldera in this image when the Pallas Project helped to determine the taken by the Mars Color Imager on Mars Reconnaissance Orbiter shape of a main-belt asteroid. - 
												
												On the Use of Scatterometer Winds in Nwp
ON THE USE OF SCATTEROMETER WINDS IN NWP Ad Stoffelen KNMI, de Bilt, the Netherlands, Email: [email protected] Lars Isaksen, Didier le Meur ECMWF, Reading, UK ABSTRACT Over the last years the processing of ERS scatterometer winds has been refined. Subsequently, High Resolution Limited Area Model, HIRLAM, and ECMWF model data assimilation experiments have been carried out to assess the impact of one scatterometer, ERS-1 and of two scatterometers, ERS-1 and ERS-2, on the analyses and forecasts. We found that scatterometer winds have a clear and beneficial impact in the data assimilation cycle and on the forecasts. Furthermore, ECMWF has shown that ERS scatterometer data improve the prediction of tropical cyclones in 4Dvar, where unprecedented skillful medium-range forecasts result of potential large social-economic value. Nevertheless, scatterometer winds contain much sub-synoptic scale information where the smallest scales resolved are difficult to assimilate into a Numerical Weather Prediction, NWP, model. This is mainly due to the otherwise general sparsity of the observing system over the ocean. In line with this it is found that scatterometer data coverage is very important for obtaining a large impact. In that respect future scatterometer systems such as SeaWinds on QuikSCAT and ADEOS- II, and ASCAT on EPS are promising. 1. INTRODUCTION After the launch of ERS-1 much improvement has been made in the interpretation of scatterometer backscatter measurements and a good quality wind product has emerged (Stoffelen and Anderson, 1997a, 1997b and 1997c). The consistency of the scatterometer winds over the swath makes them particularly useful for nowcasting purposes and several examples of the usefulness of the direct visual presentation of scatterometer winds to a meteorologist can be given. - 
												
												ASCAT – Metop's Advanced Scatterometer
ascat ASCAT – Metop’s Advanced Scatterometer R.V. Gelsthorpe Earth Observation Programmes Development Department, ESA Directorate of Application Programmes, ESTEC, Noordwijk, The Netherlands E. Schied Dornier Satelllitensysteme*, Friedrichshafen, Germany J.J.W. Wilson Eumetsat, Darmstadt, Germany Introduction Figure 1 indicates the form of the variation of Wind scatterometers already flown on ESA’s backscattering coefficient with relative wind ERS-1 and ERS-2 satellites have demonstrated direction (at a fixed incidence angle) for a range the value of such instruments for the global of wind speeds. determination of sea-surface wind vectors. These highly successful instruments – part of If an instrument were to be constructed that the Active Microwave Instrument (AMI) – were determined the sea-surface backscattering conceived about twenty years ago. During coefficient from a single look direction, the the intervening period, there has been a overlapping nature of the curves would limit considerable evolution in the capabilities of its capabilities to providing a rather coarse spaceborne hardware. estimate of wind speed and no information on wind direction. The earliest successful space- ASCAT is an advanced scatterometer that will fly as part of the borne wind scatterometer, that of Seasat, used payload of the Metop satellites, which in turn form part of the two dual-polarised antennas pointed at 45 and Eumetsat Polar System. It is developed by Dornier Satellitensysteme 135 deg with respect to the satellite’s direction under the leadership of Matra Marconi Space**, the satellite Prime of flight to determine sea-surface scattering Contractor, for ESA. From its polar orbit, ASCAT will measure sea- coefficients from two directions separated by surface winds in two 500 km wide swaths and will achieve global 90 deg. - 
												
												Educator's Guide
EDUCATOR’S GUIDE ABOUT THE FILM Dear Educator, “ROVING MARS”is an exciting adventure that This movie details the development of Spirit and follows the journey of NASA’s Mars Exploration Opportunity from their assembly through their Rovers through the eyes of scientists and engineers fantastic discoveries, discoveries that have set the at the Jet Propulsion Laboratory and Steve Squyres, pace for a whole new era of Mars exploration: from the lead science investigator from Cornell University. the search for habitats to the search for past or present Their collective dream of Mars exploration came life… and maybe even to human exploration one day. true when two rovers landed on Mars and began Having lasted many times longer than their original their scientific quest to understand whether Mars plan of 90 Martian days (sols), Spirit and Opportunity ever could have been a habitat for life. have confirmed that water persisted on Mars, and Since the 1960s, when humans began sending the that a Martian habitat for life is a possibility. While first tentative interplanetary probes out into the solar they continue their studies, what lies ahead are system, two-thirds of all missions to Mars have NASA missions that not only “follow the water” on failed. The technical challenges are tremendous: Mars, but also “follow the carbon,” a building block building robots that can withstand the tremendous of life. In the next decade, precision landers and shaking of launch; six months in the deep cold of rovers may even search for evidence of life itself, space; a hurtling descent through the atmosphere either signs of past microbial life in the rock record (going from 10,000 miles per hour to 0 in only six or signs of past or present life where reserves of minutes!); bouncing as high as a three-story building water ice lie beneath the Martian surface today. - 
												
												Emerging Technologies 1 for Human Mars Exploration
Emerging Technologies 1 for Human Mars Exploration Michelle Rucker Mars Study Capability Team NASA Johnson Space Center IEEE Aerospace Conference 2018 March, 2018 Human Explorers on Mars 2 have different needs than rovers Power Life Support Health Care Shelter Communication Earth Return Image courtesy NASA/JPL-Caltech IEEE Aerospace Conference 2018 March, 2018 Humans 3 need a lot more power! Rovers can hibernate…humans cannot . Mars rovers need less than 25 Watts (W) keep-alive power • Less than 650 W at peak loads . Human explorers may need as much as 40 kiloWatts (kW) for 300+ day surface missions • As much as 25 kW keep-alive power • Apollo missions were ~4 kW for 3 days . Kilopower Fission Power . High density energy storage . Robotic power connections IEEE Aerospace Conference 2018 March, 2018 Humans 4 need Life Support Systems! Rovers don’t need food, oxygen, water, bathrooms, or spacesuits . Closed-loop life support systems . Advanced water/air monitoring . Advanced waste management . Extended shelf-life food systems . New planetary spacesuits IEEE Aerospace Conference 2018 March, 2018 Humans 5 need Health Care! Rovers don’t get sick . Space radiation protection . Reduced gravity countermeasures . Autonomous medicine + non-physician training . In situ sample analysis, health monitoring IEEE Aerospace Conference 2018 March, 2018 Humans 6 need to come inside! Rovers don’t mind living outside . Reduced pressure . Temperature extremes . Months-long dust storms . Radiation . Long-duration habitats . Pressurized Rovers IEEE Aerospace Conference 2018 March, 2018 Humans 7 need to connect with loved ones! Isolation doesn’t bother a rover MARS . Up to 44 minutes delay between asking MARS EARTH Min. - 
												
												Tuesday, May 3Rd, Naresh Pai, University of Arkansas Poster Presenters Will Also Be Discussing Their Information
My Day-at-a-Glance Time Event Room Attending 7:00 AM to 5:45 PM Registration Desk Open Mezzanine Level Atrium 7:00 AM to 7:00 PM Posters Open 301 C 8:00 AM to 9:15 AM Technical Program — Keynote Address 104 D 8:00 AM to 5:00 PM Career Interview Room Open 201 D 9:30 AM to 11:00 AM Technical Sessions — 1 to 11 varies, see description 9:30 AM to 11:00 AM Poster Presentation I 203 A 10:00 AM to 7:00 PM Exhibit Hall Opens Exhibit Hall 301 C 11:15 AM to 12:15 PM Hot Topics varies, see description 12:15 PM to 1:30 PM 22nd Annual Awards Luncheon & 77th Installation of ASPRS Officers Ballroom 104 D 1:30 PM to 3:00 PM Technical Sessions — 12 to 21 varies, see description 1:30 PM to 3:00 PM Poster Presentation II 203 A 2:30 PM to 3:30 PM Student & Young Professionals Event — Exhibit Hall Guided Tour for Students Exhibit Hall 301 C 3:30 PM to 5:00 PM Technical Sessions — 22 to 30 varies, see description 3:30 PM to 5:00 PM Poster Presentation III 203 A 5:30 PM to 7:00 PM Exhibitors’ Welcome Reception Exhibit Hall 301 C 7:00 PM Espionage for a Great Cause Offsite The National Geospatial-Intelligence Agency (NGA) has organized a special unclassified track to run on Tuesday and Wednesday during the technical sessions. There are four special sessions, each followed by an open discussion session, in order for NGA to get important information and feedback from attendees. - 
												
												Cassini RADAR Sequence Planning and Instrument Performance Richard D
IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING, VOL. 47, NO. 6, JUNE 2009 1777 Cassini RADAR Sequence Planning and Instrument Performance Richard D. West, Yanhua Anderson, Rudy Boehmer, Leonardo Borgarelli, Philip Callahan, Charles Elachi, Yonggyu Gim, Gary Hamilton, Scott Hensley, Michael A. Janssen, William T. K. Johnson, Kathleen Kelleher, Ralph Lorenz, Steve Ostro, Member, IEEE, Ladislav Roth, Scott Shaffer, Bryan Stiles, Steve Wall, Lauren C. Wye, and Howard A. Zebker, Fellow, IEEE Abstract—The Cassini RADAR is a multimode instrument used the European Space Agency, and the Italian Space Agency to map the surface of Titan, the atmosphere of Saturn, the Saturn (ASI). Scientists and engineers from 17 different countries ring system, and to explore the properties of the icy satellites. have worked on the Cassini spacecraft and the Huygens probe. Four different active mode bandwidths and a passive radiometer The spacecraft was launched on October 15, 1997, and then mode provide a wide range of flexibility in taking measurements. The scatterometer mode is used for real aperture imaging of embarked on a seven-year cruise out to Saturn with flybys of Titan, high-altitude (around 20 000 km) synthetic aperture imag- Venus, the Earth, and Jupiter. The spacecraft entered Saturn ing of Titan and Iapetus, and long range (up to 700 000 km) orbit on July 1, 2004 with a successful orbit insertion burn. detection of disk integrated albedos for satellites in the Saturn This marked the start of an intensive four-year primary mis- system. Two SAR modes are used for high- and medium-resolution sion full of remote sensing observations by a dozen instru- (300–1000 m) imaging of Titan’s surface during close flybys. - 
												
												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. - 
												
												High-Resolution Land/Ice Imaging Using Seasat Scatterometer Measurements
HIGH-RESOLUTION LAND/ICE IMAGING USING SEASAT SCATTEROMETER MEASUREMENTS D. G. Long*, P. T. Whiting1, P. J. Hardin2 Electrical and Computer Engineering Department, 'Geography Department Brigham Young University, Provo, UT 84602 ABSTRACT is the measurement number) is a weighted average of the bo's of the individual high-resolution elements covered by the measurement, i.e., In this paper we introduce a new method for obtaining high res- olution images (to 4 km) of the land backscatter from low-resolution Seasat-A scatterometer (SASS) measurements. The method utilizes the measurement cell overlap in multiple spacecraft passes over the c=Lk e=Bk region of interest and signal processing techniques to generate high resolution images of the radar backscatter. The overlap in the 0' res- where Lk, Rk, Tk,and Bk define a bounding rectangle for the kth olution cells is exploited to estimate the underlying high resolution hexagonal U' measurement cell, h(c,a; IC) is the weighting function surface radar backscatter characteristics using a robust new mul- for the (c, a)th high-resolution element, and uo(c,a; k)is the 0" value tivariate image reconstruction algorithm. The new algorithm has for the (c, a)th high-resolution element. The incidence angle depen- been designed to operate in the high noise environment typical of dence of d' and h is subsumed in the k index. [In Eq. (2) c denotes scatterometer measurements. The ultimate resolution obtainable is the cross-track dimension while a denotes the along-track dimen- a function of the number of measurements and the measurement sion.] Over a given scatterometer measurement cell the incidence overlap.