EOS MLS Cloud Ice Measurements and Cloudy- Sky Radiative Transfer Model

Total Page:16

File Type:pdf, Size:1020Kb

EOS MLS Cloud Ice Measurements and Cloudy- Sky Radiative Transfer Model TRANSACTIONS ON GEOPHYSICS AND REMOTE SENSING 1 EOS MLS Cloud Ice Measurements and Cloudy- Sky Radiative Transfer Model Dong L. Wu, Jonathan H. Jiang, and Cory P. Davis Remote sensing of ice clouds with passive microwave Abstract— EOS MLS (Earth Observing System Microwave radiometers is a relatively new research area. A number of Limb Sounder) on the NASA Aura satellite observes upper researchers have attempted to retrieve cloud ice water path tropospheric clouds at frequencies near 118, 190, 240, 640 GHz, (IWP) from nadir-viewing radiances using cloud scattering and 2.5 THz. This paper describes MLS cloud measurement signatures [5,6,7,8,9]. Combined radar-radiometer approaches principles, the methods for cloud detection, and radiative can be used to improve cloud ice measurements with better transfer models used for interpreting and retrieving cloud vertical resolution but the retrieved IWC profiles are limited to properties. MLS 240 GHz data have been used to retrieve ice water content at pressures < 215 hPa. Some early results are airborne radar sampling [10]. shown here and the observed cloud effects are consistent with the This paper describes a cloud ice observing technique with expectation from model simulations in general. Significant cloud- EOS MLS (Earth Observing System Microwave Limb induced radiances are observed at 2.5 THz. The cloud scattering Sounder) on Aura. Cloud radiance characteristics as well as signatures at 122 GHz are polarized but the polarization measurement principles used for cloud ice retrievals are differences are typically less than 10% of the total cloud-induced discussed. EOS MLS employs the limb-viewing technique radiance. with high-frequency narrow beamwidth receivers to achieve better vertical resolution and sensitivity than nadir sounding Index Terms—satellite, microwave, cloud, limb sounding, ice [11][12]. Under limb-viewing geometry the radiative transfer water content, polarization (RT) is greatly simplified, involving only the atmosphere and clouds. These advantages yield better accuracy for cloud detection at high altitudes. I. INTRODUCTION Launched on 15 July 2004, EOS MLS has observed clouds louds play important roles in modulating the Earth’s in all the radiometers and is producing cloud IWC C dynamical, hydrological, radiative, and chemical measurements at pressures < 215 hPa. Cloud IWC and processes [1,2,3,4]. Despite terabytes of satellite cloud horizontal ice water path (hIWP) along the instrument line-of- imagery, our understanding of cloud properties and vertical light (LOS) are two primary cloud products from EOS MLS distributions remain limited, especially on ice clouds in the [Figure 1]. The IWC in the upper troposphere (UT) is upper troposphere. One of the poorly known cloud variables is retrieved from high tangent height (ht) single-frequency ice water content (IWC), which is difficult to measure from measurements assuming spherical homogeneity. This space. Visible/IR techniques are sensitive only to the assumption implies that the MLS IWC represent a volume uppermost cloud layer and often saturated by dense clouds; whereas low-frequency microwave sensors are insensitive to most of ice clouds. To overcome both penetration and sensitivity shortcomings, high-frequency microwave radiometry emerges as a promising technique for observing ice clouds in the upper troposphere. Manuscript received October 9, 2005. This work was performed at the Jet Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration (NASA). Dong L. Wu is with the Jet Propulsion Laboratory, California Institute of Figure 1. Cloud ice observations in limb viewing geometry. At Technology, Pasadena, California, USA (phone: 818-393-1954; fax: 818-393- high tangent heights, where limb radiation is optically thin for 5065; e-mail: [email protected]). window channels, single-frequency radiances are used to retrieve Jonathan H. Jiang is with the Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA (e-mail: IWC at pressures < 215 hPa. At low tangent heights, where limb [email protected]). radiation is optically thick, multiple frequency radiances with Cory P. Davis is with the Institute of Atmospheric and Environmental different penetration depths are used to infer hIWP along the Science, School of GeoSciences, University of Edinburgh, Edinburgh EH9 LOS. 3JZ, Scotland, UK. (e-mail: [email protected]). TRANSACTIONS ON GEOPHYSICS AND REMOTE SENSING 2 average over the instrument’s field-of-view (FOV). The hIWP crossing time of ~1:40 p.m. Excluding instrument calibration, is retrieved from low-ht measurements using multiple each MAF devotes ~120 MIFs for atmospheric measurements frequencies with different penetration depths. Each hIWP with a integration time of 1/6 second for a MIF. In the represents a column in the LOS direction that is nearly nominal operation [14], the GHz radiometers have ~42 MIFs horizontally with an elevation angle of ~3º. In most cases the dedicated to tropospheric measurements (separated by ~300 m MLS hIWP column does not reach the surface due to strong in ht), whereas the THz scan has only ~7 MIFs at ht < 18 km atmospheric absorption along the limb path, but in the polar [15]. regions where air is often dry, the low-ht radiances can reach Clouds reside mostly in the troposphere and occasionally the surface. shoot up to ~18 km. As a result, MLS radiances can be The retrieval technique using high-h radiances has t affected by clouds when viewing at h < ~19 km for the previously applied to UARS (Upper Atmosphere Research t instrument FOV is not infinitesimal. The measured cloud Satellite) MLS 203 GHz data, from which the 100 hPa cloud fields are subject to substantial horizontal smearing due to a ice was derived and studied for the period of 1991-1997 [13]. This work extends the cloud observing technique to EOS long (~200 km) limb path along the LOS. MLS frequencies, and the paper is organized to discuss cloud B. Radiance Uncertainties characteristics in EOS MLS radiances in section II, followed MLS clear-sky algorithms use radiance spectral variations by a description of the cloudy-sky RT model in section III. to measure gas abundances, and therefore spectrally-flat Preliminary MLS cloud observations are highlighted in radiance error has little impact on the quality of the gas section IV. measurements. The cloud measurements, however, depend critically on the absolute radiance value or accuracy of II. EOS MLS CLOUD MEASUREMENTS radiometric calibration. Thus, understanding noise accuracy is A. The EOS MLS Experiment very important for reliable cloud retrieval. Noise EOS MLS is a passive instrument that consists of seven characteristics and calibration issues are detailed in [14][15]. radiometers at frequencies near 118, 190, 240, 640 GHz, and The radiance accuracy can be affected by several factors, 2.5 THz [12][14]. There are dual polarizations for the 118 including errors in baseline, gain, and sideband ratio. The GHz and 2.5 THz receivers. Except for the 118 GHz baseline radiance may come from antenna’s ohmic emissions radiometer, all are double-sideband receivers with key and spillovers that can be removed effectively on a MAF-by- parameters specified in Table I. The GHz and THz systems MAF basis, using the measurements at ht > 85 km [14]. have separate antennas but are synchronized in sampling such Although the gain is calibrated every MAF, it can be noisy that they both produce 240 scans, or major frames (MAFs), in and affected by the sidelope/spillover radiation not accounted each orbit. Each MAF is further divided to 148 minor frames for. The radiometer sideband ratios were measured during pre- (MIFs). Unlike step-scanning with UARS MLS, EOS MLS launch testing but to the accuracy of 0.5-2%. The precision of scans are continuous in tangent height from the surface to the MLS radiances consists of two components, frequency- mesopause (~92 km) in 24.7s. Two adjacent scans are correlated and random, which can be expressed in terms of separated by ~165 km in distance. The latitude coverage variance as follows ranges from 82ºS to 82ºN with a sun-synchronous ascending Table I. Characteristics of the EOS MLS radiometers. Both vertical and horizontal FOVs are estimated at ht = 1 km. MLS Radiometera Polarization Estimated Vertical Cross-Track (frequency range in GHz) 0º = V pol Min. Errb FOV FOV 90º = H pol (K) (km) (km) R1A (115-122) 0º ± 0.5º 0.3 6.5 13 R1B (115-122) 90º ± 0.5º 0.5 6.5 13 R2 (178-184, 200-207) 0º ± 0.5º 0.3 4.5 9 R3 (230-237, 243-250) 90º ± 0.5º 0.2 3.5 7 R4 (625-637, 649-661) 90º ± 0.5º ~2 1.5 3 R5H (2501-2515, 2531-2544) ~113º ~4 2.5 2.5 R5V (2501-2515, 2531-2544) ~23º ~3 2.5 2.5 a) The two frequency ranges in R2, R3, R4, R5H and R5V reflect the receiver’s double-sideband coverage although radiances from two sidebands are inseparable in the radiometric measurements. R1A and R1B are single sideband radiometers with orthogonal polarizations. b) MLS radiance error contains frequency-correlated and random components. The latter can be reduced by averaging radiances from different frequency channels with the radiometer but the correlated component cannot by reduced by averaging, eventually becoming the dominant radiance uncertainty. Values in this column, the minimum radiance error per MIF, reflect such limit after the frequency averaging is applied. TRANSACTIONS ON GEOPHYSICS AND REMOTE SENSING 3 σ 2 = σ 2 + σ 2 (1) important for reliable cloud detection. fc r The basic cloud measurement is called cloud-induced 2 where the random componentσ r is proportional to the radiance (Tcir), defined as the difference between the inverse of the bandwidth and integration time product. For measured radiance and an estimated clear-sky background.
Recommended publications
  • Articles Upon the Hox Family by Comparing Averages of Days Impacted by These Events with Averages of Non-Impacted 3945–3977, Doi:10.5194/Acp-13-3945-2013, 2013
    Atmos. Chem. Phys., 15, 2889–2902, 2015 www.atmos-chem-phys.net/15/2889/2015/ doi:10.5194/acp-15-2889-2015 © Author(s) 2015. CC Attribution 3.0 License. Stratospheric and mesospheric HO2 observations from the Aura Microwave Limb Sounder L. Millán1,2, S. Wang2, N. Livesey2, D. Kinnison3, H. Sagawa4, and Y. Kasai4 1Joint Institute for Regional Earth System Science and Engineering, University of California, Los Angeles, California, USA 2Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA 3National Center for Atmospheric Research, Boulder, Colorado, USA 4National Institute of Information and Communications Technology, Koganei, Tokyo, Japan Correspondence to: L. Millán ([email protected]) Received: 18 June 2014 – Published in Atmos. Chem. Phys. Discuss.: 8 September 2014 Revised: 17 February 2015 – Accepted: 24 February 2015 – Published: 13 March 2015 Abstract. This study introduces stratospheric and meso- sphere where O3 chemistry is controlled by catalytic cycles spheric hydroperoxyl radical (HO2) estimates from the Aura involving the HOx (HO2, OH and H) family (Brasseur and Microwave Limb Sounder (MLS) using an offline retrieval Solomon, 2005): (i.e. run separately from the standard MLS algorithm). This new data set provides two daily zonal averages, one during X C O3 ! XO C O2 (R1) daytime from 10 to 0.0032 hPa (using day-minus-night dif- O C XO ! O2 C X; (R2) ferences between 10 and 1 hPa to ameliorate systematic bi- ases) and one during nighttime from 1 to 0.0032 hPa. The where the net effect of these two reactions is simply vertical resolution of this new data set varies from about 4 km O C O ! 2O (R3) at 10 hPa to around 14 km at 0.0032 hPa.
    [Show full text]
  • The Space-Based Global Observing System in 2010 (GOS-2010)
    WMO Space Programme SP-7 The Space-based Global Observing For more information, please contact: System in 2010 (GOS-2010) World Meteorological Organization 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int WMO Space Programme Office Tel.: +41 (0) 22 730 85 19 – Fax: +41 (0) 22 730 84 74 E-mail: [email protected] Website: www.wmo.int/pages/prog/sat/ WMO-TD No. 1513 WMO Space Programme SP-7 The Space-based Global Observing System in 2010 (GOS-2010) WMO/TD-No. 1513 2010 © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0)22 730 84 03 P.O. Box No. 2300 Fax: +41 (0)22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] FOREWORD The launching of the world's first artificial satellite on 4 October 1957 ushered a new era of unprecedented scientific and technological achievements. And it was indeed a fortunate coincidence that the ninth session of the WMO Executive Committee – known today as the WMO Executive Council (EC) – was in progress precisely at this moment, for the EC members were very quick to realize that satellite technology held the promise to expand the volume of meteorological data and to fill the notable gaps where land-based observations were not readily available.
    [Show full text]
  • Version 2.2 Level 2 Data Quality and Description Document
    JPL D-33509 Earth Observing System (EOS) Aura Microwave Limb Sounder (MLS) Version 2.2 Level 2 data quality and description document. 0 70 N FWHM / km FWHM / km -2 0 2 4 6 8 10 12 0 100 200 300 400 500 600 0.1 1.0 10.0 Pressure / hPa 100.0 1000.0 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 1.2 -2 -1 0 1 2 Kernel, Integrated kernel Profile number Equator FWHM / km FWHM / km -2 0 2 4 6 8 10 12 0 100 200 300 400 500 600 0.1 1.0 10.0 Pressure / hPa 100.0 1000.0 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 1.2 -2 -1 0 1 2 Kernel, Integrated kernel Profile number Nathaniel J. Livesey, William G. Read, Alyn Lambert, Richard E. Cofield, David T. Cuddy, Lucien Froidevaux, Ryan A Fuller, Robert F. Jarnot, Jonathan H. Jiang, Yibo B. Jiang, Brian W. Knosp, Laurie J. Kovalenko, Herbert M. Pickett, Hugh C. Pumphrey, Michelle L. Santee, Michael J. Schwartz, Paul C. Stek, Paul A. Wagner, Joe W. Waters, and Dong L. Wu. Version 2.2x-1.0a May 22, 2007 Jet Propulsion Laboratory California Institute of Technology Pasadena, California, 91109-8099 Where to find answers to key questions This document serves two purposes. Firstly, to Do not use data for any profile where the field • summarize the quality of version 2.2 (v2.2) EOS MLS Status is an odd number. Level 2 data.
    [Show full text]
  • Chapter 7 Instrument Packages
    Chapter 7 Instrument Packages Richard E. Cofield, William A. Imbriale, and Richard E. Hodges This chapter describes antennas used on various instrument packages for science spacecraft. The instruments have been primarily used for the Earth Observing System (EOS), a series of spacecraft to observe Earth from the unique vantage point of space. This chapter includes radiometers (7.1–7.3), scatterometers (7.4), radars (7.5), and altimeters (7.6). 7.1 Radiometers Richard E. Cofield Radiometry is the measurement of electromagnetic radiation using highly sensitive receivers. The blackbody radiation spectrum given by Planck’s radiation law provides a reference against which the radiation spectra of real bodies at the same physical temperature are compared. The spectral, polarization, and angular variations of a scene of interest are dictated by the geometrical configuration and physical properties (dielectric and thermal) of surfaces and interior regions of (1) the materials under study, and (2) the medium (atmosphere or space) through which we make observations. Radiometer parameters (such as frequency, viewing angle, and polarization) can be chosen to relate the radiometer’s output signal strength to properties of the observed scenes. This section describes passive microwave radiometry from spaceborne instruments developed at Jet Propulsion Laboratory (JPL): passive in contrast to active (radio detection and ranging [radar] or laser induced differential absorption radar [lidar]) systems such as altimeters and the scatterometers discussed below, and microwave as a consequence of Planck’s law at the 341 342 Chapter 7 temperature ranges of natural emitters. Hence, it is convenient to express radiometric signals (radiant power per unit bandwidth) as radiances having units of temperature (kelvin, or K).
    [Show full text]
  • Laser Video Demo on Space Station Aims to Vastly Improve Downlink Rates by Mark Whalen
    Jet FEBRUARY Propulsion 2014 Laboratory VOLUME 44 NUMBER 2 Breaking the bottleneck Laser video demo on Space Station aims to vastly improve downlink rates By Mark Whalen Technicians at Kennedy Space Center unload and inspect the Optical Payload for Lasercomm Science payload after its arrival last summer. It’s scheduled to launch no earlier than March 1. Sometime in the near future, a group of young The 90-day mission is JPL’s first payload to be JPL engineers could look back on 2014 not only as mounted on the outside of the space station (two the early days of their careers but also as the time others have gone inside), and the first to launch on they were part of critical research that’s one of the a SpaceX vehicle. When the Dragon capsule docks keys to NASA’s future success. with the station, OPALS will be robotically extracted A group of about 20 JPLers in the lab’s Phaeton from the trunk of the Dragon, then manipulated by a early-career-hire program contributed to the Optical robotic arm for positioning. Payload for Lasercomm Science, or OPALS, which is The JPL experiment won’t be serviceable from its preparing for a March 1 launch from Kennedy Space outpost. OPALS could operate for up to two years, Center to the International Space Station. The goal? noted Oaida. To lay the foundation that could boost the rate at What next? If OPALS is successful, the next step which spacecraft send data to Earth by more than a would be to try to miniaturize the technology for factor of 10.
    [Show full text]
  • Sources of Biases in Microwave Radiative Transfer Modelling Peter
    Sources of Biases in Microwave Radiative Transfer Modelling Peter Bauer ECMWF Shinfield Park, Reading, RG2 9AX, UK [email protected] 1. Introduction Microwave satellite observations represent the most important information source for atmospheric temperature and temperature distributions in most current operational numerical weather prediction systems. At ECMWF, most data from the Advanced Microwave Sounding Unit (AMSU) instruments A and B are assimilated from four different satellites of the National Oceanic and Atmospheric Administration (NOAA) polar orbiting series (NOAA-15, 16, (17,) 18) as well as from National Aeronautic and Space NASA’s Aqua satellite. Microwave imager measurements are sensitive to integrated atmospheric moisture, surface properties as well as clouds and precipitation. While advanced infrared sounders offer better vertical resolution for sounding applications, microwave data is less affected by cloud contamination and therefore provides better data coverage. At ECMWF, microwave sounder data is operationally assimilated since 1992 (Eyre et al. 1993) and imager data (Special Sensor Microwave / Imager, SSM/I) since 1999 (Phalippou 1996, Gérard and Saunders 1999). Initially, the assimilation was performed through a 1D-Var retrieval of geophysical variables such as temperature profile or integrated moisture that were then assimilated in the global system as pseudo- observations. This procedure was later replaced by the direct assimilation of radiances in the 4D-Var system (McNally et al. 2000, Bauer et al. 2002). The radiative transfer (RT) modeling was aimed at the Tiros Operational Vertical Sounder (TOVS) data modeling (RTTOV, Eyre 1991) that developed into a general RT modeling tool-kit applicable to most available satellite sensors (Saunders et al.
    [Show full text]
  • 2013 the Year's Highlights, from New Earth Missions to the Interstellar
    Jet DECEMBER Propulsion 2013 Laboratory VOLUME 43 NUMBER 12 Boldly going in 2013 The year’s highlights, from new Earth missions to the interstellar threshold Has 2013 already come and gone? Over the past 12 nitrogen, hydrogen, oxygen, phosphorus and carbon— improve accuracy of weather forecasts and climate months, JPL’s missions moved steadily along—with­­­ a some of the key chemical ingredients of life. The team change studies, is slated for launch next fall. Jason 3 few surprises along the way. looked forward to more as Curiosity rolled toward Mount will keep tabs on ocean surface topography after the Sharp, the peak towering over the center of the crater. satellite launches in early 2015. They all will keep Into the beyond teams busy for years working with new data on Earth. Today Earth, tomorrow Jupiter The Juno spacecraft returned to the planet where it In search of a likely rock was created, but not for long. In October, the Jupiter- bound orbiter skimmed past Earth at a relatively close 559 kilometers (347 miles) in order to gain enough gravi- tational energy to send it on to the solar system’s largest planet. Despite putting itself in a protective safe mode during the close encounter, Juno accomplished a a “near- perfect” trajectory that will deliver it to Jupiter on July 4, 2016. “Are we there yet?” asked Ed Stone, project scientist of JPL’s longest-flying mission. “Yes,” he concluded, “we No need to call Bruce Willis: NASA is on it. When are.” the space agency unveiled its annual budget request in “There” was the outer edge of the solar system, and April, it announced an ambitious new initiative to lasso Stone’s pronouncement came at a September news con- a near-Earth asteroid and nudge it into orbit around ference when the former JPL director and his science Earth’s moon, where it can be studied by visiting astro- colleagues on the Voyager mission announced that Voy- nauts.
    [Show full text]
  • High Performance Computing for Flight Projects at JPL
    National Aeronautics and Space Administration Jet Propulsion Laboratory California Institute of Technology Pasadena, California High Performance Computing for Flight Projects at JPL Chris Catherasoo, Ph.D. California Institute of Technology HPC User Forum Meeting Bruyères-le-Châtel, France 3-4 October 2011 National Aeronautics and Space Administration Jet Propulsion Laboratory Outline California Institute of Technology Pasadena, California . Introduction . JPL and its mission . Current flight projects . HPC resources at JPL . Institutional HPC resources . HPC resources at NASA Ames . Examples of HPC usage by flight projects . Entry, descent and landing simulations . The Phoenix Mars Lander radar ambiguity . Mars Science Laboratory supersonic parachute design . Juno planetary protection trajectory analysis . Future work . Evolutionary computing . Low-thrust orbit optimization 2 HPC for Flight Projects at JPL 3-4 Oct 11 National Aeronautics and Space Administration Jet Propulsion Laboratory Outline California Institute of Technology Pasadena, California . Introduction . JPL and its mission . Current flight projects . HPC resources at JPL . Institutional HPC resources . HPC resources at NASA Ames . Examples of HPC usage by flight projects . Entry, descent and landing simulations . The Phoenix Mars Lander radar ambiguity . Mars Science Laboratory supersonic parachute design . Juno planetary protection trajectory analysis . Future work . Evolutionary computing . Low-thrust orbit optimization 3 HPC for Flight Projects at JPL 3-4 Oct 11 National
    [Show full text]
  • Hal Maring Earth Science Division, Science Mission Directorate November 2013 Atmospheric Composition Research at NASA
    Hal Maring Earth Science Division, Science Mission Directorate November 2013 Atmospheric Composition Research at NASA • How is atmospheric composition changing? Carbon Cycle & • What chemical & Ecosystems (CO2, CH4) physical processes are important for air quality, Climate Variability radiative transfer and & Change (atmospheric climate? constituent effects on climate) • What trends in atmospheric Missions constituents, clouds and Atmospheric cloud properties as well as solar radiation are Models Composition driving global climate? • How do atmospheric Water & Energy trace constituents Technology respond to and affect Cycle (atmospheric water vapor) global environmental change? • How will changes in Earth Surface & atmospheric Interior (volcanic composition affect effects on atmosphere) ozone and regional- global climate? Weather (effects on air quality) 2 NASA Operating Missions Denotes International Collaboration LDCM NPP 3 Operating Satellite Status Current Life Mission Launch Phase Design Life (yr) (yr) Expected End Terra 18-Dec-99 Extended 5 13.3 2017 ACRIMSat 20-Dec-99 Extended 5 13.3 2020 Aqua 03-May-02 Extended 5 11.0 2022 SORCE 25-Jan-03 Extended 5 10.2 2015 Aura 15-Jul-04 Extended 5 8.8 2018 Cloudsat 28-Apr-06 Extended 3 7.0 2015 CALIPSO 28-Apr-06 Extended 3 7.0 2016 OCO - 1 24-Feb-09 Launch Failure 2 N/A N/A Glory 04-Mar-11 Launch Failure 3 N/A N/A Suomi-NPP 25-Oct-11 Prime till Oct 2016 5 1.4 not enough data 4 Operating Instrument Status INSTRUMENT INSTRUMENT MISSION STATUS Spectral Irradiance Monitor SIM SORCE Operating in
    [Show full text]
  • The Earth Observing System Microwave Limb Sounder (EOS MLS) on the Aura Satellite Joe W
    IEEE TRANSACTIONS ON GEOSCIENCE AND REMOTE SENSING, VOL. 44, NO. 5, MAY 2006 1075 The Earth Observing System Microwave Limb Sounder (EOS MLS) on the Aura Satellite Joe W. Waters, Lucien Froidevaux, Robert S. Harwood, Robert F. Jarnot, Herbert M. Pickett, William G. Read, Peter H. Siegel, Richard E. Cofield, Mark J. Filipiak, Dennis A. Flower, James R. Holden, Gary K. Lau, Nathaniel J. Livesey, Gloria L. Manney, Hugh C. Pumphrey, Michelle L. Santee, Dong L. Wu, David T. Cuddy, Richard R. Lay, Mario S. Loo, Vincent S. Perun, Michael J. Schwartz, Paul C. Stek, Robert P. Thurstans, Mark A. Boyles, Kumar M. Chandra, Marco C. Chavez, Gun-Shing Chen, Bharat V. Chudasama, Randy Dodge, Ryan A. Fuller, Michael A. Girard, Jonathan H. Jiang, Yibo Jiang, Brian W. Knosp, Remi C. LaBelle, Jonathan C. Lam, Karen A. Lee, Dominick Miller, John E. Oswald, Navnit C. Patel, David M. Pukala, Ofelia Quintero, David M. Scaff, W. Van Snyder, Michael C. Tope, Paul A. Wagner, and Marc J. Walch Abstract—The Earth Observing System Microwave Limb and mesosphere. It is an advanced follow-on to the first MLS Sounder measures several atmospheric chemical species (OH, [2], [3] on the Upper Atmosphere Research Satellite (UARS) HOP,HPO, OQ, HCl, ClO, HOCl, BrO, HNOQ,NPO, CO, HCN, launched September 12, 1991. The major objective of UARS CHQCN, volcanic SOP), cloud ice, temperature, and geopotential height to improve our understanding of stratospheric ozone chem- MLS was, in response to the industrial chlorofluorocarbon istry, the interaction of composition and climate, and pollution in threat to the ozone layer [4], to provide global information the upper troposphere.
    [Show full text]
  • 9 Catalogue of Satellite Instruments A
    9 Catalogue of Satellite Instruments A InstruMent & agency Missions Status Type MeasureMents & Technical characteristics (& any partners) applications AATSR Envisat Operational Imaging Measurements of sea surface Waveband: VIS–NIR: 0.555 µm, 0.659 µm, Advanced Along -Track multi -spectral temperature, land surface 0.86 5µm Scanning Radiometer radiometers temperature, cloud top SWIR: 1.6 µm (vis/IR) & Multiple temperature, cloud cover, MWIR: 3.7 µm BNSC direction/polarisation aerosols, vegetation, TIR: 10.85 µm, 12 µm radiometers atmospheric water vapour and Spatial resolution: IR ocean channels: 1 km x1km liquid water content. Visible land channels: 1 km x1km Swath width: 500 km Accuracy: Sea surface temperature: <0.5K over 0.5º x 0.5º (lat/long) area with 80% cloud cover Land surface temperature: 0.1K (relative) ABI GOES -R Being Imaging Detects clouds, cloud properties, Waveband: 16 bands in vis, NIR and IR Advanced Baseline GOES -S developed multi -spectral water vapour, land and sea ranging from 0.47 µm to 13.3 µm Imager radiometers (vis/IR) surface temperatures, dust, Spatial resolution: 0.5 km in 0.64 µm band aerosols, volcanic ash, fires, total 2.0 km in long wave IR and NOAA ozone, snow and ice cover, in the 1.378 µm band vegetation index. 1.0 km in all others Swath width: Accuracy: Varies by product ACC Swarm Being Precision orbit and Measurement of the spacecraft Waveband: N/A Accelerometer developed space environment non -gravitational accelerations, Spatial resolution: 0. 1 n m/s 2 linear accelerations range: Swath width:
    [Show full text]
  • Aura Key Aura Facts Joint with the Netherlands, Finland, and the U.K
    Aura Key Aura Facts Joint with the Netherlands, Finland, and the U.K. Orbit: Type: Polar, sun–synchronous Equatorial Crossing: 1:45 p.m. Altitude: 705 km Inclination: 98.2º Period: 100 minutes Aura URL Repeat Cycle: 16 days eos–aura.gsfc.nasa.gov/ Dimensions: 4.70 m × 17.37 m × 6.91 m Mass: 2967 kg (1200 kg of which are in instruments) Summary Power: Solar array provides 4800 W. Nickel– Aura’s four instruments study the atmosphere’s chemistry hydrogen battery for nighttime operations. and dynamics. Aura’s measurements enable us to inves- Downlink: X–band for science data; S–band for tigate questions about ozone trends, air–quality changes command and telemetry via Tracking and Data and their linkage to climate change. Aura’s measurements Relay Satellite System (TDRSS) and Deep Space also provide accurate data for predictive models and useful Network to polar ground stations in Alaska and information for local and national agency decision–sup- Norway. port systems. Design Life: Nominal mission lifetime of 5 years, with a goal of 6 years of operation. Instruments Contributor: Northrop Grumman Space Technology • High Resolution Dynamics Limb Sounder (HIRDLS) • Microwave Limb Sounder (MLS) • Ozone Monitoring Instrument (OMI) Launch • Tropospheric Emission Spectrometer (TES) • Date and Location: July 15, 2004, from Vandenberg Air Force Base, California Points of Contact • Vehicle: Delta II 7920 rocket • Aura Project Scientist: Mark Schoeberl, NASA Goddard Space Flight Center Relevant Science Focus Areas (see NASA’s Earth Science Program section)
    [Show full text]