List of Satellite Missions
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Correlation of the SAGE III on ISS Thermal Models in Thermal Desktop
47th International Conference on Environmental Systems ICES-2017-171 16-20 July 2017, Charleston, South Carolina Correlation of the SAGE III on ISS Thermal Models in Thermal Desktop Ruth M. Amundsen1, Warren T. Davis2, and Kaitlin A. K. Liles3 NASA Langley Research Center, Hampton, VA, 23681 and Shawn C. McLeod4 Analytical Mechanics Associates, Inc., Hampton, VA, 23666 The Stratospheric Aerosol and Gas Experiment III (SAGE III) instrument is the fifth in a series of instruments developed for monitoring aerosols and gaseous constituents in the stratosphere and troposphere. SAGE III was launched on February 19, 2017 and mounted to the International Space Station (ISS) to begin its three-year mission. A detailed thermal model of the SAGE III payload, which consists of multiple subsystems, has been developed in Thermal Desktop (TD). Correlation of the thermal model is important since the payload will be expected to survive a three-year mission on ISS under varying thermal environments. Three major thermal vacuum (TVAC) tests were completed during the development of the SAGE III Instrument Payload (IP); two subsystem-level tests and a payload-level test. Additionally, a characterization TVAC test was performed in order to verify performance of a system of heater plates that was designed to allow the IP to achieve the required temperatures during payload-level testing; model correlation was performed for this test configuration as well as those including the SAGE III flight hardware. This document presents the methods that were used to correlate the SAGE III models to TVAC at the subsystem and IP level, including the approach for modeling the parts of the payload in the thermal chamber, generating pre-test predictions, and making adjustments to the model to align predictions with temperatures observed during testing. -
Indian Payload Capabilities for Space Missions
INDIAN PAYLOAD CAPABILITIES FOR 13, Bangalore - SPACE MISSIONS July 11 A.S. Kiran Kumar Director Space Applications Centre International ASTROD Symposium, Ahmedabad th 5 Application-specific EO payloads IMS-1(2008) RISAT-1 (2012) MX/ HySI-T C-band SAR CARTOSAT-2/2A/2B RESOURCESAT-2 (2011) (2007/2009/2010) LISS 3/ LISS 4/AWiFS PAN RESOURCESAT-1 (2003) LISS 3/ LISS 4 AWiFS CARTOSAT-1 (2005) (Operational) STEREOPAN Megha-Tropiques (2011) TES(2001) MADRAS/SAPHIR/ScARaB/ Step& Stare ROSA PAN OCEANSAT-2 (2009) OCM/ SCAT/ROSA YOUTHSAT(2011) LiV HySI/RaBIT INSAT-3A (2003) KALPANA-1 (2002) VHRR, CCD VHRR Application-specific EO payloads GISAT MXVNIR/SWIR/TIR/HySI RISAT-3 RESOURCESAT-3A/3B/3C L-band SAR CARTOSAT-3 RESOURCESAT-2A LISS 3/LISS 4/AWiFS PAN LISS3/LISS4/AWiFS RESOURCESAT-3 LISS 3/LISS 4/ CARTOSAT-2C/2D AWiFS (Planned) PAN RISAT-1R C-band SAR SARAL Altimeter/ARGOS OCEANSAT-3 OCM , TIR GISAT MXVNIR/SWIR/ INSAT- 3D TIR/HySI Imager/Sounder EARTH OBSERVATION (LAND AND WATER) RESOURCESAT-1 IMS-1 RESOURCESAT-2 RISAT-1 RESOURCESAT-2A RESOURCESAT-3 RESOURCESAT-3A/3B/3C RISAT-3 GISAT RISAT-1R EARTH OBSERVATION (CARTOGRAPHY) TES CARTOSAT-1 CARTOSAT-2/2A/2B RISAT-1 CARTOSAT-2C/2D CARTOSAT-3 RISAT-3 RISAT-1R EARTH OBSERVATION (ATMOSPHERE & OCEAN) KALPANA-1 INSAT- 3A OCEANSAT-1 INSAT-3D OCEANSAT-2 YOUTHSAT GISAT MEGHA–TROPIQUES OCEANSAT-3 SARAL Current observation capabilities : Optical Payload Sensors in Spatial Res. Swath/ Radiometry Spectral bands Repetivity/ operation Coverage (km) revisit CCD 1 1 Km India & 10 bits 3 (B3, B4, B5) 4 times/ day surround. -
Landsat 9 Micrometeoroid and Orbital Debris Mission Success Approach
First Int'l. Orbital Debris Conf. 2019 (LPI Contrib. No. 2109) 6058.pdf Landsat 9 Micrometeoroid and Orbital Debris Mission Success Approach Michael S. Pryzby(1), Scott M. Hull(2), Angela M. Russo(2), Glenn T. Iona(2), Daniel Helfrich(2), and Evan H. Webb(2) (1) ATA Aerospace, 7474 Greenway Center Dr, Suite 500, Greenbelt, MD 20770, USA (2) NASA Goddard Space Flight Center, 8800 Greenbelt Rd, Greenbelt, MD 20771, USA ABSTRACT Landsat 9* (L9) is the successor mission to Landsat 8 (L8) previously known as Landsat Data Continuity Mission (LDCM). Both missions are large unmanned remote sensing satellites operating in sun- synchronous polar orbits. As opposed to L8/LDCM, systems engineers for L9 incorporated Micrometeoroid/Orbital Debris (MMOD) protection for small object collisions as part of the L9’s mission success criteria. In other words, the NASA Process for Limiting Orbital Debris (NASA-STD-8719.14A) only calls for analyses of the protection of disposal-critical hardware, but L9 opted to also assess and provide small particle penetration protections for all observatory components including instruments that are not part of the spacecraft components needed for controlled reentry. Systems engineers at Goddard developed a design process to protect against MMOD during the life of Low Earth Orbit (LEO) observatories, and in particular the Landsat 9 Mission. Simply stated, this design process enhanced the effectiveness of existing Multi-Layer Insulation (MLI) to provide the needed protection. The end goal of the design process was to establish a necessary blanket areal density for a given electronics box or instrument wall thickness and a separation between the outer MLI blanket and the structure underneath. -
Drafting Committee for the 'Asia‐Pacific
Drafting Committee for the ‘Asia‐Pacific Plan of Action for Space Applications for Sustainable Development (2018‐2030) Dr Rajeev Jaiswal EOS Programme Office Indian Space Research Organisation (ISRO) India Bangkok, Thailand 31 May ‐ 1 June 2018 India’s Current Space Assets Communication Satellites • 15 Operational (INSAT- 4A, 4B, 4CR and GSAT- 6, 7, 8, 9 (SAS), 10, 12, 14, 15, 16, 17, 18 & 19) • >300 Transponders in C, Ext C & Ku bands Remote sensing Satellites • Three in Geostationary orbit (Kalpana-1, INSAT 3D & 3DR) • 14 in Sun-synchronous orbit (RESOURCESAT- 2 & 2A; CARTOSAT-1/ 2 Series (5); RISAT-2; OCEANSAT 2; MEGHA-TROPIQUES; SARAL, SCATSAT-1) Navigation Satellites : 7 (IRNSS 1A - IG) & GAGAN Payloads in GSAT 8, 10 & 15 Space Science: MOM & ASTROSAT 1 Space Applications Mechanism in India Promoting Space Technology Applications & Tools For Governance and Development NATIONAL MEET “There should not be any space between common man and space technology” . 160 Projects across 58 Ministries . Web & Mobile Applications : 200+ . MoUs with stakeholders : 120+ . Capacity Building : 10,000+ . Space Technology Cells : 21 17 STATE MEETS Haryana, Bihar, Uttarakhand, Mizoram, Nagaland, Rajasthan, Punjab, Jharkhand, Meghalaya, Himachal 20 58 Pradesh, Kerala, Chhattisgarh, Assam, Madhya Ministries Ministries Pradesh, Tamil Nadu, Mizoram & Uttar Pradesh Space Applications Verticals SOCIO ECONOMIC SECURITY SUSTAINABLE DEVELOPMENT Food Impact Assessment Water Bio- Resources Conservation Energy Fragile & Coastal Ecosystem Health Climate Change Induced -
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. -
25 Years of Indian Remote Sensing Satellite (IRS)
2525 YearsYears ofof IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) SeriesSeries Vinay K Dadhwal Director National Remote Sensing Centre (NRSC), ISRO Hyderabad, INDIA 50 th Session of Scientific & Technical Subcommittee of COPUOS, 11-22 Feb., 2013, Vienna The Beginning • 1962 : Indian National Committee on Space Research (INCOSPAR), at PRL, Ahmedabad • 1963 : First Sounding Rocket launch from Thumba (Nov 21, 1963) • 1967 : Experimental Satellite Communication Earth Station (ESCES) established at Ahmedabad • 1969 : Indian Space Research Organisation (ISRO) established (15 August) PrePre IRSIRS --1A1A SatellitesSatellites • ARYABHATTA, first Indian satellite launched in April 1975 • Ten satellites before IRS-1A (7 for EO; 2 Met) • 5 Procured & 5 SLV / ASLV launch SAMIR : 3 band MW Radiometer SROSS : Stretched Rohini Series Satellite IndianIndian RemoteRemote SensingSensing SatelliteSatellite (IRS)(IRS) –– 1A1A • First Operational EO Application satellite, built in India, launch USSR • Carried 4-band multispectral camera (3 nos), 72m & 36m resolution Satellite Launch: March 17, 1988 Baikanur Cosmodrome Kazakhstan SinceSince IRSIRS --1A1A • Established of operational EO activities for – EO data acquisition, processing & archival – Applications & institutionalization – Public services in resource & disaster management – PSLV Launch Program to support EO missions – International partnership, cooperation & global data sets EarlyEarly IRSIRS MultispectralMultispectral SensorsSensors • 1st Generation : IRS-1A, IRS-1B • -
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. -
Bob Cabana, Director Kennedy Space Center National Aeronautics and Space Administration
Bob Cabana, Director Kennedy Space Center National Aeronautics and Space Administration Premier Multi-User Spaceport KSC Programs and Projects Commercial Crew Program Launch Services Program Exploration Ground Systems Gateway — A spaceport for human and Exploration Research & Technology robotic exploration to the Moon and beyond Programs 2019 KSC Key Milestones o March 2 SpaceX Demo-1 LC 39A o June 27 Mobile Launcher rolls testing to SLC 39B o July 2 Orion Launch Abort System Test SLC-46 o October 10 ICON Mission CCAFS Remaining Milestones Planned in 2019 Boeing Pad Abort Test – Target date 11/4/19 Boeing Orbital Flight Test – Target date mid December SpaceX In-Flight Abort Test – Target date early December Gateway Logistics Contract Award 2020 KSC Key Milestones Orion Mass Simulator on dock KSC - 1/24/20 SpaceX Demo-2 Boeing Crewed Flight Test Solar Orbiter – 2/5/20 SLS Boosters arrive and processing begins - 3/18/20 Orion turnover to EGS - 5/16/20 MARS 2020 -7/17/20 Sentinel 6A - 11/15/20 Landsat-9 – 12/15/20 7 National Aeronautics and Space Administration SpaceX Demo-1 March 2, 2019 Boeing Hotfire & Parachute Tests May 22, 2019 National Aeronautics and Space Administration High Performance Spaceflight Computing Precision Solar Landing Electric Space Technology for Propulsion 2024 and Beyond Surface Cryofluid Lunar Dust Excavation/Construction Management Mitigation In Situ Resource Extreme Environments Utilization Extreme Access Lunar Surface Power Lunar Surface Innovation Initiative NASA Internal Use Only Do Not Distribute 18 EGS Striving Toward Launch of Artemis I SLS Block 1 National Aeronautics and Space Administration Orion Liquid oxygen Artemis I Intertank Core Stage 322 feet 322 Booster Mobile Launcher 130 feet 130 Rocket Crew Access Arm 274 feet 274 feet 380 Engine NASA Internal Use Only Do Not Distribute Vehicle Assembly Building 380 feet • 10.5 million lbs. -
10Th International Limb Workshop – Scientific Program Greifswald, June 3 – 7, 2019
10th International Limb Workshop – Scientific program Greifswald, June 3 – 7, 2019 Monday, June 3, 18:00: Icebreaker and Reception Restaurant Campo Alegre (Lange Reihe 1) Session 1: Tuesday, June 4, 08:30 – 10:30 (Chair: Christian von Savigny) Welcome 08:30 – 08:35 Welcome by local organizers (Christian von Savigny) 08:35 – 08:45 Welcome address by representative of the City of Greifswald (Jeanette von Busse) 08:45 – 08:55 Welcome address by University administration (Pro-rector Prof. Katharina Riedel) 08:55 – 09:05 Welcome address by Dr. Christian Suhm (Academic coordinator of Alfried Krupp Institute of Advanced Study) 09:05 – 09:15 Logistics (Christian von Savigny) New missions and mission concepts 09:15 – 09:45 Didier Fussen Forthcoming limb observations with ALTIUS (invited talk) 09:45 – 10:00 Nick Lloyd The Canadian Atmospheric Tomography System (CATS) – The Next Generation OSIRIS Instrument 10:00 – 10:15 Marilee Roell Stratospheric Aerosol and Gas Experiment (SAGE) III installed on the International Space Station (ISS): Mission overview and Science Data Product Validation 10:15 – 10:30 Matthew DeLand MASTAR: Limb Scattering Measurements of Stratospheric Aerosols 10:30 – 11:00 Coffee break 10th International Limb Workshop, June 4 – 7, 2019 Greifswald Session 2: Tuesday, June 4, 11:00 – 13:00 (Chair: Adam Bourassa) New missions and mission concepts 11:00 – 11:25 Christoph R. Englert MIGHTI (Michelson Interferometer for Global High-resolution Thermospheric Imaging): The Wind and Temperature Instrument Onboard the NASA Ionospheric Connection (ICON) Mission (invited talk) 11:25 – 11:50 Donal Murtagh MATS - a micro satellite for studies of Mesospheric Airglow /aerosol by Tomography and Spectroscopy (invited talk) 11:50 – 12:15 Kristell Pérot SIW: a New Satellite Mission to Explore Middle Atmospheric Wind Structure and Composition (invited talk) 12:15 – 12:30 John Burrows A new Concept SLIPSTREAM/SCIA-L2 12:30 – 12:45 William E. -
Spectral Response Characterization of the Landsat 9 Operational Land Imager 2 Using the Goddard Laser for Absolute Measurement of Radiance (GLAMR)
Spectral Response Characterization of the Landsat 9 Operational Land Imager 2 using the Goddard Laser for Absolute Measurement of Radiance (GLAMR) Brian Markham, Julia Barsi, Joel McCorkel, Brendan McAndrew, Jeffrey Pedelty, + GLAMR and Ball I & T and Systems teams NASA Goddard Space Flight Center Mission Objectives Mission Parameters • Provide continuity in multi-decadal Landsat land surface observations to • Single Satellite, Mission Category 1, Risk Class B study, predict, and understand the consequences of land surface dynamics • 5-year design life after on-orbit checkout • Core Component of Sustainable Land Imaging program • At least 10 years of consumables • Sun-synchronous orbit, 705 km at equator, 98°inclination • 16-day global land revisit • Partnership: NASA & USGS Mission Team • NASA: Flight segment & checkout • NASA Goddard Space Flight Center (GSFC) • USGS: Ground system and operations • USGS Earth Resources Observation & Science (EROS) Center • Category 3 Launch Vehicle • NASA Kennedy Space Center (KSC) • Launch: Management Agreement - December 2020 Agency Baseline Commitment – November 2021 Instruments • Operational Land Imager 2 (OLI-2; Ball Aerospace) • Reflective-band push-broom imager (15-30m res) • 9 spectral bands at 15 - 30m resolution • Retrieves data on surface properties, land cover, and vegetation condition • Thermal Infrared Sensor 2 (TIRS-2; NASA GSFC) • Thermal infrared (TIR) push-broom imager • 2 TIR bands at 100m resolution • Retrieves surface temperature, supporting agricultural and climate applications, including monitoring evapotranspiration Spacecraft (S/C) & Observatory Integration & Test (I&T) • Northrop Grumman Innovation Systems (NGIS), formerly Orbital ATK (OA) Launch Services • United Launch Alliance (ULA) Atlas V 401 Increase in pivot irrigation in Saudi Arabia from 1987 to 2012 as recorded by Landsat. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 1 January–April 2019 CONTENTS SPACE POLICY AND PROGRAMMES .................................................................................... 1 Focus .................................................................................................................... 1 Europe ................................................................................................................... 4 11TH European Space Policy Conference ......................................................................... 4 EU programmatic roadmap: towards a comprehensive Regulation of the European Space Programme 4 EDA GOVSATCOM GSC demo project ............................................................................. 5 Programme Advancements: Copernicus, Galileo, ExoMars ................................................... 5 European Space Agency: partnerships continue to flourish................................................... 6 Renewed support for European space SMEs and training ..................................................... 7 UK Space Agency leverages COMPASS project for international cooperation .............................. 7 France multiplies international cooperation .................................................................... 7 Italy’s PRISMA pride ................................................................................................ 8 Establishment of the Portuguese Space Agency: Data is King ................................................ 8 Belgium and Luxembourg -
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.