Vicky Chu, Jer Ling, Tom Lin, Joe Fong, Feng-Tai Huang, Guey-Shin Chang. April 15, 2011
|
|
- Leonard Curtis
- 5 years ago
- Views:
Transcription
1 FORMOSAT-7/COSMIC-2 Overview Vicky Chu, Jer Ling, Tom Lin, Joe Fong, Feng-Tai Huang, Guey-Shin Chang April 15, 2011
2 Program Status AIT-TECRO Agreement on FORMOSAT-7/COSMIC-2 joint program has been signed in May, Joint Program Mission Design Review has been completed in August, Joint Program System Requirement Review has been completed in April 2011.
3 Joint Mission Between NSPO and NOAA Both NSPO NOAA
4 Users Requirements
5 Data Types and Data Products Data Products Neutral Atmosphere (1 km~ 60 km) Ionosphere and Space Weather (90 km ~700 km) Bending angle profile Refractivity profile Temperature profile Water vapor profile Total Electron Content Electron density profile Scintillation amplitude index Scintillation phase index Metadata GNSS and LEO satellite orbit location files Excess phase files Occultation tables Records of major processing algorithm revisions
6 Data Requirements for Neutral Atmosphere Product Item Threshold Objective Number of Profiles per day Corresponding avg. #/location/day Average Latency [minutes] 45 [TBR] 15 Average Revisit Time [hours] 6 4.8
7 Spatial and Temporal Resolution Spatial resolution Horizontal: Near-uniform global data coverage (data density at any location on the Earth s surface varies by less than a factor of 2 relative to any other location) Vertical: 0.1 km at altitudes < 25 km; 1 km at altitudes km Temporal resolution Full diurnal sampling (the local time gaps are less than 5 hours at any latitude in any given day)
8 Quality Control Neutral Atmosphere Threshold Objective 70% 90% Ionosphere 75% 90% Region Refractivity and Bending Angle Outside 30 Latitude Within 30 Latitude Outside 30 Latitude Within 30 Latitude 85% 65% 90% 70%
9 Key Requirements (1/2) Data Profiles per day (FORMOSAT-3 Reference: points per day) Data Latency 45 minutes [TBR] (FORMOSAT-3 Reference: 86 % of data is within 3-hr latency) Data Distribution Geophysical homogeneously distributed Full diurnal sampling (FORMOSAT-3 Reference: Geophysical homogeneously distributed)
10 Key Requirements (2/2) System Operational Availability 95% [TBR] Mission duration 5 years beyond 2nd launch [TBD] (FORMOSAT-3 Reference: 2 years) Satellites life (1st launch) Satellites life (2nd launch) Mission Duration
11 Mission Requirements
12 Mission Baseline FORMOSAT-7 First Launch Second Launch Mission Objectives To be achieved after Full Operational Capability: 8,000 atmospheric sounding profiles per day 45-min data latency [TBR] Constellation GNSS RO Payload Scientific Payload 6 SC to low-inclinationangle orbit (mission altitude ~520 km) TriG Velocity, Ion Density and Irregularities Instrument RF Beacon Instrument (5+1) or (6+1) SC to highinclination-angle orbit (mission altitude ~800 km) 7 satellites to be allocated for mission design purpose TriG To be determined Launch Vehicle Minotaur IV or Falcon 9 Minotaur IV or Falcon 9 Launch Schedule (as a goal) Communication Architecture 2015 Q3-Q Q3-Q4 Via ground station
13 System Architecture GALILEO or GLONASS-FDMA GPS High-inc Low-inc Spare S/C FORMOSAT-7/ COSMIC-2 TT&C stations (overseas) TT&C stations (Taiwan) US DPC Satellite Operations and Control Center Minotaur IV or Falcon 9 Users Users Fiducial Network Taiwan DPC Researchers Researchers
14 Mission Constellation 1st Launch 2nd Launch Inclination Angle 24 deg 72 deg Parking Orbit 720 km 550 km Mission Orbit 520 km 800 km Orbital Plane Separation at Equator 60 deg 30 deg
15 Constellation Deployment Unit:Km st Launch 2nd Launch Unit:Week Launch Parking Orbit Early Orbit Checkout Mission Payload Starts to Collect Data Adjust the Argument of Latitude Mission Constellation Constellation Deployment Maneuver Orbit Maintenance
16 Occultations FORMOSAT-3 Occultations 3 Hrs Coverage FORMOSAT-3 FORMOSAT-7 Occultations 3 Hrs Coverage FORMOSAT-7
17 Spacecraft Bus Requirements
18 Spacecraft Bus, Satellite, and Multi- Satellites-Suite Science Payloads Mission Payload Spacecraft Bus Satellite
19 Spacecraft Bus Key Requirements Key Parameter Spacecraft Bus Reliability Power Margin 10% Operations Attitude Attitude Control Accuracy Attitude Determination Knowledge Ground Communication Downlink Telemetry Data Rate Uplink Command Data Rate Spacecraft Bus Data Storage Payload Data Storage Requirements 0.66 for 5 years after launch Local Vertical Local Horizontal better than 1 deg [TBR], 3 σ, all axes better than 0.05 deg [TBR], 3 σ, all axes S band uplink/downlink 2 Mbps 32 Kbps 256 Mbits [TBR] 2 Gbits [TBR]
20 Conceptual Configuration TriG POD antenna TT&C S-Band antenna VIDI Sensors (may have alternative orientation) TriG OCC antenna (canted or not) Pitch (Y) Roll (X) Ram (Flight direction) RF Beacon antenna Yaw (Z) Nadir TT&C S-Band antenna
21 Next Step and Acknowledgement Next Steps To firm up segment and interface requirements To implement the corresponding segments Acknowledgements NOAA (National Oceanic and Atmospheric Administration) UCAR (University Corporation for Atmospheric Research) US Air Force JPL (Jet Propulsion Laboratory) Aerospace Corporation NSC (National Science Council) NARL (National Applied Research Laboratory) CWB (Central Weather Bureau) TTFRI (Taiwan Typhoon and Flood Research Institute) Taiwan Science Community
22 Thanks!
SSC13-VI-1 MISSION DESIGN CONCEPT
SSC13-VI-1 INTRODUCTION TO FORMOSAT-7/COSMIC-2 MISSION Alex da Silva Curiel, Meryl Lambert, Doug Liddle, Prof Sir Martin Sweeting. Surrey Satellite Technology Ltd. Tycho House, Surrey Research Park, ;
More informationSpace Programs in Taiwan
SpacePart12-4th International Conference on Particle and Fundamental Physics in Space Space Programs in Taiwan FORMOSAT 5 and FORMOSAT 7 Lou-Chuang Lee / Academia Sinica November 2012 1 Organization &
More informationFuture Low Earth Observation Satellite - Radio Occultation Mission
Future Low Earth Observation Satellite - Radio Occultation Nick L. Yen / Chen-Joe Fong National Space Organization (NSPO) F8, No. 9, Prosperity 1 st Rd. Hsinchu, Taiwan 30078, R.O.C. +886-3-578-4208x1053
More informationNOAA Satellite & Information Service (NESDIS)
Transition from Research to Operation for GNSS Radio Occultation Abigail D. Harper National Environmental Satellite, Data, and Information Service (NESDIS) Deputy Assistant Administrator, Systems April
More informationROCSAT-3 Constellation Mission
ROCSAT-3 Constellation Mission, An-Ming Wu, Paul Chen National Space Program Office 8F, 9 Prosperity 1st Road, Science Based Industrial Park, Hsin-Chu, Taiwan vicky@nspo.org.tw, amwu@nspo.org.tw, paulchen@nspo.org.tw
More informationApproaching the First Global Radio Occultation Operational Mission Using Constellation LEO Satellites
Approaching the First Global Radio Occultation Operational Using Constellation LEO Satellites Nick L. Yen, Chen-Joe Fong, G.-S. Chang National Space Organization (NSPO) F8, No. 9, Prosperity 1 st Rd. Hsinchu,
More informationVELOX-CI: Advanced Application of GPS for Radio Occultation and Satellite Attitude Determination
VELOX-CI: Advanced Application of GPS for Radio Occultation and Satellite Attitude Determination Yung-Fu Tsai, Guo Xiong Lee and Kay Soon Low Satellite Research Centre (SaRC) School of Electrical and Electronic
More informationWe have processed RO data for climate research and for validation of weather data since 1995 as illustrated in Figure 1.
Real-time Analysis of COSMIC Data Christian Rocken, Doug Hunt, Bill Schreiner University Corporation for Atmospheric Research (UCAR) COSMIC Project Office Boulder, CO Abstract UCAR has analyzed GPS radio
More informationInteracciones en la Red Iberica
2a Reunion Red Iberica MM5 Grupo 12: interacciones, modelo mm5 y proyectos actuales Lidia Cucurull UCAR - NOAA/NCEP Washington DC, USA http://www.cosmic.ucar.edu Lidia.Cucurull@noaa.gov cucurull@ucar.edu
More informationEUMETSAT's possible contributions to the future radio occultation constellation. COSMIC Workshop 2009 Boulder, USA
EUMETSAT's possible contributions to the future radio occultation constellation A. von Engeln, C. Marquardt, C. Accadia Introduction: Radio Occultation Instruments 97 98 99 00 01 02 03 03 04 05 06 07 08
More informationFORMOSAT-3 Satellite Thermal Control Design and Analysis *
Journal of Aeronautics, Astronautics and Aviation, Series A, Vol.39, No.4, pp.287-292 (27) 287 Technical Note FORMOSAT-3 Satellite Thermal Control Design and Analysis * Ming-Shong Chang **, Chia-Ray Chen,
More informationRadio occultation mission to Mars using cubesats
Radio occultation mission to Mars using cubesats LCPM-12 2017 W. Williamson, A.J. Mannucci, C. Ao 2017 California Institute of Technology. Government sponsorship acknowledged. 1 Radio Occultation Overview
More informationDARE Mission and Spacecraft Overview
DARE Mission and Spacecraft Overview October 6, 2010 Lisa Hardaway, PhD Mike Weiss, Scott Mitchell, Susan Borutzki, John Iacometti, Grant Helling The information contained herein is the private property
More information483 Lecture. Space Mission Requirements. February11, Definition Examples Dos/ Don ts Traceability
483 Lecture Space Mission February11, 2012 Photo Credit:: http://www.spacewallpapers.info/cool-space-wallpaper What s a Requirement? ification? Requirement A concept independent statement of a mix of needs,
More informationCOSMIC-2: Next Generation Atmospheric Remote Sensing System using Radio Occultation Technique
COSMIC-2: Next Generation Atmospheric Remote Sensing System using Radio Occultation Technique Bill Kuo, Bill Schreiner, Doug Hunt, Sergey Sokolovskiy UCAR COSMIC Program Office www.cosmic.ucar.edu GPS
More informationOrbit Design Marcelo Suárez. 6th Science Meeting; Seattle, WA, USA July 2010
Orbit Design Marcelo Suárez Orbit Design Requirements The following Science Requirements provided drivers for Orbit Design: Global Coverage: the entire extent (100%) of the ice-free ocean surface to at
More informationObserving System Simulation Experiments (OSSEs) with Radio Occultation observations
Observing System Simulation Experiments (OSSEs) with Radio Occultation observations Lidia Cucurull Deputy Director, NOAA Quantitative Observing System Assessment Program (QOSAP) NOAA OAR Principal Investigator
More informationSimulation Results of Alternative Methods for Formation Separation Control
Simulation Results of Alternative Methods for Formation Separation Control Thomas Heine, Charles Bussy-Virat, Mark Moldwin, Aaron Ridley Department of Climate and Space Sciences and Engineering University
More informationLADEE PDS Mission Description
Lunar Atmosphere and Dust Environment Explorer (LADEE) LADEE PDS Mission Description May 13 th, 2014 National Aeronautics and Space Administration Ames Research Center Moffett Field, California i This
More informationSpace Frequency Coordination Group
Space Coordination Group THE SFCG Recommendation SFCG 32-2R1 COMMUNICATION FREQUENCY ALLOCATIONS AND SHARING IN THE LUNAR REGION CONSIDERING a. that a regional communication network at the Moon can be
More informationA Regional Microsatellite Constellation with Electric Propulsion In Support of Tuscan Agriculture
Berlin, 20 th - 24 th 2015 University of Pisa 10 th IAA Symposium on Small Satellites for Earth Observation Student Conference A Regional Microsatellite Constellation with Electric Propulsion In Support
More informationSub-millimeter size debris monitoring system with IDEA OSG 1
Sub-millimeter size debris monitoring system with IDEA OSG 1 Masahiko Uetsuhara, Mitsunobu Okada, Yasunori Yamazaki, Astroscale Pte. Ltd. Toshiya Hanada Kyushu University ABSTRACT The 20-kg class microsatellite
More informationRadio Occultation Data Processing at the COSMIC Data Analysis and Archival Center (CDAAC)
Radio Occultation Data Processing at the COSMIC Data Analysis and Archival Center (CDAAC) Bill Schreiner, Doug Hunt, Chris Rocken, Sergey Sokolovskiy University Corporation for Atmospheric Research (UCAR),
More informationAPPENDIX 2 OVERVIEW OF THE GLOBAL PRECIPITATION MEASUREMENT (GPM) AND THE TROPICAL RAINFALL MEASURING MISSION (TRMM) 2-1
APPENDIX 2 OVERVIEW OF THE GLOBAL PRECIPITATION MEASUREMENT (GPM) AND THE TROPICAL RAINFALL MEASURING MISSION (TRMM) 2-1 1. Introduction Precipitation is one of most important environmental parameters.
More informationScience planning and operations for Mars Express
Science planning and operations for Mars Express René Pischel and Tanja Zegers ESA/ESTEC, Research and Scientific Support Department, Postbus 299, 2200 AG Noordwijk, The Netherlands I. Introduction The
More informationThe NASA EV-2 Cyclone Global Navigation Satellite System (CYGNSS) Mission
International Ocean Vector Wind Science Team Meeting Kailua-Kona, Hawaii USA 6-8 May 2013 The NASA EV-2 Cyclone Global Navigation Satellite System (CYGNSS) Mission Chris Ruf (1) (CYGNSS Principal Investigator),
More informationPrecise Orbit Determination and Radio Occultation Retrieval Processing at the UCAR CDAAC: Overview and Results
Precise Orbit Determination and Radio Occultation Retrieval Processing at the UCAR CDAAC: Overview and Results Bill Schreiner B. Kuo, C. Rocken, S. Sokolovskiy, D. Hunt, X. Yue, K. Hudnut, M. Sleziak,
More informationSatellite communications and the environment of space. V 1.1 Swiss Space Summer Camp 2016 Images: NASA 1
Satellite communications and the environment of space Swiss Space Summer Camp 2016 Images: NASA 1 Can you name these satellites? Sputnik The first man made satellite Launched in 1957 by The USSR Mass 84kg,
More informationesa ACE+ An Atmosphere and Climate Explorer based on GPS, GALILEO, and LEO-LEO Occultation Per Høeg (AIR/DMI) Gottfried Kirchengast (IGAM/UG)
ACE+ An Atmosphere and Climate Explorer based on GPS, GALILEO, and LEO-LEO Occultation Per Høeg (AIR/DMI) Gottfried Kirchengast (IGAM/UG) OPAC-1, September, 2002 1 Objectives Climate Monitoring global
More informationStatus report on the current and future meteorological satellite systems by CMA
Status report on the current and future meteorological satellite systems by CMA Presented to CGMS-44Plenary session, agenda item [D.1] Overview - Planning of China satellite systems by year 2025 NSIP:
More informationGOES-R Instrument Status and Accommodations. Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference
GOES-R Instrument Status and Accommodations Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference Agenda Instrument Developmental Status Significant Changes in the Last Year Introducing
More informationCharacterizing Irregularities and Scintillation with GNSS Radio Occultations
Characterizing Irregularities and Scintillation with GNSS Radio Occultations K. Groves, C. Carrano, W. McNeil and C. Rino Boston College Institute for Scientific Research keith.groves@bc.edu R. Caton 1
More informationAssessing attitude error of FORMOSAT-3/COSMIC satellites and its impact on orbit determination
Available online at www.sciencedirect.com Advances in Space Research 49 (2012) 1301 1312 www.elsevier.com/locate/asr Assessing attitude error of FORMOSAT-3/COSMC satellites and its impact on orbit determination
More informationN E S D I S C D A A C. COSMIC Operations JCSDA TACC NCEP ECMWF CWB GTS UKMO
CDAAC Activities Bill Schreiner B. Kuo, C. Rocken, S. Sokolovskiy, D. Hunt, X. Yue, J. Zeng, K. Hudnut, M. Sleziak, T.-K. Wee, T. Vanhove, J. Lin UCAR / COSMIC Program Office - Boulder CO COSMIC IWG Meeting
More informationApplication of Radio Occultation Data in Analyses and Forecasts of Tropical Cyclones Using an Ensemble Assimilation System
Application of Radio Occultation Data in Analyses and Forecasts of Tropical Cyclones Using an Assimilation System Hui Liu, Jeff Anderson, and Bill Kuo NCAR Acknowledgment: C. Snyder, Y. Chen, T. Hoar,
More informationImpact of FORMOSAT 3/COSMIC Radio Occultation. near Taiwan
Impact of FORMOSAT 3/COSMIC Radio Occultation Data on Predictions i of Typhoon and Mei yu Fronts near Taiwan CHING YUANG HUANG 1,2, CHAN SENG WONG 1, CHIEN JU WANG 2, and CHIN CHENG TSAI 2 1 Department
More informationOverview of the Current Baseline of the Solar-C Spacecraft System
Overview of the Current Baseline of the Solar-C Spacecraft System Keisuke YOSHIHARA (JAXA) 11 November, 2013 Solar-C Science Meeting Hida Earth Wisdom Center, Takayama, Japan Solar-C Spacecraft System
More informationOTSUKIMI Moon-sighting Satellite Kyushu Institute of Technology. 3 rd Mission Idea Contest UNISEC Global
OTSUKIMI Moon-sighting Satellite Kyushu Institute of Technology 3 rd Mission Idea Contest UNISEC Global The Idea We want to take image for the moon phases as seen from Earth Why? Introduction 1.6 billion,23.4%
More informationUpdates on CMA FENGYUN Meteorological Satellite Programs
Updates on CMA FENGYUN Meteorological Satellite Programs Peng ZHANG National Satellite Meteorological Center, China Meteorological Administration (NSMC/CMA) 29 Nov. - 5 Dec. 2017, Darmstadt, Germany 1.
More informationThe 2007 CubeSat Developers' Workshop SwissCube Project
SwissCube Project (http://swisscube.epfl.ch) The 2007 CubeSat Developers' Workshop SwissCube Project Guillaume Roethlisberger Mechanical System Engineer Space Center EPFL guillaume.roethlisberger@epfl.ch
More informationCircular vs. Elliptical Orbits for Persistent Communications
5th Responsive Space Conference RS5-2007-2005 Circular vs. Elliptical Orbits for Persistent Communications James R. Wertz Microcosm, Inc. 5th Responsive Space Conference April 23 26, 2007 Los Angeles,
More informationUse of FY-3C/GNOS Data for Assessing the on-orbit Performance of Microwave Sounding Instruments
Use of FY-3C/GNOS Data for Assessing the on-orbit Performance of Microwave Sounding Instruments Xiuqing Hu 1 Xueyan Hou 2, and Mi Liao 1 1 National Satellite Meteorological Center (NSMC), CMA 2 Chinese
More informationSatellite Position Determination of LEO Spacecraft
Satellite Position Determination of LEO Spacecraft S.C.Rathnakara ISRO Satellite Centre 5 th September, 2007 International Committee on Global Navigation Satellite Systems(ICG) Things to follow Brief background
More informationNew Worlds Observer Operations Concept NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON)
NEW WORLDS OBSERVER OPERATIONS CONCEPT (OPSCON) 1 Table of Contents 1.0 Mission Overview... 1 1.1 NWO scope... 1 2.0 System Overview... 2 2.1 System constituents... 2 2.2 system functional architecture...
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Presentation Outline Mission Overview Mission Relevance
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Mission Overview Mission Relevance ConOps INCA Payload
More informationAeolus. A Mission to Map the Winds of Mars. Anthony Colaprete Amanda Cook NASA Ames Research Center
Aeolus A Mission to Map the Winds of Mars Anthony Colaprete Amanda Cook NASA Ames Research Center Low-Cost Planetary Missions Conference 12, 2017 What is Aeolus? Science Aeolus will provide the very first
More information- an Operational Radio Occultation System
- an Operational Radio Occultation System Frans Rubek, Georg Bergeton Larsen, Hans-Henrik Benzon, Kent Bækgaard Lauritsen, Martin Bjært Sørensen Danmarks Meteorologiske Institut (Denmark) Josep M. Aparicio,
More informationProton Launch System Mission Planner s Guide SECTION 2. LV Performance
Proton Launch System Mission Planner s Guide SECTION 2 LV Performance 2. LV PERFORMANCE 2.1 OVERVIEW This section provides the information needed to make preliminary performance estimates for the Proton
More informationGoal and context a new electron density extrapolation technique (VCET) for impact parameters of 500km up to the EPS-SG orbital height.
Improved Abel Inversion and additional modeling of electron density fields: application to EUMETSAT Polar System Second Generation Miquel Garcia-Fernàndez(1,2), Manuel Hernandez- Pajares(1), Antonio Rius(3),
More informationScintillation Nowcasting with GNSS Radio Occultation Data
Scintillation Nowcasting with GNSS Radio Occultation Data Keith Groves, Charles Carrano, Charles Rino and John Retterer Institute for Scientific Research, Boston College Paul Straus Aerospace Corporation
More informationWISE Science Data System Single Frame Position Reconstruction Peer Review: Introduction and Overview
WISE Science Data System Single Frame Position Reconstruction Peer Review: Introduction and Overview R. Cutri and the WSDC Team @ IPAC 1 Review Panel Rachel Akeson (IPAC/MSC) Gene Kopan (IPAC retired)
More informationSummary of IROWG Activities
Summary of IROWG Activities Co-Chairs: Ulrich Foelsche (University of Graz), Sean Healy (ECMWF) Rapporteur: Tony Mannucci (NASA/JPL) CGMS-45 COSMIC-IROWG, Korea, June Estes 2017 Park, Sept 2017 Slide:
More informationPreliminary evaluation of the impact of. cyclone assimilation and prediction
Preliminary evaluation of the impact of the FORMOSAT 7R wind on tropical cyclone assimilation and prediction Shu Chih Yang 1,2, Cheng Chieh Kao 1,2, Wen Hao Yeh 3 and Stefani Huang 1 1 Dept. of Atmospheric
More informationNEW CGMS BASELINE FOR THE SPACE-BASED GOS. (Submitted by the WMO Secretariat) Summary and Purpose of Document
WORLD METEOROLOGICAL ORGANIZATION COMMISSION FOR BASIC SYSTEMS OPEN PROGRAMME AREA GROUP ON INTEGRATED OBSERVING SYSTEMS EXPERT TEAM ON SATELLITE SYSTEMS ET-SAT-7/Inf. 2 (12.III.2012) ITEM: 8.1 SEVENTH
More informationNASA Future Magnetospheric Missions. J. Slavin & T. Moore Laboratory for Solar & Space Physics NASA GSFC
NASA Future Magnetospheric Missions J. Slavin & T. Moore Laboratory for Solar & Space Physics NASA GSFC Future Magnetospheric Missions Strategic Missions Radiation Belt Storm Probes (LWS/2011) Magnetospheric
More informationSpace-Based Polar Remote Sensing
in co- opera+on with Space-Based Polar Remote Sensing Malcolm Macdonald working with Pamela C Anderson, Carl Warren & Ben Dobke www.strath.ac.uk/mae 12 October 2012 View of Earth at 1200hrs UTC, 12 Slide
More informationSwift Mission Requirements Document
Version 2.4 November 14, 2002 NASA Goddard Space Flight Center TABLE OF CONTENTS Page REVISION HISTORY 4 DOCUMENT TREE 5 INTRODUCTION 6 APPLICABLE DOCUMENTS 6 SCIENCE REQUIREMENTS 7 MISSION REQUIREMENTS
More informationEquatorial and Low Latitude Scintillation Initiated From Low Altitude Forcing via Hurricanes/Typhoons
Equatorial and Low Latitude Scintillation Initiated From Low Altitude Forcing via Hurricanes/Typhoons Dr. Rebecca Bishop The Aerospace Corporation PSL/SSAL 30 March 2012 The Aerospace Corporation 2012
More informationmy_epp External Payload Platform
my_epp External Payload Platform A new Cubesat testbed and payload hosting platform on the International Space Station with reliable fast-track and low-cost mission scenario Dr. P. C. Steimle*, K. Kuehnel**,
More informationIMPACT OF GROUND-BASED GPS PRECIPITABLE WATER VAPOR AND COSMIC GPS REFRACTIVITY PROFILE ON HURRICANE DEAN FORECAST. (a) (b) (c)
9B.3 IMPACT OF GROUND-BASED GPS PRECIPITABLE WATER VAPOR AND COSMIC GPS REFRACTIVITY PROFILE ON HURRICANE DEAN FORECAST Tetsuya Iwabuchi *, J. J. Braun, and T. Van Hove UCAR, Boulder, Colorado 1. INTRODUCTION
More informationSP-1291 June Mars Express. The Scientific Investigations
SP-1291 June 2009 Mars Express The Scientific Investigations Operations and Archiving Mars Express Science Planning and Operations R. Pischel & T. Zegers ESA/ESTEC, Research and Scientific Support Department,
More informationSMAP Data Product Overview
http://smap.jpl.nasa.gov/ SMAP Data Product Overview ESIP Summer 2014 Copper Mountain, Colorado Barry Weiss Jet Propulsion Laboratory California Institute of Technology Pasadena, CA July 9, 2014 Copyright
More informationSimula'ons of COSMIC Follow On Sounding Distribu'ons and Data Latency for OSSE Studies
Simula'ons of COSMIC Follow On Sounding Distribu'ons and Data Latency for OSSE Studies Bill Schreiner Bill Kuo, Chris Rocken, Sergey Sokolovskiy UCAR/COSMIC Project Office Outline RO sounding distribugon
More informationThe Impacts of GPS Radio Occultation Data on the Analysis and Prediction of Tropical Cyclones. Bill Kuo, Xingqin Fang, and Hui Liu UCAR COSMIC
The Impacts of GPS Radio Occultation Data on the Analysis and Prediction of Tropical Cyclones Bill Kuo, Xingqin Fang, and Hui Liu UCAR COSMIC GPS Radio Occultation α GPS RO observations advantages for
More informationNew Radiosonde Temperature Bias Adjustments for Potential NWP Applications Based on GPS RO Data
Eighth FORMOSAT-3/COSMIC Data Users Workshop 30 September 2 October 2014 Boulder, Colorado, USA New Radiosonde Temperature Bias Adjustments for Potential NWP Applications Based on GPS RO Data Bomin Sun
More informationImpact of GPS RO Data on the Prediction of Tropical Cyclones
Impact of GPS RO Data on the Prediction of Tropical Cyclones Ying-Hwa Kuo, Hui Liu, UCAR Ching-Yuang Huang, Shu-Ya Chen, NCU Ling-Feng Hsiao, Ming-En Shieh, Yu-Chun Chen, TTFRI Outline Tropical cyclone
More informationProton Launch System Mission Planner s Guide APPENDIX F. Proton Launch System Options and Enhancements
Proton Launch System Mission Planner s Guide APPENDIX F Proton Launch System Options and Enhancements F. PROTON LAUNCH SYSTEM OPTIONS AND ENHANCEMENTS The missions presented in the previous sections represent
More informationClimate Monitoring with Radio Occultation Data
Climate Monitoring with Radio Occultation Data Systematic Error Sources C. Rocken, S. Sokolovskiy, B. Schreiner, D. Hunt, B. Ho, B. Kuo, U. Foelsche Radio Occultation Claims Most stable Global Thermometer
More informationBOWSER Balloon Observatory for Wavelength and Spectral Emission Readings
COSGC Space Research Symposium 2009 BOWSER Balloon Observatory for Wavelength and Spectral Emission Readings BOWSER 1 Mission Premise 4.3 km above sea level 402.3km above sea level BOWSER 2 Information
More informationDynamical. regions during sudden stratospheric warming event (Case study of 2009 and 2013 event)
Dynamical Coupling between high and low latitude regions during sudden stratospheric warming event (Case study of 2009 and 2013 event) Vinay Kumar 1,S. K. Dhaka 1,R. K. Choudhary 2,Shu-Peng Ho 3,M. Takahashi
More information4/23/2014. Radio Occultation as a Gap Filler for Infrared and Microwave Sounders Richard Anthes Presentation to Joshua Leiling and Shawn Ward, GAO
Radio Occultation as a Gap Filler for Infrared and Microwave Sounders Richard Anthes Presentation to Joshua Leiling and Shawn Ward, GAO 1 RICHARD ANTHES is President Emeritus of the University Corporation
More informationJAXA s Venus Climate Orbiter (PLANET-C) overview. Launch: Jun 2010 Arrival: Dec 2010 Mission life: 2 years
JAXA s Venus Climate Orbiter (PLANET-C) overview Launch: Jun 2010 Arrival: Dec 2010 Mission life: 2 years Venus and Earth They have almost the same size and mass. Surface environments are completely different.
More informationSciBox, a Proven Automated Planning and Commanding System
SciBox, a Proven Automated Planning and Commanding System Teck Choo, Edward Russell, Michael Kim February 25, 2014 2014 by The Johns Hopkins University/Applied Physics Laboratory. Published by The Aerospace
More informationESSE Payload Design. 1.2 Introduction to Space Missions
ESSE4360 - Payload Design 1.2 Introduction to Space Missions Earth, Moon, Mars, and Beyond Department of Earth and Space Science and Engineering Room 255, Petrie Science and Engineering Building Tel: 416-736
More informationFuture Opportunities of Using Microwave Data from Small Satellites for Monitoring and Predicting Severe Storms
Future Opportunities of Using Microwave Data from Small Satellites for Monitoring and Predicting Severe Storms Fuzhong Weng Environmental Model and Data Optima Inc., Laurel, MD 21 st International TOV
More informationA Case Study of Modal Mass Acceleration Curve Loads vs. Sine Loads
A Case Study of Modal Mass Acceleration Curve Loads vs. Sine Loads Ramses Mourhatch Bing-Chung Chen Walter Tsuha Peyman Mohasseb Chia-Yen Peng Jet Propulsion Laboratory California Institute of Technology
More informationOVERVIEW OF EUMETSAT RADIO OCCULTATION ACTIVITIES
1 Eighth FORMOSAT-3/COSMIC Data Users' Workshop, Sep/Oct 2014, Boulder OVERVIEW OF EUMETSAT RADIO OCCULTATION ACTIVITIES Axel von Engeln, Christian Marquardt, Yago Andres Overview EUMETSAT Mission Overview
More informationDevelopment of the Next Generation GRAS Instrument
Development of the Next Generation GRAS Instrument Jacob Christensen Magnus Bonnedal, Anders Carlström, Thomas Lindgren Sean Healy (ECMWF), Hans-Henrik Benzon (DMI) RUAG Space Gothenburg Sweden D-I-HO-00022-RSE,
More informationThe Use of GPS Radio Occultation Data for Tropical Cyclone Prediction. Bill Kuo and Hui Liu UCAR
The Use of GPS Radio Occultation Data for Tropical Cyclone Prediction Bill Kuo and Hui Liu UCAR Current capability of the National Hurricane Center Good track forecast improvements. Errors cut in half
More informationThe AEOLUS Mission - In Orbit Commissioning and Verification
The AEOLUS Mission - In Orbit Commissioning and Verification ADM-Aeolus CAL/VAL Workshop, ESRIN P McGoldrick, J Brewster, J Marshall, F Fabre Airbus Defence and Space, UK and France 12 th February 2015
More informationIR sounder small satellite for polar orbit weather measurements
IR sounder small satellite for polar orbit weather measurements Sara Lampen, Sonny Yi, Jared Lang, Caleb Lampen, Adam Vore, David Warren, Eric Herman The Aerospace Corporation John J. Pereira National
More informationSystem engineering approach toward the problem of required level of in-orbit autonomousoperation of a LEO microsatellite mission
System engineering approach toward the problem of required level of in-orbit autonomousoperation of a LEO microsatellite mission H.Bonyan Amirkabir University of Technology (AUT) H.Bonyan@dena.aut.ac.ir
More informationMegha-Tropiques Presentation by Indian Delegation at the 55th Session of UNCOPUOS Vienna 12 June 2012
Megha-Tropiques Presentation by Indian Delegation at the 55 th Session of UNCOPUOS Vienna 12 June 2012 Megha-Tropiques Mission Indo-French Joint Satellite for studying tropical atmosphere Megha in Sanskrit
More informationSystems Engineering in Venus Satellite
Systems Engineering in Venus Satellite How to benefit from system engineering process in designing a microsatellite Jacob Herscovitz Venus Project Manager RAFAEL - Israel 1 Presentation Contents Introduction
More informationOperational Aspects of Space Weather-Related Missions
Operational Aspects of Space Weather-Related Missions Richard G. Marsden, ESA/SCI-SH Outline SOHO: Example of Near-Earth Observatory-class Mission Ulysses: Example of Deep Space Monitor-class Mission Solar
More informationReduction of the Response Time of Earth Observation Satellite Constellations using Inter-satellite Links
Reduction of the Response Time of Earth Observation Satellite Constellations using Inter-satellite Links S. De Florio Data quality of Earth observation satellites is often evaluated in terms of short system
More informationExploration Carriers UPC-Orion Launch Opportunities for Lunar Missions. presented to The Joint Annual Meeting of LEAG-ICEUM-SRR
Exploration Carriers UPC-Orion Launch Opportunities for Lunar Missions presented to The Joint Annual Meeting of LEAG-ICEUM-SRR Bruce Milam and Ruthan Lewis, Ph.D. NASA Goddard Space Flight Center October
More informationINTEGRATED OPERATIONAL PRECISE ORBIT DETERMINATION FOR LEO
INTEGRATED OPERATIONAL PRECISE ORBIT DETERMINATION FOR LEO J. Fernández Sánchez, F. M. Martínez Fadrique, A. Águeda Maté, D. Escobar Antón GMV S.A., Isaac Newton, 8760 Tres Cantos, Spain, Email: jfernandez@gmv.com,
More informationTaiwan Radio Occultation Process System (TROPS)
Taiwan Radio Occultation Process System (TROPS) Cheng-Yung Huang, Wen-Hao Yeh, Kun-Lin Chen National Space Organization, National Applied Research Laboratories Shu-Ya Chen, Jing-Mei Wu, Hsiu-Wen Li, Kuo-Hsin
More informationThe Orbiting Carbon Observatory (OCO) Mission Watching The Earth Breathe Mapping CO 2 From Space. The OCO-3 Mission: An Overview
The Orbiting Carbon Observatory (OCO) Mission Watching The Earth Breathe Mapping CO 2 From Space. The OCO-3 Mission: An Overview Annmarie Eldering and the OCO-3 Team May 2013 IWGGMS Meeting Yokohama, Japan
More informationAdvanced Ionospheric Probe Onboard FORMOSAT-5 Satellite
Advanced Ionospheric Probe Onboard FORMOSAT-5 Satellite C. K. Chao 1, C. M. Huang 1, Y. H. Chu 1, C. L. Su 1, J. Y. Liu 1, and S. Minami 2 1 Institute of Space Science, National Central University, Taiwan
More informationF. Letterio, S. Tonetti, S. Cornara, G. Vicario presented by Mariano Sánchez Nogales
DESEO Design Engineering F. Letterio, S. Tonetti, S. Cornara, G. Vicario presented by Mariano Sánchez Nogales DEIMOS Space S.L.U., Spain - 1 - Table of Contents DESEO Overview Toolkit Heritage Software
More informationFigure 1. View of ALSAT-2A spacecraft
ALSAT-2A TRANSFER AND FIRST YEAR OPERATIONS M. Kameche (1), A.H. Gicquel (2), D. Joalland (3) (1) CTS/ASAL, 1 Avenue de la Palestine, BP 13, Arzew 31200 Oran, Algérie, email:mo_kameche@netcourrier.com
More informationAvailable online at ScienceDirect. Procedia Engineering 79 (2014 ) Chen-Hao Wang*, Jeng-Der Huang, Chia-Ray Chen
Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 79 (2014 ) 279 288 37th National Conference on Theoretical and Applied Mechanics (37th NCTAM 2013) & The 1st International Conference
More informationSpace Studies Board Meeting Mary E. Kicza
Space Studies Board Meeting Mary E. Kicza Assistant Administrator for Satellites and Information Services May 14, 2009 1 Summary Budget Update FY 2009 Stimulus (ARRA) FY 2009 Omnibus FY 2010 President
More informationTeam X Study Summary for ASMCS Theia. Jet Propulsion Laboratory, California Institute of Technology. with contributions from the Theia Team
Team X Study Summary for ASMCS Theia Jet Propulsion Laboratory, California Institute of Technology with contributions from the Theia Team P. Douglas Lisman, NASA Jet Propulsion Laboratory David Spergel,
More informationDevelopment of Spaceborne Dualfrequency. and Its Role for the Global Precipitation Measurement
Development of Spaceborne Dualfrequency Precipitation Radar and Its Role for the Global Precipitation Measurement Shinsuke Satoh (1), Riko Oki (1), Nobuhiro Takahashi (2), and Toshio Iguchi (2) (1) National
More informationA New Mission Concept: The Search for Trace Gases in the Mars Atmosphere
A New Mission Concept: The Search for Trace Gases in the Mars Atmosphere Richard Zurek Jet Propulsion Laboratory/California Institute of Technology Augustin Chicarro European Space Agency November 27,
More informationAttitude Control Simulator for the Small Satellite and Its Validation by On-orbit Data of QSAT-EOS
SSC17-P1-17 Attitude Control Simulator for the Small Satellite and Its Validation by On-orbit Data of QSAT-EOS Masayuki Katayama, Yuta Suzaki Mitsubishi Precision Company Limited 345 Kamikmachiya, Kamakura
More information