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Geostationary Operational Environmental Satellite- R Series (GOES-R) 2016
Student Works 12-14-2016 Geostationary Operational Environmental Satellite- R Series (GOES-R) 2016 Paige N. Dixon Embry-Riddle Aeronautical University Follow this and additional works at: https://commons.erau.edu/student-works Part of the Aviation and Space Education Commons, Meteorology Commons, and the Space Vehicles Commons Scholarly Commons Citation Dixon, P. N. (2016). Geostationary Operational Environmental Satellite- R Series (GOES-R) 2016. , (). Retrieved from https://commons.erau.edu/student-works/67 This Undergraduate Research is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Student Works by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Geostationary Operational Environmental Satellite- R Series (GOES-R) 2016 Paige N. Dixon Embry-Riddle Aeronautical University, Prescott, Arizona ABSTRACT This is a report on the first NOAA GOES-R satellite, launched on November 19th, 2016. This report will cover some of the details of the GOES-R project, as well as discuss the collaborations that made the project possible. This document will also detail some of the new satellite’s capabilities including geostationary lightning detection, and space weather monitoring, and will focus on real-world application of such technology. Additionally, this report will list some of the current and projected GOES-R products, and the potential benefits if testing proves successful. 1 1. Introduction The National Oceanic and Atmospheric Administration better known as NOAA, in collaboration with the National Aeronautics and Space Administration or NASA launched the first of the R-series GOES satellites into orbit on 19 November, of this year. -
Gridded Satellite (Gridsat) GOES and CONUS Data Kenneth R
Discussions Earth Syst. Sci. Data Discuss., https://doi.org/10.5194/essd-2018-33 Earth System Manuscript under review for journal Earth Syst. Sci. Data Science Discussion started: 27 April 2018 c Author(s) 2018. CC BY 4.0 License. Open Access Open Data Gridded Satellite (GridSat) GOES and CONUS data Kenneth R. Knapp1 and Scott L. Wilkins2 1NOAA/NESDIS/National Centers for Environmental Information, Asheville, NC 28801, USA 2Cooperative Institute for Climate and Satellites – North Carolina (CICS-NC), North Carolina State University, Asheville, NC 5 28801, USA Correspondence to: Kenneth R. Knapp ([email protected]) Abstract. The Geostationary Operational Environmental Satellite (GOES) series is operated by the U. S. National Oceanographic and Atmospheric Administration (NOAA). While in operation since the 1970s, the current series (GOES 8- 15) has been operational since 1994. This document describes the Gridded Satellite (GridSat) data, which provides GOES data 10 in a modern format. Four steps describe the conversion of original GOES data to GridSat data: 1) temporal resampling to produce files with evenly spaced time steps, 2) spatial remapping to produce evenly spaced gridded data (0.04° latitude), 3) calibrating the original data and storing brightness temperatures for infrared channels and reflectance for the visible channel, and 4) calculating spatial variability to provide extra information that can help identify clouds. The GridSat data are provided on two separate domains: GridSat-GOES provides hourly data for the Western Hemisphere (spanning the entire GOES domain) 15 and GridSat-CONUS covers the contiguous U.S. (CONUS) every 15 minutes. Dataset reference: doi:10.7289/V5HM56GM 1 Introduction NOAA has used the Geostationary Operational Environmental Satellite (GOES) series since 1975 to monitor weather. -
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. -
2019 Nano/Microsatellite Market Forecast, 9Th Edition
2019 NANO/MICROSATELLITE MARKET FORECAST, 9TH EDITION Copyright 2018, SpaceWorks Enterprises, Inc. (SEI) APPROVED FOR PUBLIC RELEASE. SPACEWORKS ENTERPRISES, INC., COPYRIGHT 2018. 1 Since 2008, SpaceWorks has actively monitored companies and economic activity across both the satellite and launch sectors 0 - 50 kg 50 - 250kg 250 - 1000kg 1000 - 2000kg 2000kg+ Custom market assessments are available for all mass classes NANO/MICROSATELLITE DEFINITION Picosatellite Nanosatellite Microsatellite Small/Medium Satellite (0.1 – 0.99 kg) (1 – 10 kg) (10 – 100 kg) (100 – 1000 kg) 0 kg 1 kg 10 kg 100 kg 1000 kg This report bounds the upper range of interest in microsatellites at 50 kg given the relatively large amount of satellite development activity in the 1 – 50 kg range FORECASTING METHODOLOGY SpaceWorks’ proprietary Launch Demand Database (LDDB) Downstream serves as the data source for all satellite market Demand assessments ▪ Planned The LDDB is a catalogue of over 10,000+ historical and Constellations future satellites containing both public and non-public (LDDB) satellite programs Launch Supply SpaceWorks newly updated Probabilistic Forecast Model (PFM) is used to generate future market potential SpaceWorks PFM Model ▪ The PFM considers down-stream demand, announced/planed satellite constellations, and supply-side dynamics, among other relevant factors Expert Analysis The team of expert industry analysts at SpaceWorks SpaceWorks further interprets and refines the PFM results to create Forecast accurate market forecasts Methodology at a Glance 2018 SpaceWorks forecasted 2018 nano/microsatellite launches with unprecedented accuracy – actual satellites launched amounted to just 5% below our analysts’ predictions. In line with SpaceWorks’ expectations, the industry corrected after a record launch year in 2017, sending 20% less nano/microsatellites to orbit than in 2018. -
ITU Smallsat Workshop
Exponential Improvements in SmallSat Technology Jenny Barna! Launch Manager, Spire! [email protected] Spire’s Beginnings • Founded in 2012 as Nanosatisfi to launch cubesats with Arduino educational payloads! • Headquarters in San Francisco, CA! • Launched first crowd-funded satellite in 2013! • Rebranded to Spire in 2014 (Spire Global, Inc) 2 Spire Today • Raised $25M Series A (2014)! • Opened offices in Singapore, Glasgow! • Team of 40+ and growing! • Remote sensing payloads! • Global AIS ship tracking! • GPS-RO weather data ! • Ardusat-Spire educational partnership 3 Spire’s Launch History 4 satellites launched to date:! ! • ArduSat-1, ArduSat-X (1U)! August 2013! H-IIB/ISS! ! • ArduSat-2 (2U)! January 2014! Antares/ISS! ! • LEMUR-1 (3U) - operational June 2014! Dnepr 4 The TechnologyThe Technology The platform" • 3U cubesat! • Designed & manufactured by Spire • Leverages COTS hardware! • In-house software development! ! The constellation! • 20 satellites in orbit by end of 2015" • 100+ satellites in orbit in 3 years" • Variety of altitudes (500-700 km)" • Variety of inclinations" • Unprecedented coverage, revisit time 5 SmallSats:! Because we’ve come a long way since the 80’s. 6 HistoryMoore’s RepeatingLaw - Consumer Itself Electronics(Moore’s Law) 10x lighter! 1990 10x cheaper! 2015 100x more capable Mac IIfx Cost: $10,000! MacBook Air Cost: $1000! Weight: 24 pounds! Weight: < 3 pounds! Memory: 16 MB! Memory: 4 GB! Processor: 40 MHz Processor:1.4 GHz 7 HistoryMoore’s RepeatingLaw - Spacecraft Itself Sensors(Moore’s Law) 1000x ! price/performance improvement 5g (cubesat shop) TNO Digital Sun Sensor, 475g 2012 2006 8 Moore’sCubesat Law Technology - Cubesats Shift Memory Power Bandwidth 9 Easier,Launch More Opportunity Frequent Access Shift to Space 2000 2015 ULA launches costed about an average of $225 Spaceflight’s first SHERPA fully booked with Million, and were almost exclusively sold to the US SmallSats. -
Preparation of Papers for AIAA Journals
Analysis of Satellite Radio Occultation Architecture and its Stakeholders I. Josue Tapia-Tamayo1 and Paul T. Grogan2 Stevens Institute of Technology, Hoboken, NJ 07030, USA Global Navigation Satellite System Radio Occultation (GNSS-RO) is a technique that relies on the change of a signal transmitted from a Global Navigation Satellite System (GNSS) as it passes through the planet’s atmosphere. This technique is not only suitable to study weather forecasting or climate change, but also offers a low-cost application. This report aims to characterize and parametrize the system architecture of commercial companies pursuing the Commercial Weather Data Pilot (CWDP) contract by the National Oceanic and Atmospheric Administration (NOAA). The approach of the paper will start by explaining the Radio Occultation technique and its potential application to Numerical Weather Prediction (NWP). The paper then identifies the main stakeholders of radio occultation and NWP, and their needs. Some key functional requirements are pinpointed, and the challenges that some of these architectures must overcome is discussed. Introduction The increase of severe weather in the last decade has led to the need for improvement of U.S. weather forecasting. Severe weather such as hurricanes and flooding causes great economic damage to cities. According to National Oceanic and Atmospheric Administration (NOAA), the cost of economic damage caused by hurricanes was $161 billion for Katrina in 2005, $71 billion for Sandy in 2012, $125 billion for Harvey in 2017, $90 billion for Maria in 2017, and $50 billion for Irma in 2017. The overall cost of hurricanes in the U.S. reached $515.4 billion in insured property losses from 1986 to 2015. -
Spire's Cubesat Constellation of GNSS, AIS, and ADS-B Sensors
Seizing Opportunity: Spire’s CubeSat Constellation of GNSS, AIS, and ADS-B Sensors Dallas Masters, Director of GNSS, Spire Global, Inc. Stanford PNT Symposium, 2018-11-08 WHO & WHAT IS SPIRE? We’re a new, innovative satellite & data services company that you might not have heard of… We’re what you get when you mix agile development with nanosatellites... We’re the transformation of a single , crowd-sourced nanosatellite into one of the largest constellations of satellites in the world... Stanford PNT Symposium, 2018-11-08 OUTLINE 1. Overview of Spire 2. Spire satellites and PNT payloads & products a. AIS ship tracking b. GNSS-based remote sensing measurements: radio occultation (RO), ionosphere electron density, bistatic radar (reflections) c. ADS-B aircraft tracking (early results) 3. Spire’s lofty long-term goals Stanford PNT Symposium, 2018-11-08 AN OVERVIEW OF SPIRE Stanford PNT Symposium, 2018-11-08 SPIRE TODAY • 150 people across five offices (a distributed start-up) - San Francisco, Boulder, Glasgow, Luxembourg, and Singapore • 60+ LEO 3U CubeSats (10x10x30 cm) in orbit with passive sensing payloads, 30+ global ground stations - 16 launch campaigns completed with seven different launch providers - Ground station network owned and operated in-house for highest level of security and resilience • Observing each point on Earth 100 times per day, everyday - Complete global coverage, including the polar regions • Deploying new applications within 6-12 month timeframes • World’s largest ship tracking constellation • World’s largest weather -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Since Our Last SIA Member News Summary, Press Releases and Posts
SIA PRESIDENT’S REPORT – MEMBER NEWS FOR FEB 2021 Since our last SIA Member News Summary, press releases and posts from many SIA Members including ABS, Boeing, Hawkeye 360, Inmarsat, Omnispace, OneWeb, Planet, SES, SpaceX, Spire Global, ULA and Viasat have released news. Please see the summary of stories and postings below and click on the COMPANY LINK for more details. Above: The ULA Vulcan Centaur launch platform (VLP) and Pathfinder Tanking Test (PTT) booster nears the ULA Spaceflight Operations Control Center located at the Cape Canaveral Space Force Station. For more details, see the information below. Photo credit: Image courtesy of ULA. ULA On Feb 22nd, ULA posted the following blog announcement. “At ULA's Vertical Integration Facility (VIF) on Monday, Feb. 15, the Vulcan Centaur program achieved a significant milestone when the Pathfinder Tanking Test (PTT) booster was hoisted into place aboard the Vulcan Launch Platform (VLP). PTT is a flight configuration core stage that will complete validations of the launch site and later be used on a Vulcan Centaur launch into space.” Earlier in the month, a pathfinder first stage that will pave the way for Vulcan Centaur's inaugural launch arrived at Cape Canaveral from ULA's factory in Decatur, Alabama, to begin launch site testing of the next-generation rocket. The Pathfinding Tanking Test (PTT) booster, a flight configuration Vulcan Centaur core fitted with a pair of BE-4 development engines, was produced using the advanced automation and tooling in Decatur that is designed for maximum efficiency and reliability. INMARSAT On Feb 24th, Inmarsat announced the appointment of Rajeev Suri as CEO replacing Rupert Pearce. -
'IT's Business Time' Press Kit NOVEMBER 2018 ROCKET LAB PRESS KIT 'IT's BUSINESS TIME' 2018
ROCKET LAB USA 2018 'IT's business time' press Kit NOVEMBER 2018 ROCKET LAB PRESS KIT 'IT'S BUSINESS TIME' 2018 Mission Overview About the It’s Business Time Payloads Rocket Lab will open a nine day launch window for It's Business Time from 11 - 19 November 2018 NZDT. Launch attempts will take place within this during a daily four hour window beginning at 16:00 NZDT, or 03:00 UTC. Rocket Lab's Electron launch vehicle will loft six satellites and a technology demonstrator to Low Earth Orbit. The payloads will be launched to a 210km x 500km circular orbit at 85 degrees, before being circularized to 500 x 500 km using Rocket Lab’s Curie engine powered kick stage. It's Business Time is manifested with commercial satellites from Spire Global, Tyvak Nano-Satellite Systems, Fleet Space Technologies, as well as an educational payload from the Irvine CubeSat STEM Program (ICSP) and a drag sail technology demonstrator designed and built by High Performance Space Structure Systems GmBH (HPS GmbH). Ecliptic Enterprises Corporation, assisted with the pairing of NABEO with Electron as a candidate hosted technology demonstrator. PAYLOADS LEMUR-2-ZUPANSKI & LEMUR-2-CHANUSIAK Tyvak Nanosatellite Systems Electron will loft two Lemur-2 satellites, LEMUR-2-ZUPANSKI and It's Business Time will also carry a satellite for GeoOptics Inc., built LEMUR-2-CHANUSIAK, for data and analytics company Spire. These by Tyvak Nano-Satellite Systems. Headquartered in Irvine, CA, Tyvak satellites will join Spire's constellation of more than sixty nanosatellites Nano-Satellite Systems provides end-to-end nanosatellite solutions to currently in Low Earth Orbit. -
Early Contributions to Today's JPSS Initiatives As Seen from the First
TIROS-1 Established the Foundation for Today’s Remarkable JPSS and GOES-R Satellite Systems Gerald J. Dittberner* CIRA, Colorado State University, Fort Collins, CO and Thomas H. Vonder Haar Colorado State University, Fort Collins, CO *[email protected] Presented at the 16th Annual Symposium on New Generation Operational Environmental Satellite Systems, 100th American Meteorological Society Annual Meeting, Boston, MA, January 13, 2020 1 Outline JPSS TIROS ✦ The Path to Polar and Geostationary Systems th ✦ Celebrate the 60 anniversary of TIROS-1 ✦ The first operational weather satellite (1 Apr 1960) ✦ Satellites and Instruments ✦ Milestones ✦ Meteorology: Early initiatives for Operational Applications Dittberner and Vonder Haar, CIRA, Colorado State University 2 First Color Image from Space - JPSS TIROS Aerobee Rocket (1954) Source: Hubert and Berg, 1944 Dittberner and Vonder Haar, CIRA, Colorado State University 3 Diverse Collaborators Initiated Weather Satellites JPSS TIROS IGY Satellites TIROS Satellites 1955 - 1958 1958+ National Academies NASA* Designated to Coordinate Planning: Sponsor & Coordinate Execution - Army Signal Corps Rsrch Lab (Payload) - US Weather Bureau (Data Handling) - Naval Rsrch Lab (Vanguard Team) - Army Signal Corps Rsrch Lab (Payload) - Army Corps of Engineers - Naval Rsrch Lab (Vanguard Team) - Army Ballistic Missile Agency (Explorer) - Industries (esp. RCA) - Industries (esp. RCA) - Universities (Univ Iowa esp) - Universities (esp. Univ Iowa) - WWW (International Cooperation) - ARPA* Office of Naval Research* National Science Foundation* *sponsor transferring from ONR and NSF during IGY Source: A. Callahan, 2013 Dittberner and Vonder Haar, CIRA, Colorado State University 4 TIROS-1 JPSS TIROS Equipped with two TV cameras and two video recorders, the spacecraft orbited 450 miles above Earth, relaying nearly 20,000 images of clouds and storm systems moving across our planet. -
Failures in Spacecraft Systems: an Analysis from The
FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof.