FY18 Q1 REPORT Quarterly Report for the Period October 1 – December 31, 2017
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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 -
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. -
ISS National Lab Q1FY19 Report Quarterly Report for the Period October 1 – December 31, 2018
NASAWATCH.COM ISS National Lab Q1FY19 Report Quarterly Report for the Period October 1 – December 31, 2018 Contents Q1FY19 Metrics ........................................................................................................................................... 2 Key Portfolio Data Charts ............................................................................................................................. 6 Program Successes ...................................................................................................................................... 6 In-Orbit Activities ........................................................................................................................................ 7 Research Solicitations in Progress ................................................................................................................ 7 Appendix .................................................................................................................................................... 8 Authorized for submission to NASA by: _______________________________ Print Name _______________ Signature ________________________________________________________ 1 NASAWATCH.COM NASAWATCH.COM ISS National Lab Q1FY19 Report Q1FY19 Metrics SECURE STRATEGIC FLIGHT PROJECTS: Generate significant, impactful, and measurable demand from customers that recognize value of the ISS National Lab as an innovation platform TARGET ACTUAL Q1 ACTUAL Q2 ACTUAL Q3 ACTUAL Q4 YTD FY19 FY19 ISS National Lab payloads manifested -
'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. -
SSEP Mission 14 to ISS Profile
SSEP Mission 14 to ISS Profile Contact: Jeff Goldstein, SSEP National Program Director, 301-395-0770, [email protected] Payload and Flight Ops: Number of SSEP experiments: 33 experiments, with 3 flying on SpaceX-23 SSEP Payload Designation: Apollo (SSEP16) Flight: SpaceX CRS-23, Launch Complex 39A, Kennedy Space Center, Florida Mission 14 Community Engagement: Number of communities engaged: 32 Number of students engaged in microgravity experiment design: 16,600 (grades 5-16) Number of flight experiment proposals submitted by student teams: 3,076 Number of finalist proposals submitted to Step 2 Review at NASA Goddard Spaceflight Center’s Visitor Center: 97 Number of experiments selected for flight (one for 31 communities and two for 1 community): 33 Flight Experiment Student Researchers: 129 (82 PIs & Co-PIs; 22 Co-Is; 25 Collaborators) The Student Spaceflight Experiments Program [or SSEP] is a program of the National Center for Earth and Space Science Education (NCESSE) in the U.S. and the Arthur C. Clarke Institute for Space Education internationally. It is enabled through a strategic partnership with DreamUp PBC and NanoRacks LLC, which are working with NASA under a Space Act Agreement as part of the utilization of the International Space Station as a National Laboratory. SSEP is the first pre- college STEM education program that is both a U.S. national initiative and implemented as an on-orbit commercial space venture. The Smithsonian National Air and Space Museum, the Center for the Advancement of Science in Space (CASIS), and Subaru of America, Inc., are U.S. National Partners on the Student Spaceflight Experiments Program. -
CWDP) Round 2 Summary
NOAA/NESDIS Commercial Weather Data Pilot (CWDP) Round 2 Summary June 2020 Commercial Weather Data Pilot: Round 2 Summary June 2020 Background Radio Occultation (RO) is an established method for remote sounding of the atmosphere. The technique uses an instrument in low-Earth orbit to track radio signals from Global Navigation Satellite System (GNSS) transmitters as they rise or set through the atmosphere. The occulting atmosphere refracts or bends the radio signals, and given the precise positions of both satellites, the bending angle can be deduced from the time delay of the signal. Collecting these measurements for a full occultation through the atmosphere provides a vertical profile of bending angles, from which profiles of physical quantities such as temperature, humidity, and ionospheric electron density can be retrieved. These data primarily feed numerical weather prediction (NWP) models that support weather forecasts, and also support space weather applications. Deployable on small satellites, RO instruments complement microwave and infrared sensors, fill in the sparse geographical and temporal coverage of radiosondes, and provide vertical and temporal resolution complementing other satellite observations. Weather centers currently ingest thousands of RO profiles per day from various government satellite systems. Studies indicate that increasing the quantity of RO data, particularly in orbits and times not served by government systems, would further improve forecasts. Ionospheric observations from RO sensors also enhance space weather situational awareness, revealing variations in the ionosphere that impact GNSS performance and radio communications. Beyond these direct benefits, additional sources of RO data could provide risk mitigation for any unexpected reductions in other data streams. NOAA began assessing the potential of commercial sources of RO data in 2008 as part of contracted studies to assess a variety of commercial capabilities. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 3 July–September 2019 CONTENTS FOCUS ..................................................................................................................... 1 A new European Commission DG for Defence Industry and Space .............................................. 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 EEAS announces 3SOS initiative building on COPUOS sustainability guidelines ............................ 2 Europe is a step closer to Mars’ surface ......................................................................... 2 ESA lunar exploration project PROSPECT finds new contributor ............................................. 2 ESA announces new EO mission and Third Party Missions under evaluation ................................ 2 ESA advances space science and exploration projects ........................................................ 3 ESA performs collision-avoidance manoeuvre for the first time ............................................. 3 Galileo's milestones amidst continued development .......................................................... 3 France strengthens its posture on space defence strategy ................................................... 3 Germany reveals promising results of EDEN ISS project ....................................................... 4 ASI strengthens -
Orbital Debris Assessment Report and Mitigation Plan Spire Global, Inc. FCC ELS Text Documents Document [1228-EX-ST-2019]
2017 Spire Global, Inc. Orbital Debris Assessment Report LEMUR-2 Satellites Phase IC (with Hosted Payloads) and Phase II Revision History Revision Description of Revisions Release Date 1 Initial Release 10/13/2017 An orbital debris risk assessment of LEMUR-2 Phase IC (with hosted payload) and Phase II satellites Section 1: Program Management and Mission Overview Program / Project Jenny Barna Manager Mission The purpose of the LEMUR-2 satellite constellation is to provide high-revisit global maritime and Description aircraft domain monitoring data, weather data, and hosted payload services. This orbital debris risk assessment report (“ODAR”) covers any LEMUR-2 Phase IC satellites with a hosted payload and Phase II satellites proposed to be launched by Spire Global, Inc. (“Spire”). Foreign None Government Involvement Project Milestones LEMUR-2 satellites are usually launched in small deployments depending on available capacity, quality of orbit, service and constellation replenishment needs, and risk profiles of the launch Proposed vehicle and campaign. Launch Date Given the potential long lead time for the instant application and state of the low-Earth orbit Proposed launch market for secondary payloads, Spire is filing this application early and is not capable of Launch Vehicles providing launch parameters for the Phase II satellites at this time. However, it notes that these satellites (similar to the Phase I, IB, and IC satellites) will only deploy at orbital altitudes from 385 Proposed to 650 km and inclinations ranging from equatorial to polar sun-synchronous (98 degrees). Launch Sites This analysis considers the range of representative orbits and includes a debris assessment of the Launch Vehicle worst-case altitude and lifetime in order to provide the most conservative results. -
Synthetic Biology for Climate Change
Abdullah 1 SYNTHETIC BIOLOGY FOR CLIMATE CHANGE: APPLYING MODIFIED CARBON DIOXIDE CONSUMING E.COLI TESTED IN SPACE TO CARBON SCRUBBING TECHNOLOGY IN SPACE AND ON EARTH Mahlak Abdullah Space4Youth Essay Competition Date Submitted: 25 April 2021 Abdullah 2 Abstract Compared to conventional production methods, a genetically modified strain of E. coli made to consume carbon dioxide could contribute to previous efforts made to improve air quality. With the results from a NASA sponsored research I worked on to send this E.coli to the ISS, the applications to climate change can reach to and beyond using this bacteria in carbon scrubbing technology. In a fluid containing enclosure, we observed E.coli's growth in a weightless environment. This investigation proposal strives to build upon our results by expanding the applicability of this modified microbe in both gravity and microgravity environments. Abdullah 3 Introduction Despite growing awareness of climate change, global greenhouse gas emissions are taking their toll. Taking this into consideration and thought, scientists have, in recent years, worked to implement improvements that have been made in synthetic biology (Milo et. al, 2019). Synthetic biology refers to the implementation of engineering principles to studies pertaining to the ways in which organic life is driven (Biotechnology Innovation Organization). Such principles are being utilized to aid in combating some of our most pressing environmental challenges. The Genetic Modification of Escherichia coli for a Carbon Dioxide-Based Diet Taking matters into hand, researchers in the Middle Eastern region have been tapping synthetic organisms in hopes of converting atmospheric carbon dioxide into various forms for human use including food, fuel, and organic chemicals.