Spaceflight Joins with Nanoracks to Deploy Satellites from the International Space Station
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Spacex Launch Manifest - a List of Upcoming Missions 25 Spacex Facilities 27 Dragon Overview 29 Falcon 9 Overview 31 45Th Space Wing Fact Sheet
COTS 2 Mission Press Kit SpaceX/NASA Launch and Mission to Space Station CONTENTS 3 Mission Highlights 4 Mission Overview 6 Dragon Recovery Operations 7 Mission Objectives 9 Mission Timeline 11 Dragon Cargo Manifest 13 NASA Slides – Mission Profile, Rendezvous, Maneuvers, Re-Entry and Recovery 15 Overview of the International Space Station 17 Overview of NASA’s COTS Program 19 SpaceX Company Overview 21 SpaceX Leadership – Musk & Shotwell Bios 23 SpaceX Launch Manifest - A list of upcoming missions 25 SpaceX Facilities 27 Dragon Overview 29 Falcon 9 Overview 31 45th Space Wing Fact Sheet HIGH-RESOLUTION PHOTOS AND VIDEO SpaceX will post photos and video throughout the mission. High-Resolution photographs can be downloaded from: http://spacexlaunch.zenfolio.com Broadcast quality video can be downloaded from: https://vimeo.com/spacexlaunch/videos MORE RESOURCES ON THE WEB Mission updates will be posted to: For NASA coverage, visit: www.SpaceX.com http://www.nasa.gov/spacex www.twitter.com/elonmusk http://www.nasa.gov/nasatv www.twitter.com/spacex http://www.nasa.gov/station www.facebook.com/spacex www.youtube.com/spacex 1 WEBCAST INFORMATION The launch will be webcast live, with commentary from SpaceX corporate headquarters in Hawthorne, CA, at www.spacex.com. The webcast will begin approximately 40 minutes before launch. SpaceX hosts will provide information specific to the flight, an overview of the Falcon 9 rocket and Dragon spacecraft, and commentary on the launch and flight sequences. It will end when the Dragon spacecraft separates -
Orbital Lifetime Predictions
Orbital LIFETIME PREDICTIONS An ASSESSMENT OF model-based BALLISTIC COEFfiCIENT ESTIMATIONS AND ADJUSTMENT FOR TEMPORAL DRAG co- EFfiCIENT VARIATIONS M.R. HaneVEER MSc Thesis Aerospace Engineering Orbital lifetime predictions An assessment of model-based ballistic coecient estimations and adjustment for temporal drag coecient variations by M.R. Haneveer to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Thursday June 1, 2017 at 14:00 PM. Student number: 4077334 Project duration: September 1, 2016 – June 1, 2017 Thesis committee: Dr. ir. E. N. Doornbos, TU Delft, supervisor Dr. ir. E. J. O. Schrama, TU Delft ir. K. J. Cowan MBA TU Delft An electronic version of this thesis is available at http://repository.tudelft.nl/. Summary Objects in Low Earth Orbit (LEO) experience low levels of drag due to the interaction with the outer layers of Earth’s atmosphere. The atmospheric drag reduces the velocity of the object, resulting in a gradual decrease in altitude. With each decayed kilometer the object enters denser portions of the atmosphere accelerating the orbit decay until eventually the object cannot sustain a stable orbit anymore and either crashes onto Earth’s surface or burns up in its atmosphere. The capability of predicting the time an object stays in orbit, whether that object is space junk or a satellite, allows for an estimate of its orbital lifetime - an estimate satellite op- erators work with to schedule science missions and commercial services, as well as use to prove compliance with international agreements stating no passively controlled object is to orbit in LEO longer than 25 years. -
Nanoracks External Platform (NREP) Interface Definition Document (IDD)
NanoRacks External Platform (NREP) Interface Definition Document (IDD) Doc No: NR-NREP-S0001 Revision: B © Copyright NanoRacks, LLC 2016. All Rights Reserved. NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B NanoRacks External Platform (NREP) IDD NREP Prepared by Steven Stenzel; Systems Engineer; Date Reviewed by Mark Rowley; Mechanical Design; Date Reviewed by Keith Tran; Operations Manager; Date Reviewed by Troy Guy; Avionics Manager; Date Reviewed by Bob Alexander; Safety; Date Reviewed by Susan Lufkin; Systems Engineer; Date Reviewed by Kirk Woellert; Payload Coordinator; Date Approved by Mike Lewis; Chief Technology Officer; Date NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B List of Revisions Revision Revision Date Revised By Revision Description - 3/16/2016 Steve Stenzel Initial Release A 4/20/2016 Steve Stenzel Update logo on cover page B 11/14/2016 C. Cummins Replace Proprietary Statement with a Copyright statement. NanoRacks External Platform IDD NREP Doc No: NR-NREP-S0001 Rev: B Table of Contents 1 Introduction 1 1.1 Purpose 1 1.2 Scope 1 1.3 Use 1 1.4 Exceptions 1 2 Acronyms, Definitions and Applicable Documents 2 3 NanoRacks NREP Overview 4 3.1 NREP Physical Descriptions 4 3.1.1 NREP-P Baseplate 4 3.1.2 NanoRacks External Plate - Payload 5 3.1.3 NREP Coordinate System 5 3.1.4 NREP General Dimensions 6 3.1.5 NREP Payload Configurations 6 3.1.6 NREP Baseplate Location Numbering System 7 3.2 NREP Operations Overview 10 3.2.1 Schedule 10 3.2.2 Ground Operations 11 3.2.2.1 Delivery to NanoRacks -
Spacex CRS-4 National Aeronautics and Fourth Commercial Resupply Services Flight Space Administration
SpaceX CRS-4 National Aeronautics and Fourth Commercial Resupply Services Flight Space Administration to the International Space Station September 2014 OVERVIEW The Dragon spacecraft will be filled with more than 5,000 pounds of supplies and payloads, including critical materials to support 255 science and research investigations that will occur during Expeditions 41 and 42. Dragon will carry three powered cargo payloads in its pressurized section and two in its unpressurized trunk. Science payloads will enable model organism research using rodents, fruit flies and plants. A special science payload is the ISS-Rapid Scatterometer to monitor ocean surface wind speed and direction. Several new technology demonstrations aboard will enable bone density studies, test how a small satellite moves and positions itself in space using new thruster technology, and use the first 3-D printer in space for additive manufacturing. The mission also delivers IMAX cameras for filming during four increments and replacement batteries for the spacesuits. After four weeks at the space station, the spacecraft will return with about 3,800 pounds of cargo, including crew supplies, hardware and computer resources, science experiments, space station hardware, and four powered payloads. DRAGON CARGO LAUNCH ITEMS RETURN ITEMS TOTAL CARGO: 4885 lbs / 2216 kg 3276 lbs / 1486 kg · Crew Supplies 1380 lbs / 626 kg 132 lbs / 60 kg Crew care packages Crew provisions Food · Vehicle Hardware 403 lbs / 183 kg 937 lbs / 425 kg Crew Health Care System hardware Environment Control & Life Support equipment Electrical Power System hardware Extravehicular Robotics equipment Flight Crew Equipment Japan Aerospace Exploration Agency equipment · Science Investigations 1644 lbs / 746 kg 2075 lbs / 941 kg U.S. -
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. -
Mission Overview
CRS Orb-1 Mission Mission Overview Overview Under the Commercial Resupply Services (CRS) contract with NASA, Orbital will provide approximately 20 metric tons of cargo to the International Space Station over the course of eight missions. Orb-1 is the first of those missions. The Orb-1 mission builds on the successful Commercial Orbital Transportation Services (COTS) demonstration mission conducted from September 18 to October 23, 2013. The Orb-1 flight will carry substantially more cargo (1465 kg vs. 700 kg) than the COTS mission, including several time-sensitive payloads and Cygnus’ first powered payload, the Commercial Generic Bioprocessing Apparatus (CGBA) from Bioserve. Mission Overview, Cont. Antares® The configuration of the Antares launch vehicle for the Orb-1 Mission is much the same as the two previous Antares flights with a CASTOR 30B second stage motor instead of the CASTOR 30 used previously. The first stage includes a core that contains the tanks for the liquid oxygen and kerosene, the first stage avionics, and two AJ26 rocket engines. The second stage consists of the CASTOR® 30B solid rocket motor, an avionics section containing the flight computer and guidance/ navigation/control functions, an interstage that connects the solid rocket motor to the first stage, the Cygnus spacecraft, and a fairing that encloses and protects the Cygnus spacecraft during ascent. Continued on Next Page Mission Overview, Cont. Cygnus™ The Cygnus spacecraft is composed of two elements, the Service Module (SM) and the Pressurized Cargo Module (PCM). The SM provides the propulsion, power, guidance, navigation and control, and other “housekeeping” services for the duration of the mission. -
Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on Behalf of the Satellite Industry Association1
Spectrum & the Technological Transformation of the Satellite Industry Spectrum and the Technological Transformation of the Satellite Industry Prepared by Strand Consulting on behalf of the Satellite Industry Association1 1 AT&T, a member of SIA, does not necessarily endorse all conclusions of this study. Page 1 of 75 Spectrum & the Technological Transformation of the Satellite Industry 1. Table of Contents 1. Table of Contents ................................................................................................ 1 2. Executive Summary ............................................................................................. 4 2.1. What the satellite industry does for the U.S. today ............................................... 4 2.2. What the satellite industry offers going forward ................................................... 4 2.3. Innovation in the satellite industry ........................................................................ 5 3. Introduction ......................................................................................................... 7 3.1. Overview .................................................................................................................. 7 3.2. Spectrum Basics ...................................................................................................... 8 3.3. Satellite Industry Segments .................................................................................... 9 3.3.1. Satellite Communications .............................................................................. -
NANORACKS, LLC 555 Forge River Rd., Suite 120 Webster, TX 77598 4369 Phone: 832-632-7754 Fax: 832-575-4767
NANORACKS, LLC 555 Forge River Rd., Suite 120 Webster, TX 77598 4369 Phone: 832-632-7754 Fax: 832-575-4767 www.nanoracks.com Contract Administrator: Christopher Cummins Email Address: [email protected] Business Size: Small For more information on ordering from Federal Supply Schedules click on the FSS Schedules button at fss.gsa.gov. TABLE OF CONTENTS COMPANY OVERVIEW ...............................................................................................................3 CUSTOMER INFORMATION .......................................................................................................5 GSA PRICELIST .............................................................................................................................8 SERVICE DESCRIPTIONS ..........................................................................................................13 NanoRacks, LLC 47QRAA18D004R 2 About NanoRacks NanoRacks was founded on the vision of building a business ecosystem in space. Our company has been integrating customer payloads for the International Space Station since our first launch in 2010. As of February 2018, we have integrated and operated over 600 payloads on 32 launches to the Space Station, including Shuttle, Antares/Cygnus, Atlas V/Cygnus, Falcon/Dragon, HTV, ATV, and Soyuz. To date, we have also deployed over 200 satellites into low-Earth orbit. NanoRacks comes with a team that has real hands on experience with payloads ranging from professional grade research to DOD to high school experiments. NanoRacks -
Nanoracks Completes First Mission on India's Polar Satellite Launch
NanoRacks Completes First Mission on India’s Polar Satellite Launch Vehicle, Launches Spire’s 100th Satellite NanoRacks, the world’s leading commercial space station company, completed its first CubeSat deployment mission on India Space Research Organization’s (ISROs) Polar Satellite Launch Vehicle (PSLV). This mission was brokered on behalf of Spire, which now has four more of their LEMUR 3U CubeSats in orbit. Notably, this mission included the launch of Spire’s 100th Lemur satellite. “Congratulations to Spire on this incredible achievement,” says NanoRacks Payloads Director, Conor Brown. “Spire has been with us from the beginning, not just as a customer but as a partner, working alongside us to pioneer new capabilities across platforms on the Space Station, Cygnus, and now finally on the PSLV. Spire’s diversified launch approach and willingness to embrace new technologies continues to foster the marketplace and we couldn’t be more excited to have deployed the 100th satellite!” NanoRacks announced sun synchronous polar orbit launch opportunities after receiving significant customer demand and strong feedback for the customer support that the Company offers. Polar orbit offerings come in addition to NanoRacks’ proven success in small satellite deployments, having deployed over 230 satellites to date. Spire’s CubeSats offer data and analytics for parts of the world where collecting data is notoriously difficult, tracking ships, planes, and weather in remote regions which often go unmonitored. To date, of the 100 satellites Spire has launched, 37 were on NanoRacks missions from the Space Station, the Cygnus Spacecraft, and now PSLV. “Spire is excited to share this milestone with NanoRacks,” says Jenny Barna, Spire’s Director of Launch. -
Study of Future Perspectives of Micro/Nanosatellites Constellations in the Earth Observation Market
Study of future perspectives of Micro/Nano-satellites constellations in the Earth Observation market Master’s thesis Master’s Degree in Aeronautical Engineering ANNEX Mariona Costa Rabionet June 2019 Supervisor of the TFM: Miquel Sureda Anfres Co-Supervisor of TFM: Silvia Rodríguez Donaire Study of future perspectives of micro/nanosatellites constellations in the Earth Observation market Content ANNEX 1: New Space companies .................................................................................................. 3 ANNEX 2: Flock satellites status. ................................................................................................. 11 ANNEX 3: TLE number of Flock constellation satellites .............................................................. 31 ANNEX 4: Flock satellites orbital parameters. ............................................................................ 42 ANNEX 4: SaVi configuration ....................................................................................................... 56 Bibliography ................................................................................................................................ 65 2 Study of future perspectives of micro/nanosatellites constellations in the Earth Observation market ANNEX 1: New Space companies In this annex, it can be found the list of New space companies that has been analysed to be included in the qualitative analysis (table 1). Table 1. New space companies[1] Planned Organization Launched First launch Form factor Field Technical -
The Impact of New Trends in Satellite Launches on Orbital Debris Environment
THE IMPACT OF NEW TRENDS IN SATELLITE LAUNCHES ON ORBITAL DEBRIS ENVIRONMENT Arif Göktuğ Karacalıoğlu STC / NASA Ames Research Center, United States, [email protected] Jan Stupl SGT / NASA Ames Research Center, United States The main goal of this study is to examine the impact of new trends in satellite launch activities on the orbital debris environment and collision risk. Starting from the launch of the first artificial satellite in 1957, space borne technology has become an indispensable part of our lives. More than 6,000 satellites have been launched into Earth orbit. Though the annual number of satellites launched stayed flat for many decades, the trend has recently changed. The satellite market has been undergoing a major evolution with new space companies replacing the traditional approach of deploying a few large, complex and costly satellites with an approach to use a multitude of smaller, less complex and cheaper satellites. This new approach creates a sharp increase in the number of satellites and so the historic trends are no longer representative. As a foundation for this study, a scenario for satellite deployments based on publicly announced future satellite missions has been developed. These constellation-deploying companies include, but are not limited to, Blacksky, CICERO, EROS, Landmapper, Leosat, Northstar, O3b, OmniEarth, OneWeb, Orbcomm, OuterNet, PlanetIQ, Planet Labs, Radarsat, RapidEye Next Generation, Sentinel, Skybox, SpaceX, and Spire. Information such as the annual number of launches, the number of orbital planes to be used by the constellation, as well as apogee, perigee, inclination, spacecraft mass and area were included or approximated. -
Cubesat-Services.Pdf
Space• Space Station Station Cubesat CubesatDeployment Services Deployment Services NanoRacks Cubesat Deployer (NRCSD) • 51.6 degree inclination, 385-400 KM • Orbit lifetime 8-12 months • Deployment typically 1-3 months after berthing • Soft stowage internal ride several times per year Photo credit: NASA NRCSD • Each NRCSD can deploy up to 6U of CubeSats • 8 NRCSD’s per airlock cycle, for a total of 48U deployment capability • ~2 Air Lock cycles per mission Photo Credit: NanoRacks LLC Photo credit: NASA 2. Launched by ISS visiting vehicle 3. NRCSDs installed by ISS Crew 5. Grapple by JRMS 4. JEM Air Lock depress & slide 6. NRCSDs positioned by JRMS table extension 1. NRCSDs transported in CTBs 7. Deploy 8. JRMS return NRCSD-MPEP stack to slide table; 9. ISS Crew un-install first 8 NRCSDs; repeat Slide table retracts and pressurizes JEM air lock install/deploy for second set of NRCSDs NanoRacks Cubesat Mission (NR-CM 3 ) • Orbital Sciences CRS-1 (Launched Jan. 9, 2014) • Planet Labs Flock1A, 28 Doves • Lithuanian Space Assoc., LitSat-1 • Vilnius University & NPO IEP, LituanicaSat-1 • Nanosatisfi, ArduSat-2 • Southern Stars, SkyCube • University of Peru, UAPSat-1 Photo credit: NASA Mission Highlights Most CubeSats launched Two countries attain in a single mission space-faring status World’s largest remote Kickstarter funding sensing constellation • NR-CM3 • Orbital Science CRS-1, Launch Jan 9, 2014 • Air Lock Cycle 1, Feb 11-15, 2014 Dove CubeSats • Deployers 1-8 (all Planet Labs Doves) Photo credit: NASA • NR-CM3 • Orbital Science CRS-1,