Falcon 9 Rocket and Dragon Spacecraft, and Commentary on the Launch and Flight Sequences
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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 -
China's Touch on the Moon
commentary China’s touch on the Moon Long Xiao As well as being a milestone in technology, the Chang’e lunar exploration programme establishes China as a contributor to space science. With much still to learn about the Moon, fieldwork beyond Earth’s orbit must be an international effort. hen China’s Chang’e 3 spacecraft geological history of the landing site. touched down on the lunar High-resolution images have shown rocky Wsurface on 14 December 2013, terrain with outcrops of porphyritic basalt, it was the first soft landing on the Moon such as Loong Rock (Fig. 2). Analysis since the Soviet Union’s Luna 24 mission of data collected by the penetrating in 1976. Following on from the decades- Chang’e 3 radar should lead to identification of the old triumphs of the Luna missions and underlying layers of regolith, impact breccia NASA’s Apollo programme, the Chang’e and basalt. lunar exploration programme is leading the China’s robotic field geologist Yutu has charge of a new generation of exploration Basalt outcrop Yutu rover stalled in its traverse of the lunar surface, on the lunar surface. Much like the earlier but plans for the Chang’e 5 sample-return space programmes, the China National mission are moving forward. The primary Space Administration (CNSA) has been objective of the mission will be to return developing its capabilities and technologies 100 m 2 kg of samples from the surface and depths step by step in a series of Chang’e missions UNIVERSITY STATE © NASA/GSFC/ARIZONA of up to 2 m, probably also in the relatively of increasing ambition: orbiting and Figure 1 | The Chinese Chang’e 3 spacecraft and smooth northern Mare Imbrium. -
One Small Step for the EPA, One Giant Leap for the Environment: a Hybrid Proposal for Regulating Rocket Emissions Due to the Rising Commercial Space Industry
NOTES One Small Step for the EPA, One Giant Leap for the Environment: A Hybrid Proposal for Regulating Rocket Emissions Due to the Rising Commercial Space Industry Ashima Talwar* I. Introduction As the industry matures and costs decrease, satellite launches and space tourism will likely become commonplace. When asked what they want to be when they grow up, kids Scientists predict that these aggregated rocket emissions often respond, “An astronaut! I want to go to space!” But this could significantly exacerbate changes to the climate and the generation of children may not need to become astronauts ozone layer.3 Neither Congress nor the U.S. Environmental to go to space—the commercial space industry is rapidly on Protection Agency (“EPA”) has yet addressed this concern the rise. through legislation or regulation. However, in a policy deter- Along with the excitement at the prospect of space explo- mination letter, the EPA categorized rocket launching as a ration, tourism, and commercial enterprise, however, comes mobile source activity rather than a stationary source activity a new set of problems for the environmental and legal com- under the Clean Air Act (“CAA”), absolving a space com- munities to solve. One such difficulty this boon of progress pany of potential permitting requirements.4 This conclusion will pose is the emissions of air pollutants. Simply watch- provided the EPA less oversight over the company’s emissions ing a rocket lift off, with billows of black smoke gathering and lowered the company’s administrative burden. Although ominously below, should concern any environmentalist. the EPA’s decision is based on sound logic, it requires clarifi- Some experts have noted the relatively low environmental cation so that the burgeoning commercial space industry has cost attributed to rocket launches, based on certain exhaust certainty in how it can expect to be regulated in the future. -
Space Reporter's Handbook Mission Supplement
CBS News Space Reporter's Handbook - Mission Supplement Page 1 The CBS News Space Reporter's Handbook Mission Supplement Shuttle Mission STS-125: Hubble Space Telescope Servicing Mission 4 Written and Produced By William G. Harwood CBS News Space Analyst [email protected] CBS News 5/10/09 Page 2 CBS News Space Reporter's Handbook - Mission Supplement Revision History Editor's Note Mission-specific sections of the Space Reporter's Handbook are posted as flight data becomes available. Readers should check the CBS News "Space Place" web site in the weeks before a launch to download the latest edition: http://www.cbsnews.com/network/news/space/current.html DATE RELEASE NOTES 08/03/08 Initial STS-125 release 04/11/09 Updating to reflect may 12 launch; revised flight plan 04/15/09 Adding EVA breakdown; walkthrough 04/23/09 Updating for 5/11 launch target date 04/30/09 Adding STS-400 details from FRR briefing 05/04/09 Adding trajectory data; abort boundaries; STS-400 launch windows Introduction This document is an outgrowth of my original UPI Space Reporter's Handbook, prepared prior to STS-26 for United Press International and updated for several flights thereafter due to popular demand. The current version is prepared for CBS News. As with the original, the goal here is to provide useful information on U.S. and Russian space flights so reporters and producers will not be forced to rely on government or industry public affairs officers at times when it might be difficult to get timely responses. All of these data are available elsewhere, of course, but not necessarily in one place. -
IAC-17-D2.4.3 Page 1 of 18 IAC-17
68th International Astronautical Congress (IAC), Adelaide, Australia, 25-29 September 2017. Copyright ©2017 by DLR-SART. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-17- D2.4.3 Evaluation of Future Ariane Reusable VTOL Booster stages Etienne Dumonta*, Sven Stapperta, Tobias Eckerb, Jascha Wilkena, Sebastian Karlb, Sven Krummena, Martin Sippela a Department of Space Launcher Systems Analysis (SART), Institute of Space Systems, German Aerospace Center (DLR), Robert Hooke Straße 7, 28359 Bremen, Germany b Department of Spacecraft, Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Bunsenstraße 10, 37073 Gottingen, Germany *[email protected] Abstract Reusability is anticipated to strongly impact the launch service market if sufficient reliability and low refurbishment costs can be achieved. DLR is performing an extensive study on return methods for a reusable booster stage for a future launch vehicle. The present study focuses on the vertical take-off and vertical landing (VTOL) method. First, a restitution of a flight of Falcon 9 is presented in order to assess the accuracy of the tools used. Then, the preliminary designs of different variants of a future Ariane launch vehicle with a reusable VTOL booster stage are described. The proposed launch vehicle is capable of launching a seven ton satellite into a geostationary transfer orbit (GTO) from the European spaceport in Kourou. Different stagings and propellants (LOx/LH2, LOx/LCH4, LOx/LC3H8, subcooled LOx/LCH4) are considered, evaluated and compared. First sizing of a broad range of launcher versions are based on structural index derived from existing stages. -
Competition and Efficiency in the U.S. Launch Vehicle Market to What Extent Has the U.S
Competition and Efficiency in the U.S. Launch Vehicle Market To what extent has the U.S. launch vehicle market become more allocatively and productively efficient as a result of increased competition? 1 Table of Contents Introduction................................................................................................................................................3 Definitions & Guidelines......................................................................................................................3 Method..................................................................................................................................................4 Analysis......................................................................................................................................................7 The state of the market in 2013.............................................................................................................7 Changes from 2013 to 2018................................................................................................................10 The Decline of Cost-Plus................................................................................................................10 Economies of Scale & Vertical Integration....................................................................................12 Restructuring of companies............................................................................................................15 The expansion of SpaceX and overall increase -
March 29, 2021 Ms. Lisa Felice Executive Secretary Michigan
8 8 KARL L. GOTTING PAULA K. MANIS PLLC JACK C. DAVIS MICHAEL G. OLIVA JAMES R. NEAL JEFFREY L. GREEN8 (1938-2020) [email protected] 8 MICHAEL G. OLIVA KELLY REED LUCAS DIRECT DIAL: 517-318-9266 8 MICHAEL H. RHODES RICHARD W. PENNINGS NOTES: MOBILE: 989-798-2650 EFFREY HEUER1 ICHAEL OLMES8 ______________________ J S. T M A. H 1 KEVIN J. RORAGEN YING BEHER8 ALSO LICENSED IN MD 2 REPLY TO LANSING OFFICE ED OZEBOOM ARREN EAN5,8 ALSO LICENSED IN FL T S. R W T. D 3 7,8 ALSO LICENSED IN CT SARA L. CUNNINGHAM JACK L. HOFFMAN 4 2 7,8 ALSO LICENSED IN NY JAMES F. ANDERTON, V HOLLY L. JACKSON 5 ALSO LICENSED IN OH 6 DOMINIC R. RIOS ALSO LICENSED BY USPTO 3,4,6 MIKHAIL MURSHAK 7 GRAND RAPIDS OFFICE GABRIELLE C. LAWRENCE 8 OF COUNSEL ALAN G. ABOONA6 AMIA A. BANKS HANNAH E. BUZOLITS March 29, 2021 Ms. Lisa Felice Executive Secretary Michigan Public Service Commission 7109 W. Saginaw Highway Lansing, MI 48917 Re: Starlink Services, LLC Application for CLEC License MPSC Case No U-21035 Dear Ms. Felice: Enclosed for filing on behalf of Starlink Services, LLC please find: • Application Of Starlink Services, LLC For A Temporary And Permanent License To Provide Basic Local Exchange Service In Michigan • Prefiled Testimony of Matt Johnson • Exhibits SLS-1, SLS-2, SLS-3 and Confidential Exhibit SLS-4 Confidential Exhibit SLS-4 is not being filed electronically, but a sealed copy of Confidential Exhibit SLS-4 is being delivered via overnight mail to the Commission’s offices. -
Thermal Design, Analysis and Test Validation of Turksat-3Usat Satellite
Journal of Thermal Engineering, Vol. 7, No. 3, pp. 468-482, March, 2021 Yildiz Technical University Press, Istanbul, Turkey THERMAL DESIGN, ANALYSIS AND TEST VALIDATION OF TURKSAT-3USAT SATELLITE Murat Bulut1,*, Nedim Sözbir2 ABSTRACT When CubeSat projects are a useful means by which universities can engage their students in space-related activities. TURKSAT-3USAT is a three-unit amateur radio CubeSat jointly developed by the Space Systems Design and Test Laboratory and the Radio Frequency Electronics Laboratory of Istanbul Technical University (ITU), in collaboration with TURKSAT, A.S. company as well as the Turkish Amateur Technology Organization. It was launched on April 26, 2013 as a secondary payload on a CZ-2D rocket from China’s Jiuquan Space Center to an altitude of approximately 680 km. The mission of the satellite has two primary goals: (1) to voice communication at Low Earth Orbit (LEO) and (2) to educate students by providing hands-on experience. TURKSAT-3USAT was designed to sustain a circular, near sun-synchronous LEO, and has dimensions of 10 x 10 x 34 cm3. Within the course of this paper, TURKSAT-3USAT’s thermal control will be addressed. TURKSAT-3USAT’s thermal control model was developed using ThermXL and ESATAN-TMS software. Using this model, temperature distributions of the CubeSat when subjected to various experimental conditions of interest were computed. Using a thermal vacuum chamber (TVAC), thermal cycling and bake-out testing were carried out on the flight model to verify the thermal design performance and check the mathematical model. Based on thermal analysis results, the temperature of equipment was within the allowable temperature range except for the batteries that were between 42.56 oC and -20.31 oC. -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
Since Our Last SIA Member News Summary, Press Releases and Posts
SIA PRESIDENT’S REPORT – MEMBER NEWS FOR OCT 2020 Since our last SIA Member News Summary, press releases and posts from many SIA Members including AGI, Blue Origin, Hawkeye 360, Inmarsat, Integrasys, Iridium, Kymeta, Lockheed Martin, OneWeb, Planet, SES, SpaceX, Spire, Telesat and XTAR have released news. Please see the summary of stories and postings below and click on the COMPANY LINK for more details. PLANET (above) On Oct 28th, Planet announced the successful launch of nine Flock 4e latest-generation SuperDove satellites onboard a Rocket Lab Electron rocket from New Zealand. The Flock 4e’ SuperDoves were deployed into an approximately 500 km, morning-crossing Sun Synchronous Orbit (SSO), joining the rest of the constellation providing medium-resolution Earth imagery with unprecedented coverage and frequency of update. The nine SuperDoves are equipped with 8 spectral bands that provide high image quality and accurate surface reflectance values for advanced algorithms and time-series analysis. Planet’s SuperDoves are also interoperable with publicly available imagery, like Copernicus’ Sentinel-2, enabling innovative applications and use cases. (Photo credit: Image courtesy of Planet and Rocket Lab) AGI On Oct 26th, Analytical Graphics Inc., (AGI) announced that AGI and Ansys, a leading innovator of engineering software, had entered into a definitive acquisition agreement. According to the terms of the agreement, Ansys would acquire AGI. The purchase price for the transaction, which is expected to close in Q4 of 2020 pending regulatory clearance, is $700 million. SPACEX On Oct 24th, SpaceX announced that a Falcon 9 rocket had launched 60 Starlink satellites to orbit from Space Launch Complex 40 (SLC-40) at Cape Canaveral Air Force Station in Florida. -
Espinsights the Global Space Activity Monitor
ESPInsights The Global Space Activity Monitor Issue 2 May–June 2019 CONTENTS FOCUS ..................................................................................................................... 1 European industrial leadership at stake ............................................................................ 1 SPACE POLICY AND PROGRAMMES .................................................................................... 2 EUROPE ................................................................................................................. 2 9th EU-ESA Space Council .......................................................................................... 2 Europe’s Martian ambitions take shape ......................................................................... 2 ESA’s advancements on Planetary Defence Systems ........................................................... 2 ESA prepares for rescuing Humans on Moon .................................................................... 3 ESA’s private partnerships ......................................................................................... 3 ESA’s international cooperation with Japan .................................................................... 3 New EU Parliament, new EU European Space Policy? ......................................................... 3 France reflects on its competitiveness and defence posture in space ...................................... 3 Germany joins consortium to support a European reusable rocket......................................... -
Falcon 1 User's Guide
Falcon 1 Launch Vehicle Payload User’s Guide Rev 7 TABLE OF CONTENTS 1. Introduction 4 1.1. Revision History 4 1.2. Purpose 6 1.3. Company Description 6 1.4. Falcon Program Overview 6 1.5. Mission Management 7 2. Falcon 1 Launch Vehicles 8 2.1. Overview 8 2.1.1. Falcon 1 9 2.1.2. Falcon 1e 11 2.2. Availability 12 2.3. Reliability 13 2.4. Performance 15 2.5. Pricing 16 2.6. Standard Services 16 2.7. Non‐standard Services 16 2.8. Vehicle Axes/Attitude Definitions 17 3. Requirements & Environments 18 3.1. Mass Properties 18 3.2. Payload Interfaces 19 3.2.1. Falcon Payload Attach Fittings 19 3.2.2. Test Fittings and Fitcheck Policy 19 3.2.3. Electrical Design Criteria 19 3.3. Documentation Requirements 21 3.4. Payload Environments 23 3.4.1. Transportation Environments 23 3.4.2. Humidity, Cleanliness and Thermal Control 23 3.4.3. Payload Air Conditioning 24 3.4.4. Launch and Flight Environments 24 4. Facilities 32 4.1. Headquarters – Hawthorne, California 32 4.2. Washington, DC 32 4.3. Test Facility ‐ Central Texas 32 4.4. Launch Site – Kwajalein Atoll 33 4.4.1. Processing Services and Equipment 33 5. Launch Operations 36 5.1. Launch Control Organization 36 5.2. Mission Integration 37 5.2.1. Payload Transport to Launch Site 38 5.2.2. Payload Integration 38 5.2.3. Example Flight Profiles 41 D000973 Rev Falcon 1 User’s Guide ‐ D000973 Rev. 7 Page | 3 6.