Evolution of Communications Payload Technologies for Satellites
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The Annual Compendium of Commercial Space Transportation: 2013
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2013 February 2014 About FAA \ NOTICE ###i# £\£\ ###ii# Table of Contents TABLE OF CONTENTS INTRODUCTION. 1 YEAR AT A GLANCE ..............................................2 COMMERCIAL SPACE TRANSPORTATION 2013 YEAR IN REVIEW ........5 7 ORBITAL LAUNCH VEHICLES .....................................21 3 SUBORBITAL REUSABLE VEHICLES ...............................47 33 ON-ORBIT VEHICLES AND PLATFORMS ............................57 LAUNCH SITES .................................................65 COMMERCIAL VENTURES BEYOND EARTH ORBIT ...................79 44 REGULATION AND POLICY .......................................83 3 5 3 53 3 8599: : : ;55: 9 < 5; < 2013 COMMERCIAL SPACE TRANSPORTATION FORECASTS ..........89 4 3 4 : ACRONYMS AND ABBREVIATIONS ...............................186 2013 WORLDWIDE ORBITAL LAUNCH EVENTS .....................192 DEFINITIONS ..................................................196 ###iii# £\£\ LIST OF FIGURES COMMERCIAL SPACE TRANSPORTATION YEAR IN REVIEW = =999 =99 = =3> =:9;> LAUNCH SITES = :< 2013 COMMERCIAL SPACE TRANSPORTATION FORECASTS =944 =4 =?4;9 =99493 =3 =:5= =< =;=9 =95;@3 =A =;=9 A 3 =994?: =9999 ? =54 =359 =:5 3 =<999= ? =99=5 ?3 =;>>99: =99 ? 3 ==9 ? 3: =3 =>3 =?: =3?: =:? : ###iv# LIST OF TABLES COMMERCIAL SPACE TRANSPORTATION YEAR IN REVIEW 99 : 3< :9=99< <99 ORBITAL LAUNCH VEHICLES 99 99 59595 593 SUBORBITAL REUSABLE VEHICLES 3 :5933 ON-ORBIT VEHICLES -
Cubesat Mission: from Design to Operation
applied sciences Article CubeSat Mission: From Design to Operation Cristóbal Nieto-Peroy 1 and M. Reza Emami 1,2,* 1 Onboard Space Systems Group, Department of Computer Science, Electrical and Space Engineering, Luleå University of Technology, Space Campus, 981 92 Kiruna, Sweden 2 Aerospace Mechatronics Group, University of Toronto Institute for Aerospace Studies, Toronto, ON M3H 5T6, Canada * Correspondence: [email protected]; Tel.: +1-416-946-3357 Received: 30 June 2019; Accepted: 29 July 2019; Published: 1 August 2019 Featured Application: Design, fabrication, testing, launch and operation of a particular CubeSat are detailed, as a reference for prospective developers of CubeSat missions. Abstract: The current success rate of CubeSat missions, particularly for first-time developers, may discourage non-profit organizations to start new projects. CubeSat development teams may not be able to dedicate the resources that are necessary to maintain Quality Assurance as it is performed for the reliable conventional satellite projects. This paper discusses the structured life-cycle of a CubeSat project, using as a reference the authors’ recent experience of developing and operating a 2U CubeSat, called qbee50-LTU-OC, as part of the QB50 mission. This paper also provides a critique of some of the current poor practices and methodologies while carrying out CubeSat projects. Keywords: CubeSat; miniaturized satellite; nanosatellite; small satellite development 1. Introduction There have been nearly 1000 CubeSats launched to the orbit since the inception of the concept in 2000 [1]. An up-to-date statistics of CubeSat missions can be found in Reference [2]. A summary of CubeSat missions up to 2016 can also be found in Reference [3]. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
Spacex's Expanding Launch Manifest
October 2013 SpaceX’s expanding launch manifest China’s growing military might Servicing satellites in space A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS SpaceX’s expanding launch manifest IT IS HARD TO FIND ANOTHER SPACE One of Brazil, and the Turkmensat 1 2012, the space docking feat had been launch services company with as di- for the Ministry of Communications of performed only by governments—the verse a customer base as Space Explo- Turkmenistan. U.S., Russia, and China. ration Technologies (SpaceX), because The SpaceX docking debunked there simply is none. No other com- A new market the myth that has prevailed since the pany even comes close. Founded only The move to begin launching to GEO launch of Sputnik in 1957, that space a dozen years ago by Elon Musk, is significant, because it opens up an travel can be undertaken only by na- SpaceX has managed to win launch entirely new and potentially lucrative tional governments because of the contracts from agencies, companies, market for SpaceX. It also puts the prohibitive costs and technological consortiums, laboratories, and univer- company into direct competition with challenges involved. sities in the U.S., Argentina, Brazil, commercial launch heavy hitters Ari- Teal Group believes it is that Canada, China, Germany, Malaysia, anespace of Europe with its Ariane mythology that has helped discourage Mexico, Peru, Taiwan, Thailand, Turk- 5ECA, U.S.-Russian joint venture Inter- more private investment in commercial menistan, and the Netherlands in a rel- national Launch Services with its Pro- spaceflight and the more robust growth atively short period. -
Increasing Launch Rate and Payload Capabilities
Aerial Launch Vehicles: Increasing Launch Rate and Payload Capabilities Yves Tscheuschner1 and Alec B. Devereaux2 University of Colorado, Boulder, Colorado Two of man's greatest achievements have been the first flight at Kitty Hawk and pushing into the final frontier that is space. Air launch systems aim to combine these great achievements into a revolutionary way to deliver satellites, cargo and eventually people into space. Launching from an aircraft has many advantages, including the ability to launch at any inclination and from above bad weather, which could delay ground launches. While many concepts for launching rockets from an airplane have been developed, very few have made it past the drawing board. Only the Pegasus and, to a lesser extent, SpaceShipOne have truly shown the feasibility of such a system. However, a recent push for rapid, small payload to orbit launches by the military and a general need for cheaper, heavy lift options are leading to an increasing interest in air launch methods. In order for the efficiency and flexibility of the system to be realized, however, additional funding and research are necessary. Nomenclature ALASA = airborne launch assist space access ALS = air launch system DARPA = defense advanced research project agency LEO = low Earth orbit LOX = liquid oxygen RP-1 = rocket propellant 1 MAKS = Russian air launch system MECO = main engine cutoff SS1 = space ship one SS2 = space ship two I. Introduction W hat typically comes to mind when considering launching people or satellites to space are the towering rocket poised on the launch pad. These images are engraved in the minds of both the public and scientists alike. -
Paper Session II-B-National Launch System Payload Accommodations
The Space Congress® Proceedings 1992 (29th) Space - Quest For New Fontiers Apr 22nd, 2:00 PM Paper Session II-B - National Launch System Payload Accommodations Capt James M. Knauf National Launch System Requirements Officer HQ Airor F ce Space Command Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Knauf, Capt James M., "Paper Session II-B - National Launch System Payload Accommodations" (1992). The Space Congress® Proceedings. 15. https://commons.erau.edu/space-congress-proceedings/proceedings-1992-29th/april-22-1992/15 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. NATIONAL LAUNCH SYSTEM PAYLOAD ACCOMMODATIONS Capt James M. Knauf National Launch System Requirements Officer HQ Air Force Space Command - Peterson AFB, CO ABSTRACT Early definition, documentation, acceptance, and continuing implementation of a standard system of payload accommodations for space launch systems is essential. Attempts to provide truly standard payload accommodations have not met with significant success in increasing responsiveness or reducing operations costs. The operational philosophy of the National Launch System (NLS) is based on standardization and includes standardized payload accommodations. These must be incorporated into NLS design concepts early in the development phase to ensure the NLS goal of increased responsiveness and reduced operating cost. At the same time, sufficient flexibility will be maintained to accommodate the rare unique payload requirement which cannot meet the standard due to specific mission requirements, safety concerns, or other reasons. -
List of Satellite Missions (By Year and Sponsoring
Launch Year EO Satellite Mission (and sponsoring agency) 2008 CARTOSAT-2A (ISRO) 1967 Diademe 1&2 (CNES) 2008 FY-3A (NSMC-CMA / NRSCC) 1975 STARLETTE (CNES) 2008 OSTM (Jason-2) (NASA / NOAA / CNES / EUMETSAT) 1976 LAGEOS-1 (NASA / ASI) 2008 RapidEye (DLR) 1992 LAGEOS-2 (ASI / NASA) 2008 HJ-1A (CRESDA / CAST) 1993 SCD-1 (INPE) 2008 HJ-1B (CRESDA / CAST) 1993 STELLA (CNES) 2008 THEOS (GISTDA) 1997 DMSP F-14 (NOAA / USAF) 2008 COSMO-SkyMed 3 (ASI / MoD (Italy)) 1997 Meteosat-7 (EUMETSAT / ESA) 2008 FY-2E (NSMC-CMA / NRSCC) 1997 TRMM (NASA / JAXA) 2009 GOSAT (JAXA / MOE (Japan) / NIES (Japan)) 1998 NOAA-15 (NOAA) 2009 NOAA-19 (NOAA) 1998 SCD-2 (INPE) 2009 RISAT-2 (ISRO) 1999 Landsat 7 (USGS / NASA) 2009 GOES-14 (NOAA) 1999 QuikSCAT (NASA) 2009 UK-DMC2 (UKSA) 1999 Ikonos-2 2009 Deimos-1 1999 Ørsted (Oersted) (DNSC / CNES) 2009 Meteor-M N1 (ROSHYDROMET / ROSKOSMOS) 1999 DMSP F-15 (NOAA / USAF) 2009 OCEANSAT-2 (ISRO) 1999 Terra (NASA / METI / CSA) 2009 DMSP F-18 (NOAA / USAF) 1999 ACRIMSAT (NASA) 2009 SMOS (ESA / CDTI / CNES) 2000 NMP EO-1 (NASA) 2010 GOES-15 (NOAA) 2001 Odin (SNSB / TEKES / CNES / CSA) 2010 CryoSat-2 (ESA) 2001 QuickBird-2 2010 TanDEM-X (DLR) 2001 PROBA (ESA) 2010 COMS (KARI) 2002 GRACE (NASA / DLR) 2010 AISSat-1 (NSC) 2002 Aqua (NASA / JAXA / INPE) 2010 CARTOSAT-2B (ISRO) 2002 SPOT-5 (CNES) 2010 FY-3B (NSMC-CMA / NRSCC) 2002 Meteosat-8 (EUMETSAT / ESA) 2010 COSMO-SkyMed 4 (ASI / MoD (Italy)) 2002 KALPANA-1 (ISRO) 2011 Elektro-L N1 (ROSKOSMOS / ROSHYDROMET) 2003 CORIOLIS (DoD (USA)) 2011 RESOURCESAT-2 (ISRO) 2003 SORCE (NASA) -
Integrated Spacecraft/Payload Element Fact Sheet
National Aeronautics and Space Administration Space Launch System Integrated Spacecraft/ Payload Element NASA’s Space Launch System (SLS) will pro- vide the agency with super heavy-lift capability to return astronauts to the Moon and launch payloads to the Moon or deeper into the solar system. The integrated spacecraft/payload element for the initial SLS configuration, called Block 1, consists of the upper stage and payload section facts of the rocket, above the core stage, including adapters and separation systems. In the SLS Block 1 crew configuration, the inte- grated spacecraft/payload element connects the core stage to the Orion crew vehicle. In the Block 1 cargo variant, the integrated spacecraft/ payload element sits at the top of the vehicle, above the core stage, and includes a 5 meter- diameter payload fairing that encapsulates the payload. NASA is building the super heavy-lift SLS rocket to send astronauts in Orion to the Moon and NASA to launch cargo and scientific payloads to the Moon or deep into the solar system. Block 1 is the initial launcher, with progressively more powerful vehicles planned for the future to SLS Block 1 will be used for NASA’s first Artemis enable NASA to establish a sustainable pres- missions. The initial flight, Artemis I, is a test of ence at the Moon before sending humans to the new system – including Orion and ground sys- Mars. tems at Kennedy Space Center – and will include deployment of 13 CubeSats. The integrated spacecraft/payload element on the Block 1 crew vehicle is comprised of the In- The next flight, Artemis II, is a lunar flyby mission terim Cryogenic Propulsion Stage (ICPS), which that will make astronauts in Orion the record- provides in-space propulsion, the Launch Ve- holders for farthest distance humans have trav- hicle Stage Adapter (LVSA), and the Orion Stage eled from Earth. -
Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid
Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid Rocket Engines by DAVID PHILLIP RUSS S.B., Massachusetts Institute of Technology 1987 SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN AERONAUTICS AND ASTRONAUTICS at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY May 1988 ® David P. Russ 1988 The author hereby grants M.I.T. and Hughes Aircraft Company permission to reproduce and to distribute copies of this thesis document in whole or in part. Signature of Author Department of Aeronautics and Astronautics December 18, 1987 Reviewed by C. P. Rubin Hughes Aircraft Company Certified by Professor Walter M. Hollister Thesis Supervjsor, Departmer of Aeronautics and Astronautics .. Accepted by , .AU Professor Harold Y. Wachman Chairman, Depart'rmental Graduate Committee Department of Aeronautics and Astronautics MAY i od ;WITHDRAWfIN i M.I.1W.i..: P. I LBRARt S UBAer 7:Ir_ Aero Analysis of a Heavy Lift Launch Vehicle Design Using Small Liquid Rocket Engines by David P. Russ Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics May, 1988 Abstract The trend in launch vehicle design has been to increase performance by using en- gines of greater and greater complexity, which has a negative effect on cost and reliability. However, a design making use of over 300 small, simple rocket engines can deliver over 340,000 lbs to low Earth orbit. This design, derived by using the rocket equations to size the major components, features a 42 ft. -
Dragon Spacecraft, and Commentary on the Launch and Flight Sequences
SpaceX CRS-3 Mission Press Kit CONTENTS 3 Mission Overview 7 Mission Timeline 9 Graphics – Rendezvous, Grapple and Berthing, Departure and Re-Entry 11 International Space Station Overview 13 Falcon 9 Overview 16 Dragon Overview 18 SpaceX Facilities 20 SpaceX Overview 22 SpaceX Leadership SPACEX MEDIA CONTACT Emily Shanklin Senior Director, Marketing and Communications 310-363-6733 [email protected] NASA PUBLIC AFFAIRS CONTACTS Trent Perrotto Michael Curie Josh Byerly Public Affairs Officer News Chief Public Affairs Officer Human Exploration and Operations Launch Operations International Space Station NASA Headquarters NASA Kennedy Space Center NASA Johnson Space Center 202-358-1100 321-867-2468 281-483-5111 Rachel Kraft George Diller Public Affairs Officer Public Affairs Officer Human Exploration and Operations Launch Operations NASA Headquarters NASA Kennedy Space Center 202-358-1100 321-867-2468 1 HIGH RESOLUTION PHOTOS AND VIDEO SpaceX will post photos and video throughout the mission. High-resolution photographs can be downloaded from: spacex.com/media Broadcast quality video can be downloaded from: vimeo.com/spacexlaunch/ MORE RESOURCES ON THE WEB For SpaceX coverage, visit: For NASA coverage, visit: spacex.com www.nasa.gov/station twitter.com/elonmusk www.nasa.gov/nasatv twitter.com/spacex twitter.com/nasa facebook.com/spacex facebook.com/ISS plus.google.com/+SpaceX plus.google.com/+NASA youtube.com/spacex youtube.com/nasatelevision WEBCAST INFORMATION The launch will be webcast live, with commentary from SpaceX corporate headquarters in Hawthorne, CA, at spacex.com/webcast and NASA’s Kennedy Space Center at www.nasa.gov/nasatv. Web pre-launch coverage will begin at approximately 3:00 a.m. -
Table 21 Page4
2008 Commercial Space Transportation Forecasts About the Office of Commercial Space Transportation and the Commercial Space Transportation Advisory Committee The Federal Aviation Administration’s The primary goals of COMSTAC are to: Office of Commercial Space Transportation (FAA/AST) licenses and regulates U.S. • Evaluate economic, technological and commercial space launch and reentry activity institutional issues relating to the U.S. as authorized by Executive Order 12465 commercial space transportation (Commercial Expendable Launch Vehicle industry; Activities) and 49 United States Code Subtitle IX, Chapter 701 (formerly the Commercial • Provide a forum for the discussion of issues Space Launch Act). AST’s mission is to license involving the relationship between industry and regulate commercial launch and reentry and government requirements; and operations to protect public health and safety, the safety of property, and the national security • Make recommendations to the Administrator and foreign policy interests of the United States. on issues and approaches for Federal Chapter 701 and the 2004 U.S. Space policies and programs regarding the Transportation Policy also direct the Federal industry. Aviation Administration to encourage, facilitate, and promote commercial launches and reentries. Additional information concerning AST and COMSTAC can be found on AST’s web site, The Commercial Space Transportation Advisory http://ast.faa.gov. Committee (COMSTAC) provides information, advice, and recommendations to the Administrator of the Federal Aviation Administration within the Department of Transportation (DOT) on matters relating to the U.S. commercial space transportation industry. Established in 1985, COMSTAC is made up of senior executives from the U.S. commercial space transportation and satellite industries, space-related state government officials, and other space professionals. -
Diapositive 1
PROSPECTS FOR THE SMALL SATELLITE MARKET 4th edition A GLOBAL SUPPLY & DEMAND ANALYSIS OF GOVERNMENT & COMMERCIAL SATELLITES UP TO 500 KG – AN EXTRACT A Euroconsult Executive Report - 2018 PROSPECTS FOR THE SMALL SATELLITE MARKET // AN EXTRACT © Euroconsult 2018 – Approved for public release WHO WE ARE / WHAT WE DO TRAINING PROSPECTS FOR THE SMALL SATELLITE MARKET // AN EXTRACT © Euroconsult 2018 – Approved for public release ABOUT THIS RESEARCH REPORT SCOPE Prospects for the small satellite market presents the various factors that will drive/inhibit growth in demand for small satellites (<500 kg) over the next 10 years. This report considers satellites by four mass categories, six regions, six satellite applications and five manufacturer typologies. EXTENSIVE FIGURES & ANALYSIS FOR THE COMING DECADE All Euroconsult research has, at its core, data derived from over 30 years of tracking all levels of the satellite/space value chain. To this we add dozens of dedicated industry interviews each year, along with the continual refinement of our data models, and the collection and interpretation of company press releases and financial filings. Our consultants have decades of experience interpreting and analyzing our proprietary databases in light of the INCLUDED IN THIS PRODUCT broader value chain. When you purchase research from Euroconsult, you receive Forecast up to 2027 in units and value thousands of data points and the expert interpretation of what this means for specific verticals and sectors of the satellite value chain, including forecasts based on years of data and highly refined All segments of the value chain reviewed models. This report contains thousands of data points.