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Detecting, Tracking and Imaging Space Debris
r bulletin 109 — february 2002 Detecting, Tracking and Imaging Space Debris D. Mehrholz, L. Leushacke FGAN Research Institute for High-Frequency Physics and Radar Techniques, Wachtberg, Germany W. Flury, R. Jehn, H. Klinkrad, M. Landgraf European Space Operations Centre (ESOC), Darmstadt, Germany Earth’s space-debris environment tracked, with estimates for the number of Today’s man-made space-debris environment objects larger than 1 cm ranging from 100 000 has been created by the space activities to 200 000. that have taken place since Sputnik’s launch in 1957. There have been more than 4000 The sources of this debris are normal launch rocket launches since then, as well as many operations (Fig. 2), certain operations in space, other related debris-generating occurrences fragmentations as a result of explosions and such as more than 150 in-orbit fragmentation collisions in space, firings of satellite solid- events. rocket motors, material ageing effects, and leaking thermal-control systems. Solid-rocket Among the more than 8700 objects larger than 10 cm in Earth orbits, motors use aluminium as a catalyst (about 15% only about 6% are operational satellites and the remainder is space by mass) and when burning they emit debris. Europe currently has no operational space surveillance aluminium-oxide particles typically 1 to 10 system, but a powerful radar facility for the detection and tracking of microns in size. In addition, centimetre-sized space debris and the imaging of space objects is available in the form objects are formed by metallic aluminium melts, of the 34 m dish radar at the Research Establishment for Applied called ‘slag’. -
To Secure Long-Term Spaceflight Safety and Orbital Sustainability for the Benefit of Future Generations the Impact of Space Debris
To secure long-term spaceflight safety and orbital sustainability for the benefit of future generations The impact of space debris Our growing reliance on satellite services 1 active satellite 1957 1,950 active satellites 2019 20,000+ active satellites by 2030 67,000 collision alerts per year very day billions of people around the world rely One of the key ways to reduce the risk of collision in on data from satellites to go about their lives. We orbit is to remove potential threats. Designing and Eexchange messages, talk to family and friends, building a satellite to identify, track, rendezvous, dock check the weather, manage finances, and undertake and de-orbit a piece of debris is an extraordinarily numerous other tasks. In addition, satellites are used difficult technical task on its own. However, developing to manage and mitigate natural disasters, monitor the an orbital debris removal business involves more than Earth’s climate and well-being and provide information just creating the technical solution. We now need a for national security. In short, without satellite data, the consistent global effort to shape regulations and a lives of people around the world would be dramatically vibrant ecosystem that assures a business case. At different. And now the source of this data is at growing Astroscale we are working these important tasks risk of being destroyed by space debris. – developing the technologies, working with the policymakers and closing the business case – that will We don’t see these satellites and the millions of pieces allow for a long-term orbital debris solution. -
B-180466 Polar Orbiting Weather Satellite Programs
U-180466 l’ht! Honorable Frank E. Moss Chai rmnn, Committee on Aeronautical .r- Cf ‘ind Space Sciences ;>, r-,rr*Id- l~llll~llllllllllllllllllluu~llllllllllllllll United States Senate LM095911 f?- Dear Ilr. Chairman: Your January 1.6, 19 74, letter asked us to obtain cost and other data ~ on both the Department of the Air Force and the joint Natioual Aeronauticsn and Space Administration (NASA)/National Oceanic and Atmospheric Adminis- *76 tration (NOAA) polar orbiting weather satellite programs. L .-__,__ cs&~yl”.^-b -.,I-*Ii*--... --:- -*-“a .-,. We interviewed officials in NASA, NOM, the Department of the Air Force and the Office of Management and Budget (OHU). At these meetings they told us of the existence of two classified studies which provided some comparative analyses of the technical cfrar; cteristics and costs of the NASA and Air Force operational weather satellite systems and the follow-on sys tems in development . We then met with your staff on February 13, 1974, and orally presented the information, At that meeting your staff as ed us for 11 written re- port, We have not independently verified the d :ta; however, we have dis- cussed the matters in this report with the agent y officials. We plan to discuss briefly the history of I he NASA/NOM and Air Force satellite sys terns, compare tl~e characteristics Ilf both systems, provide cost comparisons of the operational- and develop~oental satellite --.-.systems, and furnish information on plans to obtain some mcasurc of commonality of bcltll sys terns. --_.III STORY _-- OF NASA/NOM --_-PKOCRhM The purpose of the joint NASA/NOAA weather satellite system is to provide systematic, +;Lobal cloud cover observations and other meteorologi- cal observations to incrt*&x: man’s ability to -forecast wc;lthcrI m--...YII-._conditions. -
History of NOAA's Polar Observational Environmental Satellites the First
History of NOAA’s Polar Observational Environmental Satellites The first weather satellite in a series of spacecraft originally known as the Television Infrared Observation Satellites (TIROS) was launched on April 1, 1960. By the mid 1970’s NOAA and NASA agreed to produce the series operationally based on the TIROS-N generation of satellites. TIROS-N, a research and development spacecraft serving as a prototype for the operational follow-on series, NOAA-A through NOAA-N Prime was on launched October 13, 1978. Beginning with NOAA-E, launched in 1983, the basic satellite was “stretched” to permit accommodation of additional research instruments. This became known as the Advanced TIROS-N configuration. Some of the additional instruments flown include: Search and Rescue; Earth Radiation Budget Experiment, and the Solar Backscatter Ultraviolet spectrometer. Three of those instruments, Search and Rescue Repeater, Search and Rescue Processor and Solar Backscatter Ultraviolet Radiometer, became part of the operational program. The primary sounding instrumentation has remained essentially unchanged until the addition of Advanced Microwave Sounding Units-A and -B on NOAA-K (15). The Microwave Humidity Sounder replaces the AMSU-B on NOAA-N Prime performing essentially the same science. The satellite design life throughout the series has been two years. The lifetime is a cost/risk tradeoff since more years normally result in a more expensive satellite. To mitigate that risk, the NOAA-N Prime satellite uses the most reliable NASA-approved flight parts, Class S, and considerable redundancy in critical subsystem components. The instruments are not redundant, but they have a three-year design life in order to enhance their expected operational reliability. -
NASA Process for Limiting Orbital Debris
NASA-HANDBOOK NASA HANDBOOK 8719.14 National Aeronautics and Space Administration Approved: 2008-07-30 Washington, DC 20546 Expiration Date: 2013-07-30 HANDBOOK FOR LIMITING ORBITAL DEBRIS Measurement System Identification: Metric APPROVED FOR PUBLIC RELEASE – DISTRIBUTION IS UNLIMITED NASA-Handbook 8719.14 This page intentionally left blank. Page 2 of 174 NASA-Handbook 8719.14 DOCUMENT HISTORY LOG Status Document Approval Date Description Revision Baseline 2008-07-30 Initial Release Page 3 of 174 NASA-Handbook 8719.14 This page intentionally left blank. Page 4 of 174 NASA-Handbook 8719.14 This page intentionally left blank. Page 6 of 174 NASA-Handbook 8719.14 TABLE OF CONTENTS 1 SCOPE...........................................................................................................................13 1.1 Purpose................................................................................................................................ 13 1.2 Applicability ....................................................................................................................... 13 2 APPLICABLE AND REFERENCE DOCUMENTS................................................14 3 ACRONYMS AND DEFINITIONS ...........................................................................15 3.1 Acronyms............................................................................................................................ 15 3.2 Definitions ......................................................................................................................... -
Space Debris
IADC-11-04 April 2013 Space Debris IADC Assessment Report for 2010 Issued by the IADC Steering Group Table of Contents 1. Foreword .......................................................................... 1 2. IADC Highlights ................................................................ 2 3. Space Debris Activities in the United Nations ................... 4 4. Earth Satellite Population .................................................. 6 5. Satellite Launches, Reentries and Retirements ................ 10 6. Satellite Fragmentations ................................................... 15 7. Collision Avoidance .......................................................... 17 8. Orbital Debris Removal ..................................................... 18 9. Major Meetings Addressing Space Debris ........................ 20 Appendix: Satellite Break-ups, 2000-2010 ............................ 22 IADC Assessment Report for 2010 i Acronyms ADR Active Debris Removal ASI Italian Space Agency CNES Centre National d’Etudes Spatiales (France) CNSA China National Space Agency CSA Canadian Space Agency COPUOS Committee on the Peaceful Uses of Outer Space, United Nations DLR German Aerospace Center ESA European Space Agency GEO Geosynchronous Orbit region (region near 35,786 km altitude where the orbital period of a satellite matches that of the rotation rate of the Earth) IADC Inter-Agency Space Debris Coordination Committee ISRO Indian Space Research Organization ISS International Space Station JAXA Japan Aerospace Exploration Agency LEO Low -
Orbiting Debris: a Space Environmental Problem (Part 4 Of
Orbiting Debris: A Since Environmential Problem ● 3 Table 2--of Hazardous Interference by environment. Yet, orbital debris is part of a Orbital Debris larger problem of pollution in space that in- cludes radio-frequency interference and inter- 1. Loss or damage to space assets through collision; ference to scientific observations in all parts of 2. Accidental re-entry of space hardware; the spectrum. For example, emissions at ra- 3. Contamination by nuclear material of manned or unmanned spacecraft, both in space and on Earth; dio frequencies often interfere with radio as- 4. Interference with astronomical observations, both from the tronomy observations. For several years, ground and in space; gamma-ray astronomy data have been cor- 5. Interference with scientific and military experiments in space; rupted by Soviet intelligence satellites that 14 6. Potential military use. are powered by unshielded nuclear reactors. The indirect emissions from these satellites SOURCE: Space Debris, European Space Agency, and Office of Technology As- sessment. spread along the Earth’s magnetic field and are virtually impossible for other satellites to Earth. The largest have attracted worldwide escape. The Japanese Ginga satellite, attention. 10 Although the risk to individuals is launched in 1987 to study gamma-ray extremely small, the probability of striking bursters, has been triggered so often by the populated areas still finite.11 For example: 1) Soviet reactors that over 40 percent of its available observing time has been spent trans- the U.S.S.R. Kosmos 954, which contained a 15 nuclear power source,12 reentered the atmos- mitting unintelligible “data.” All of these phere over northwest Canada in 1978, scatter- problem areas will require attention and posi- ing debris over an area the size of Austria; 2) a tive steps to guarantee access to space by all Japanese ship was hit in 1969 by pieces of countries in the future. -
Space Almanac 2007
2007 Space Almanac The US military space operation in facts and figures. Compiled by Tamar A. Mehuron, Associate Editor, and the staff of Air Force Magazine 74 AIR FORCE Magazine / August 2007 Space 0.05g 60,000 miles Geosynchronous Earth Orbit 22,300 miles Hard vacuum 1,000 miles Medium Earth Orbit begins 300 miles 0.95g 100 miles Low Earth Orbit begins 60 miles Astronaut wings awarded 50 miles Limit for ramjet engines 28 miles Limit for turbojet engines 20 miles Stratosphere begins 10 miles Illustration not to scale Artist’s conception by Erik Simonsen AIR FORCE Magazine / August 2007 75 US Military Missions in Space Space Support Space Force Enhancement Space Control Space Force Application Launch of satellites and other Provide satellite communica- Ensure freedom of action in space Provide capabilities for the ap- high-value payloads into space tions, navigation, weather infor- for the US and its allies and, plication of combat operations and operation of those satellites mation, missile warning, com- when directed, deny an adversary in, through, and from space to through a worldwide network of mand and control, and intel- freedom of action in space. influence the course and outcome ground stations. ligence to the warfighter. of conflict. US Space Funding Millions of constant Fiscal 2007 dollars 60,000 50,000 40,000 30,000 20,000 10,000 0 Fiscal Year 59 62 65 68 71 74 77 80 83 86 89 92 95 98 01 04 Fiscal Year NASA DOD Other Total Fiscal Year NASA DOD Other Total 1959 1,841 3,457 240 5,538 1983 13,051 18,601 675 32,327 1960 3,205 3,892 -
IADC Space Debris Mitigation Guidelines
IADC-02-01 Revision 2 Mar 2020 IADC Space Debris Mitigation Guidelines Issued by IADC Steering Group and Working Group 4 Table of Contents Table of Contents .................................................................................................................. 1 Revision History .................................................................................................................... 2 List of Abbreviations .............................................................................................................. 3 1 Scope ............................................................................................................................. 6 2 Application ...................................................................................................................... 6 3 Terms and definitions ..................................................................................................... 6 3.1 Space Debris ........................................................................................................... 6 3.2 Spacecraft, Launch Vehicles, and Orbital Stages .................................................... 6 3.3 Orbits and Protected Regions ................................................................................. 7 3.4 Mitigation Measures and Related Terms ................................................................. 8 3.5 Operational Phases ................................................................................................. 8 4 General Guidance ......................................................................................................... -
10. Satellite Weather and Climate Monitoring
II. INTENSITY: ACTIVITIES AND OUTPUTS IN THE SPACE ECONOMY 10. Satellite weather and climate monitoring Meteorology was the first scientific discipline to use space Figure 1.2). The United States, the European Space Agency capabilities in the 1960s, and today satellites provide obser- and France have established the most joint operations for vations of the state of the atmosphere and ocean surface environmental satellite missions (e.g. NASA is co-operating for the preparation of weather analyses, forecasts, adviso- with Japan’s Aerospace Exploration Agency on the Tropical ries and warnings, for climate monitoring and environ- Rainfall Measuring Mission (TRMM); ESA and NASA cooper- mental activities. Three quarters of the data used in ate on the Solar and Heliospheric Observatory (SOHO), numerical weather prediction models depend on satellite while the French CNES is co-operating with India on the measurements (e.g. in France, satellites provide 93% of data Megha-Tropiques mission to study the water cycle). Para- used in Météo-France’s Arpège model). Three main types of doxically, although there have never been so many weather satellites provide data: two families of weather satellites and environmental satellites in orbit, funding issues in and selected environmental satellites. several OECD countries threaten the sustainability of the Weather satellites are operated by agencies in China, provision of essential long-term data series on climate. France, India, Japan, Korea, the Russian Federation, the United States and Eumetsat for Europe, with international co-ordination by the World Meteorological Organisation Methodological notes (WMO). Some 18 geostationary weather satellites are posi- Based on data from the World Meteorological Orga- tioned above the earth’s equator, forming a ring located at nisation’s database Observing Systems Capability Analy- around 36 000 km (Table 10.1). -
Joint Polar Satellite System (JPSS) Common Ground System (CGS)
Joint Polar Satellite System (JPSS) Common Ground System (CGS) A flexible, cost-effective global common ground system designed to support current and future weather and environmental sensing satellite missions. Key Features and Benefits The JPSS Program Overview The JPSS program will also The polar orbiters which are able Joint Polar Satellite System (JPSS) integrate future civilian and to monitor the entire planet and g Operational -- supported is designed to monitor global military (Defense Weather Satellite provide data for long-range successful NPP launch environmental conditions in System – DWSS) polar-orbiting weather and climate forecasts, will g Flexible architecture designed addition to collecting and environmental satellite space and carry a complement of advanced to quickly adapt to evolving disseminating data related to the ground segments with a single imaging and sounding sensors mission needs weather, atmosphere, oceans, land ground system. that will acquire data at a much and near-space environment. The higher fidelity and frequency than g Unique integration of new and JPSS Top Level Architecture new system represents a major heritage systems available today. legacy technologies JPSS is an “end-to-end” system upgrade to the existing Polar- that includes sensors; spacecraft; The JPSS CGS Distributed g Available to support diverse orbiting Operational command, control and Receptor Network (DRN) civil, military and scientific Environmental Satellites (POES), communications; data routing; architecture will provide frequent environmental needs which have successfully served the and ground based processing. JPSS downlinks to maximize contact operational weather forecasting g Fully integrated global ground and DWSS spacecraft will carry duration at low cost. JPSS CGS community for nearly 50 years. -
Japan's Technical Prowess International Cooperation
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Japan’s Technical Prowess Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness.