This document provides an assessment of the nano/microsatellite market from 2014-2020 conducted by SpaceWorks Enterprises. Some key findings include:
- SpaceWorks projects 410-543 nano/microsatellites will need launches globally in 2020, compared to 92 in 2013, representing significant growth.
- While the civil sector will remain important, contributing over 1/3 of future satellites, commercial companies are emerging and expected to influence the market greatly, contributing an estimated 56% of future satellites.
- Earth observation and remote sensing are projected to be the largest application areas for nano/microsatellites in the future, replacing technology demonstration as the main purpose in the past.
- Continued standardization, technology
Space Works Nano Microsatellite Market forecast 2016Dmitry Tseitlin
This document provides a summary of SpaceWorks' 2016 forecast for the nano/microsatellite market. Some key points:
- SpaceWorks predicts over 480 nano/microsatellites (1-50kg) will launch globally in 2016-2018, a 35% increase from their 2014 forecast, driven by growing commercial interest.
- The commercial sector is expected to contribute over 70% of future satellites compared to 37% in 2009-2015.
- More than 70% of future satellites will be used for Earth observation and remote sensing, compared to 37% in 2009-2015.
- While still popular for academia, 1-3kg CubeSats will decline to under 30% of the market
Nano-satellites Design, Development, Implementation and Applicationajogeo
This document discusses nanosatellites, which are miniaturized satellites between 1-10kg that are as small as 10x10x10 cm. Nanosatellites are commonly used in constellations to allow for multi-point data collection across large areas in space. They are advantageous due to their cost effectiveness, enabling large scale applications with functionality and robustness. Some of the key challenges in nanosatellite design include miniaturizing subsystems, managing thermal regulation, increasing electrical power efficiency, integrating structures, developing micropropulsion, and ensuring safety. The proliferation of nanosatellites is driving commercialization of space technologies.
The document discusses nanosatellites and their advantages over larger satellites. It defines different classes of small satellites based on mass, including nanosatellites which are between 1-10 kg. Nanosatellites allow for lower costs, easier production, and more opportunities for new missions compared to larger satellites. Examples of nanosatellite applications demonstrated include technology demonstrations, Earth observation, and biological experiments. The global market for nanosatellite launches is projected to grow significantly in the coming years.
The document provides an overview of trends in the nanosatellite industry as of October 2013. It discusses how nanosatellites are categorized based on weight, trends of increasing users from educational to commercial applications, enabling technologies like improved communications and attitude determination and control systems, and debunks myths about nanosatellite reliability compared to facts about operational lifetimes of over 10 years for some nanosatellites.
Mini, micro, and nanosatellites are classifications of small, low-mass satellites under 500 kg. Miniaturizing satellites reduces costs by requiring smaller, cheaper launch vehicles. They also allow for more missions like satellite constellations and university research. The nanosatellite market is growing rapidly, with over 1,000 projected to launch in the next five years. ISRO has launched several microsatellites to demonstrate new technologies and conduct academic research missions with lower costs.
This document discusses the potential role of nanosatellites in future geodesy missions. It describes several ways nanosatellites could improve geodetic measurements, such as increasing spatial and temporal sampling. Specific nanosatellite missions discussed include the Drag Free Satellite, Gravity Explorer, and the Canadian CanX-4 and CanX-5 formation flying satellites. Payloads that could be miniaturized for nanosatellites include accelerometers, atomic clocks, star cameras, GPS receivers, and intersatellite ranging instruments. Attitude control techniques like magnetic torquers would need to be studied further for precision formation flying applications. The conclusion is that nanosatellites have the potential to contribute useful data to future gravity field
Nano-satellites are small satellites with a mass between 1-10 kg that are used to reduce the cost of satellite launches. They can be spin-stabilized to maximize solar power or use 3-axis stabilization. Key technologies for nano-satellites include miniaturized propulsion, guidance and sensors, low-power electronics, thermal management, and communication systems. Nano-satellites are designed to be autonomous and conduct in-situ measurements to minimize operational costs when deployed in large constellations.
This presentation provides an overview of small satellites, including microsatellites, nanosatellites, and picosatellites. It discusses the history and increasing use of small satellites worldwide. Key points include:
- Small satellites are less than 100kg and have smaller electronic components, making them more cost-effective for certain space missions.
- India has launched several small satellites in recent years including Jugnu in 2011, the first Indian nanosatellite developed by IIT Kanpur.
- Small satellites have applications in areas like weather measurement, communication, and earth observation and can provide efficient access to space for educational institutions and corporations.
- Advantages of small satellites include lower cost, easier launch
Space Works Nano Microsatellite Market forecast 2016Dmitry Tseitlin
This document provides a summary of SpaceWorks' 2016 forecast for the nano/microsatellite market. Some key points:
- SpaceWorks predicts over 480 nano/microsatellites (1-50kg) will launch globally in 2016-2018, a 35% increase from their 2014 forecast, driven by growing commercial interest.
- The commercial sector is expected to contribute over 70% of future satellites compared to 37% in 2009-2015.
- More than 70% of future satellites will be used for Earth observation and remote sensing, compared to 37% in 2009-2015.
- While still popular for academia, 1-3kg CubeSats will decline to under 30% of the market
Nano-satellites Design, Development, Implementation and Applicationajogeo
This document discusses nanosatellites, which are miniaturized satellites between 1-10kg that are as small as 10x10x10 cm. Nanosatellites are commonly used in constellations to allow for multi-point data collection across large areas in space. They are advantageous due to their cost effectiveness, enabling large scale applications with functionality and robustness. Some of the key challenges in nanosatellite design include miniaturizing subsystems, managing thermal regulation, increasing electrical power efficiency, integrating structures, developing micropropulsion, and ensuring safety. The proliferation of nanosatellites is driving commercialization of space technologies.
The document discusses nanosatellites and their advantages over larger satellites. It defines different classes of small satellites based on mass, including nanosatellites which are between 1-10 kg. Nanosatellites allow for lower costs, easier production, and more opportunities for new missions compared to larger satellites. Examples of nanosatellite applications demonstrated include technology demonstrations, Earth observation, and biological experiments. The global market for nanosatellite launches is projected to grow significantly in the coming years.
The document provides an overview of trends in the nanosatellite industry as of October 2013. It discusses how nanosatellites are categorized based on weight, trends of increasing users from educational to commercial applications, enabling technologies like improved communications and attitude determination and control systems, and debunks myths about nanosatellite reliability compared to facts about operational lifetimes of over 10 years for some nanosatellites.
Mini, micro, and nanosatellites are classifications of small, low-mass satellites under 500 kg. Miniaturizing satellites reduces costs by requiring smaller, cheaper launch vehicles. They also allow for more missions like satellite constellations and university research. The nanosatellite market is growing rapidly, with over 1,000 projected to launch in the next five years. ISRO has launched several microsatellites to demonstrate new technologies and conduct academic research missions with lower costs.
This document discusses the potential role of nanosatellites in future geodesy missions. It describes several ways nanosatellites could improve geodetic measurements, such as increasing spatial and temporal sampling. Specific nanosatellite missions discussed include the Drag Free Satellite, Gravity Explorer, and the Canadian CanX-4 and CanX-5 formation flying satellites. Payloads that could be miniaturized for nanosatellites include accelerometers, atomic clocks, star cameras, GPS receivers, and intersatellite ranging instruments. Attitude control techniques like magnetic torquers would need to be studied further for precision formation flying applications. The conclusion is that nanosatellites have the potential to contribute useful data to future gravity field
Nano-satellites are small satellites with a mass between 1-10 kg that are used to reduce the cost of satellite launches. They can be spin-stabilized to maximize solar power or use 3-axis stabilization. Key technologies for nano-satellites include miniaturized propulsion, guidance and sensors, low-power electronics, thermal management, and communication systems. Nano-satellites are designed to be autonomous and conduct in-situ measurements to minimize operational costs when deployed in large constellations.
This presentation provides an overview of small satellites, including microsatellites, nanosatellites, and picosatellites. It discusses the history and increasing use of small satellites worldwide. Key points include:
- Small satellites are less than 100kg and have smaller electronic components, making them more cost-effective for certain space missions.
- India has launched several small satellites in recent years including Jugnu in 2011, the first Indian nanosatellite developed by IIT Kanpur.
- Small satellites have applications in areas like weather measurement, communication, and earth observation and can provide efficient access to space for educational institutions and corporations.
- Advantages of small satellites include lower cost, easier launch
The document discusses pico, nano, and micro satellites, noting their size has decreased significantly over time from the size of a bus to as small as a postcard. It provides an overview of the basic components of satellites including communication systems, power systems, on-board computers, and payloads. The document also notes that smaller satellites are advantageous as they are cheaper to design and launch compared to conventional satellites.
A CubeSat (U-class spacecraft) is a type of miniaturized satellite for space research that is made up of multiples of 10×10×10 cm cubic units. CubeSats have a mass of no more than 1.33 kilograms per unit.
The document discusses the potential for lunar ultraviolet observatories. It notes that the Moon provides a stable location with no atmosphere to observe UV radiation from sources like the intergalactic medium, exoplanets, and the Earth's magnetosphere and exosphere. A proposed mission called EarthASAP would use a cubesat in lunar orbit to produce the first 3D map of the Earth's exosphere and monitor interactions between the Earth and solar wind. Such observations from the Moon's perspective could provide important data for studying exoplanets and space weather effects. The document outlines the science goals and technological requirements for EarthASAP and lunar UV observatories more broadly.
The document discusses plans to convert an existing 32-meter satellite dish in Greece called ThermopYlae into a radio telescope. It was originally used for telecommunications but is now part of a global effort to repurpose large satellite antennas for radio astronomy research. The document outlines work already completed, such as preliminary measurements and collaborations. Future plans include upgrading receivers, implementing new control systems, and using ThermopYlae for single dish observations and inclusion in radio interferometry networks to help detect astrophysical sources. The document also discusses broader topics like conducting radio astronomy from the moon to study the early universe.
The document summarizes the first direct image taken of a black hole by the Event Horizon Telescope in 2017. Key points include:
1) The image showed a dark circle surrounded by a bright ring, matching predictions from Einstein's theory of general relativity for the shadow and photon ring around a black hole.
2) Analysis of the image allowed estimation of the black hole's size and properties, concluding it has a mass of around 6.5 billion solar masses and is located 53 million light years away at the center of the M87 galaxy.
3) Future research aims to take even higher resolution images with improved telescopes to learn more about black hole physics and further test Einstein's theory of general relativity. Asia
Foing vienna astromoon galaxy forum 18 sept 2020ILOAHawaii
This document discusses astronomy projects from the Moon including:
1) Robotic telescopes could observe from the Moon in all wavelengths without atmospheric interference and study the solar system.
2) The ExoGeoLab project developed a lunar lander and remote-controlled telescope to demonstrate astronomy and remote supervision from the Moon.
3) Upcoming projects include the Chang'E 3 telescope on the Moon, radio astronomy from orbiters and small landers, and future observatories at human outposts. Liquid mirror telescopes are also proposed to take advantage of the Moon's environment.
GSAT-14 is an Indian communications satellite launched in 2014. It was constructed by ISRO based on the I-2K satellite bus, weighing 851 kg without fuel. GSAT-14 has a design life of 12 years and carries experiments in new technologies. After a scrubbed first launch attempt in 2013, GSAT-14 was successfully launched in January 2014 atop a GSLV Mk-II rocket, ending a streak of four previous GSLV failures. Aryabhata was India's first satellite, launched in 1975 to gain experience in space and conduct experiments in x-ray astronomy, agriculture, and solar physics. It helped establish India's space program and space science investigations.
International Astronomy from the Moon
Southeast Asia and Beyond
The document discusses conducting astronomy from the moon, including as a shield from the sun/earth, as a stable platform, and for access from a lunar base. It outlines past and current lunar astronomy studies and proposals from agencies like NASA, ESA, China, and opportunities for involvement from Southeast Asian countries. Key points include China's Chang'e lunar telescope capturing over 32,000 images, and potential for commercial communications from the moon to expand coverage. Moon plans from agencies like NASA, JAXA, ISRO, KARI, and CSA are summarized.
A GEO satellite’s distance from earth gives it a large coverage area, almost a fourth of the earth’s surface and also have 24 hour view of a particular area.This will be very helpful to army,navy etc.,These factors make it ideal for satellite broadcast and other multipoint applications.Continuous monitoring is done and also cost effective in long term, risk-less.
The document provides an overview of the Maunakea Spectroscopic Explorer (MSE), an innovative upgrade to the 3.6m Canada-France-Hawaii Telescope (CFHT) located on Maunakea, Hawaii. MSE will have the unique capability to obtain spectra of thousands of astronomical targets simultaneously, allowing it to survey the sky and answer fundamental questions in astronomy. It will have a large primary mirror, wide field of view, and ability to observe in optical and near-infrared wavelengths. MSE is designed through international collaboration and will continue CFHT's legacy of community outreach and education.
Galaxy Forum SEA 2016 Malaysia - Hakim MalasanILOAHawaii
The 1st Galaxy Forum in Malaysia is being held in cooperation with the Space Science Centre at the National University of Malaysia in Kuala Lumpur. The event will be held in Dewan Kuliah Tun Abdullah Mohd Salleh Hall. ANGKASA was founded as a multidisciplinary research institute conducting teaching at postgraduate level and research in the field of;
Space Science: Astronomy, astrophysics, astrobiology, space chemistry, geology and meteorology of the planet
Space Technology: Design and installation of systems for communication, control and drive for rocket and spacecraft
Space Technology Applications: Covering meteorologists field, environmental management, disaster management and land use
Space Governance: Space law and international relations associated with the exploration and use of space
Galaxy Forum is the primary education and outreach initiative of the International Lunar Observatory Association, an architecture designed to advance 21st Century science, education, enterprise and development.
Galaxy Forums are public events specifically geared towards high school teachers, educators, astronomers of all kinds, students and the general public. Presentations are provided by experts in the fields of astrophysics / galaxy research, space exploration and STEM education, as well as related aspects of culture and traditional knowledge. Interactive panel discussions allow for community participation and integration of local perspectives.
Sixty-five Galaxy Forums with a total of almost 300 presentations have been held in 26 locations worldwide (since Galaxy Forum USA, July 4, 2008) including Hawaii, Silicon Valley, Canada, China, India, Southeast Asia, Japan, Europe, Africa, Chile, Brazil, Kansas and New York.
This document discusses various applications of microsatellites including expanding access to space for countries, conducting science experiments in orbit related to biology and atmospheric research, demonstrating new technologies, supporting education through university and high school satellite projects, enabling private imaging satellites, and allowing amateur satellite projects. The future applications discussed include using microsatellites as auxiliary payloads on interplanetary missions and as constellations. The conclusion predicts that 2,000-2,750 nano/microsatellites will require launches between 2014-2020 based on a market assessment.
The UH88" telescope located on Maunakea in Hawaii is well positioned for the 21st century. It was the first large telescope built on Maunakea in 1968 and its observations led to the discovery of the Kuiper Belt in 1992. With recent refurbishments and funding for new instrumentation, the UH88" can continue its unique science and educational role. It has a superb location for astronomy and can enable innovative capabilities like robotic observing and adaptive optics to perform high cadence classification of supernovae and other targets. The telescope also provides students with hands-on experience and helps develop a STEM workforce through technology innovation.
Cube Satellites are standardized Nano-satellites for space researches and applications. CubeSat can be created using COTS Hardware and is a very creative utilizing of the knowledge of Embedded Systems and various MEMS sensor devices
Galaxy Forum Southeast Asia 2013 - Dr. Boonrucksar soonthornthumILOAHawaii
NARIT is Thailand's national research institute for astronomy. It aims to develop astronomy education in Thailand and Southeast Asia through several initiatives:
1. It supports astronomy education in Thai schools and universities by developing curriculum and signing agreements with cooperative universities.
2. NARIT established the Thai National Observatory with a 2.4-meter telescope to conduct research and provide training.
3. It leads regional astronomy networks and collaborates internationally on education, research, and telescope development to advance the field in Southeast Asia.
This document summarizes the proceedings of the 3rd annual meeting of the NASA Institute for Advanced Concepts (NIAC) held on June 5-6, 2001 at NASA Ames Research Center. It provides an overview of proposals received and awards given by NIAC, as well as summaries of the status reports presented on innovative advanced aerospace concepts. The status reports covered concepts such as a space elevator, robotic planetary explorers, very large space telescopes, and in-situ resource utilization for Mars missions. Keynote speakers discussed visions for the future of aeronautics and space.
Satellites orbit Earth for a variety of purposes such as communication, weather monitoring, and navigation. They come in different types depending on their distance from Earth, including low-Earth orbit, medium-Earth orbit, and geostationary orbit. The Global Positioning System is a constellation of 24 satellites that provides location and time information to GPS receivers anywhere on Earth.
ILOA Galaxy Forum SEA 2014 -- Taufiq HidayatILOAHawaii
This document outlines a plan for a new multi-wavelength astronomical observatory in Indonesia. It discusses the history and facilities of the Bosscha Observatory and the need to modernize. Previous proposals from the 1980s are mentioned. Current preparations include site selection surveys of over 30 mountain sites, with Mount Timau emerging as a top candidate. Technical development work is also underway at Bosscha Observatory. The conclusion calls for further development, fundraising, and cooperation to realize the new observatory outlined in a "grand proposal."
The document discusses the growth of small satellites or smallsats, including NewSpace constellations. Over 3,600 smallsats are expected to be launched between 2016 and 2025 for applications like Earth observation, technology demonstration, satellite communications, science, and space situational awareness. The value of the smallsat market is estimated to reach $22 billion during this period, driven largely by planned constellations like OneWeb. New dedicated smallsat manufacturers are entering the market to provide flexible and lower-cost satellite solutions to support the growing demand.
The document provides an overview of the space sector, including the value chain from satellite manufacturing to services. It discusses major players in upstream manufacturing (Boeing, Lockheed Martin, etc.) and downstream services (telecom providers, satellite TV, etc.). The business models are described as institutional, government owned/operated, concession, and mature private. Sustainability challenges are noted when applications are emerging but investment is large. Potential influencers and investors in the sector are also mentioned, such as Elon Musk, Mark Zuckerberg, and Bill Gates.
The document discusses pico, nano, and micro satellites, noting their size has decreased significantly over time from the size of a bus to as small as a postcard. It provides an overview of the basic components of satellites including communication systems, power systems, on-board computers, and payloads. The document also notes that smaller satellites are advantageous as they are cheaper to design and launch compared to conventional satellites.
A CubeSat (U-class spacecraft) is a type of miniaturized satellite for space research that is made up of multiples of 10×10×10 cm cubic units. CubeSats have a mass of no more than 1.33 kilograms per unit.
The document discusses the potential for lunar ultraviolet observatories. It notes that the Moon provides a stable location with no atmosphere to observe UV radiation from sources like the intergalactic medium, exoplanets, and the Earth's magnetosphere and exosphere. A proposed mission called EarthASAP would use a cubesat in lunar orbit to produce the first 3D map of the Earth's exosphere and monitor interactions between the Earth and solar wind. Such observations from the Moon's perspective could provide important data for studying exoplanets and space weather effects. The document outlines the science goals and technological requirements for EarthASAP and lunar UV observatories more broadly.
The document discusses plans to convert an existing 32-meter satellite dish in Greece called ThermopYlae into a radio telescope. It was originally used for telecommunications but is now part of a global effort to repurpose large satellite antennas for radio astronomy research. The document outlines work already completed, such as preliminary measurements and collaborations. Future plans include upgrading receivers, implementing new control systems, and using ThermopYlae for single dish observations and inclusion in radio interferometry networks to help detect astrophysical sources. The document also discusses broader topics like conducting radio astronomy from the moon to study the early universe.
The document summarizes the first direct image taken of a black hole by the Event Horizon Telescope in 2017. Key points include:
1) The image showed a dark circle surrounded by a bright ring, matching predictions from Einstein's theory of general relativity for the shadow and photon ring around a black hole.
2) Analysis of the image allowed estimation of the black hole's size and properties, concluding it has a mass of around 6.5 billion solar masses and is located 53 million light years away at the center of the M87 galaxy.
3) Future research aims to take even higher resolution images with improved telescopes to learn more about black hole physics and further test Einstein's theory of general relativity. Asia
Foing vienna astromoon galaxy forum 18 sept 2020ILOAHawaii
This document discusses astronomy projects from the Moon including:
1) Robotic telescopes could observe from the Moon in all wavelengths without atmospheric interference and study the solar system.
2) The ExoGeoLab project developed a lunar lander and remote-controlled telescope to demonstrate astronomy and remote supervision from the Moon.
3) Upcoming projects include the Chang'E 3 telescope on the Moon, radio astronomy from orbiters and small landers, and future observatories at human outposts. Liquid mirror telescopes are also proposed to take advantage of the Moon's environment.
GSAT-14 is an Indian communications satellite launched in 2014. It was constructed by ISRO based on the I-2K satellite bus, weighing 851 kg without fuel. GSAT-14 has a design life of 12 years and carries experiments in new technologies. After a scrubbed first launch attempt in 2013, GSAT-14 was successfully launched in January 2014 atop a GSLV Mk-II rocket, ending a streak of four previous GSLV failures. Aryabhata was India's first satellite, launched in 1975 to gain experience in space and conduct experiments in x-ray astronomy, agriculture, and solar physics. It helped establish India's space program and space science investigations.
International Astronomy from the Moon
Southeast Asia and Beyond
The document discusses conducting astronomy from the moon, including as a shield from the sun/earth, as a stable platform, and for access from a lunar base. It outlines past and current lunar astronomy studies and proposals from agencies like NASA, ESA, China, and opportunities for involvement from Southeast Asian countries. Key points include China's Chang'e lunar telescope capturing over 32,000 images, and potential for commercial communications from the moon to expand coverage. Moon plans from agencies like NASA, JAXA, ISRO, KARI, and CSA are summarized.
A GEO satellite’s distance from earth gives it a large coverage area, almost a fourth of the earth’s surface and also have 24 hour view of a particular area.This will be very helpful to army,navy etc.,These factors make it ideal for satellite broadcast and other multipoint applications.Continuous monitoring is done and also cost effective in long term, risk-less.
The document provides an overview of the Maunakea Spectroscopic Explorer (MSE), an innovative upgrade to the 3.6m Canada-France-Hawaii Telescope (CFHT) located on Maunakea, Hawaii. MSE will have the unique capability to obtain spectra of thousands of astronomical targets simultaneously, allowing it to survey the sky and answer fundamental questions in astronomy. It will have a large primary mirror, wide field of view, and ability to observe in optical and near-infrared wavelengths. MSE is designed through international collaboration and will continue CFHT's legacy of community outreach and education.
Galaxy Forum SEA 2016 Malaysia - Hakim MalasanILOAHawaii
The 1st Galaxy Forum in Malaysia is being held in cooperation with the Space Science Centre at the National University of Malaysia in Kuala Lumpur. The event will be held in Dewan Kuliah Tun Abdullah Mohd Salleh Hall. ANGKASA was founded as a multidisciplinary research institute conducting teaching at postgraduate level and research in the field of;
Space Science: Astronomy, astrophysics, astrobiology, space chemistry, geology and meteorology of the planet
Space Technology: Design and installation of systems for communication, control and drive for rocket and spacecraft
Space Technology Applications: Covering meteorologists field, environmental management, disaster management and land use
Space Governance: Space law and international relations associated with the exploration and use of space
Galaxy Forum is the primary education and outreach initiative of the International Lunar Observatory Association, an architecture designed to advance 21st Century science, education, enterprise and development.
Galaxy Forums are public events specifically geared towards high school teachers, educators, astronomers of all kinds, students and the general public. Presentations are provided by experts in the fields of astrophysics / galaxy research, space exploration and STEM education, as well as related aspects of culture and traditional knowledge. Interactive panel discussions allow for community participation and integration of local perspectives.
Sixty-five Galaxy Forums with a total of almost 300 presentations have been held in 26 locations worldwide (since Galaxy Forum USA, July 4, 2008) including Hawaii, Silicon Valley, Canada, China, India, Southeast Asia, Japan, Europe, Africa, Chile, Brazil, Kansas and New York.
This document discusses various applications of microsatellites including expanding access to space for countries, conducting science experiments in orbit related to biology and atmospheric research, demonstrating new technologies, supporting education through university and high school satellite projects, enabling private imaging satellites, and allowing amateur satellite projects. The future applications discussed include using microsatellites as auxiliary payloads on interplanetary missions and as constellations. The conclusion predicts that 2,000-2,750 nano/microsatellites will require launches between 2014-2020 based on a market assessment.
The UH88" telescope located on Maunakea in Hawaii is well positioned for the 21st century. It was the first large telescope built on Maunakea in 1968 and its observations led to the discovery of the Kuiper Belt in 1992. With recent refurbishments and funding for new instrumentation, the UH88" can continue its unique science and educational role. It has a superb location for astronomy and can enable innovative capabilities like robotic observing and adaptive optics to perform high cadence classification of supernovae and other targets. The telescope also provides students with hands-on experience and helps develop a STEM workforce through technology innovation.
Cube Satellites are standardized Nano-satellites for space researches and applications. CubeSat can be created using COTS Hardware and is a very creative utilizing of the knowledge of Embedded Systems and various MEMS sensor devices
Galaxy Forum Southeast Asia 2013 - Dr. Boonrucksar soonthornthumILOAHawaii
NARIT is Thailand's national research institute for astronomy. It aims to develop astronomy education in Thailand and Southeast Asia through several initiatives:
1. It supports astronomy education in Thai schools and universities by developing curriculum and signing agreements with cooperative universities.
2. NARIT established the Thai National Observatory with a 2.4-meter telescope to conduct research and provide training.
3. It leads regional astronomy networks and collaborates internationally on education, research, and telescope development to advance the field in Southeast Asia.
This document summarizes the proceedings of the 3rd annual meeting of the NASA Institute for Advanced Concepts (NIAC) held on June 5-6, 2001 at NASA Ames Research Center. It provides an overview of proposals received and awards given by NIAC, as well as summaries of the status reports presented on innovative advanced aerospace concepts. The status reports covered concepts such as a space elevator, robotic planetary explorers, very large space telescopes, and in-situ resource utilization for Mars missions. Keynote speakers discussed visions for the future of aeronautics and space.
Satellites orbit Earth for a variety of purposes such as communication, weather monitoring, and navigation. They come in different types depending on their distance from Earth, including low-Earth orbit, medium-Earth orbit, and geostationary orbit. The Global Positioning System is a constellation of 24 satellites that provides location and time information to GPS receivers anywhere on Earth.
ILOA Galaxy Forum SEA 2014 -- Taufiq HidayatILOAHawaii
This document outlines a plan for a new multi-wavelength astronomical observatory in Indonesia. It discusses the history and facilities of the Bosscha Observatory and the need to modernize. Previous proposals from the 1980s are mentioned. Current preparations include site selection surveys of over 30 mountain sites, with Mount Timau emerging as a top candidate. Technical development work is also underway at Bosscha Observatory. The conclusion calls for further development, fundraising, and cooperation to realize the new observatory outlined in a "grand proposal."
The document discusses the growth of small satellites or smallsats, including NewSpace constellations. Over 3,600 smallsats are expected to be launched between 2016 and 2025 for applications like Earth observation, technology demonstration, satellite communications, science, and space situational awareness. The value of the smallsat market is estimated to reach $22 billion during this period, driven largely by planned constellations like OneWeb. New dedicated smallsat manufacturers are entering the market to provide flexible and lower-cost satellite solutions to support the growing demand.
The document provides an overview of the space sector, including the value chain from satellite manufacturing to services. It discusses major players in upstream manufacturing (Boeing, Lockheed Martin, etc.) and downstream services (telecom providers, satellite TV, etc.). The business models are described as institutional, government owned/operated, concession, and mature private. Sustainability challenges are noted when applications are emerging but investment is large. Potential influencers and investors in the sector are also mentioned, such as Elon Musk, Mark Zuckerberg, and Bill Gates.
Space Mission UK is an exciting series of entrepreneur missions specifically designed to support UK startups with their ambition to build world-leading space and satellite application companies. It’s supported by Innovate UK, UK Trade & Investment and produced by Chinwag.
The first mission took place 8-14 August 2015 visiting the Small Sat Conference in Utah, followed by a packed programme in San Francisco, Silicon Valley and Los Angeles.
Editorial – Jan/Feb/Mar 2013 – Impact of the loss/addition of satellite altimetry on operational
products
Greengs all,
This issue is dedicated to the study of the impact of the loss or addion of satellite almetry on operaonal products and systems.
The first news feature by Larnicol et al. is presenng the GODAE OceanView Observing System Evaluaon Task Team which primary objecve is to
support observaonal agencies by demonstrang the impact of observaons on operaonal forecast and reanalysis systems. Its secondary objecve
is to improve the performance of operaonal ocean forecast systems.
The second paper by Labroue et al. is reminding us about the main 2012 events within the satellite almetry constellaon. For the past two decades,
we have been used to take for granted the presence of several satellites flying together. The loss of Envisat in April 2012 and the decision to
put Jason-1 on its end of life orbit is a crude reminder of this constellaon fragility. Hence during 2012, the DUACS and MyOcean Sea Level TAC
teams have contributed to secure the almetry component in the frame of operaonal oceanography.
The third paper by Labroue et al. is displaying the potenal offered by Cryosat-2 for the mesoscale signal. The added value brought by Cryosat-2 as a
complement to the exisng almetry constellaon is discussed as well as how Cryosat-2 could contribute to secure the almetry constellaon and
thus the operaonal oceanography. Cryosat-2 mission has been introduced into the Near Real Time Sea Level system since February 2012 and has
been added to the Delayed Time system in April 2012.
The fourth paper by Remy et al. addresses the impact of the change of the satellite constellaon on the French Mercator Ocean analysis and forecas
ng systems. The impact of the loss of the ENVISAT and Jason1 along track Sea Level Anomaly data in the beginning of the year 2012 in the real
me products is studied. A dedicated set of Observing System Experiments (OSEs) is performed and preliminary results are shown. An OSE involves
running a copy of an exisng assimilaon run where some observaons are excluded. The difference between this run and the original run assimila
ng all the observaons allows a detailed assessment of the impact the observaons have on the assimilaon system.
Finally, the fi8h paper by Lea et al. is showing a number of Observing System Experiments (OSEs) to assess the impact of the observing network on
FOAM, the UK Met Office’s ocean assimilaon and forecasng system, as part of GODAE OceanView. A parallel version of the FOAM operaonal
system was run, during April 2011, withholding Jason-2 almeter observaons. Withholding Jason-2 removed 43% of the almeter data and resulted
in a 4% increase in the RMS SSH observaon-minus-background differences and around ±2ºC small scale changes in 100m temperature as well as
around ±0.2 psu changes in surface salinity.
We will meet again in April 2013 for a j
This document summarizes the goals and organization of the Canadian Satellite Design Challenge (CSDC) team at York University. The team aims to design and build a cubesat carrying an infrared camera to obtain spectral imagery of the upper atmosphere and analyze greenhouse gases. The diverse team of engineering, science, and business students works towards this goal through designing the satellite, managing the project, and securing facilities. The experience provides hands-on learning for students while pursuing the mission objectives.
This document presents an analysis of low Earth orbit (LEO) launch capabilities conducted for SPEC Innovations. The analysis aimed to determine the optimal mix of current launch vehicles and technologies to transport 1000 metric tons of material to LEO within 30 months for less than $32 billion. The analysis considered variables such as cost, turnaround time, payload capacity, and technology readiness for different launch options. An optimization model was developed and run to identify the initial optimal launch strategy. Extensive sensitivity analysis was then performed to account for risks from immature technologies and potential geopolitical issues limiting availability of certain options. The results showed that limiting launch vehicle choices would significantly increase total project costs, and removing either the Falcon Heavy or Pro
This document proposes launching a fleet of 75 satellites to form company logos and names in the sky. It estimates costs for the Boeing 702HP satellites at $100 million each, a Sea Launch rocket at $57 million per launch, and a 24-year, 300-person operations team. The timeline is to start satellite production in 2012, with launches from 2017-2020. Additional revenue streams could come from branding the satellites or leasing transponder space. The overall budget is preliminary and does not include many additional expenses.
TU1.L10 - Globwave and applications of global satellite wave observationsgrssieee
The GlobWave project aims to improve the use of satellite-derived wind and wave data. It develops a web portal providing access to multi-sensor satellite wave data in a common format, demonstration products, and tools for comparing satellite and model wave data. The project is led by Logica and involves partners ESA, CNES, Ifremer, SatOC, CLS, and NOC.
Small Satellites: Landscape and Market - New Constellations - New Uses Cases ...Hugo Wagner
Constellations of small satellites—“smallsats”, i.e. low cost, low mass (1-150 kg) and small sized—
dominate the news today, touted in applications as wide-ranging as providing universal connectivity,
ubiquitous broadband coverage, and daily observation of the Earth. Today, a combination of
miniaturized commercial off-the-shelf components (COTS) and satellite technology, coupled with
advanced sensors, faster computing, and a need for better actionable imagery, have all acted to usher
in a new era for smallsats in the commercial market. In reality, increasingly reliable technology and
permissive regulation have enabled ambitious constellation projects that could threaten the
telecommunications industry and claim a non-negligible share of the emerging markets. This report
surveys the technical and entrepreneurial landscape and uses these insights to develop future
adoption scenarios for smallsats in key commercial applications. !
Silicon Valley is the locus of space entrepreneurship activity. From here, we observe
the following:
• smallsat companies want to provide worldwide internet access!
• smallsat companies are shaping a new wireless architecture!
• smallsat companies aim at providing cheaper data, voice and instant messaging services in remote areas!
• legacy satellite operators want to compete with cellular offers to provide connectivity to connected
cars, aircraft, and the Internet of Things ecosystem!
• satellite antenna manufacturers are bringing smaller, cheaper, more agile, and embedded antennas to
fit the market’s need for more mobility and capacity in order to allow for these applications.
1. Micro satellites, defined as satellites under 100kg, are becoming more widely used due to their lower cost and shorter development time compared to large satellites. They are well suited for new entrants to the space industry and developing human resources.
2. Japan has launched several micro satellites for technology demonstrations including the SDS and CubeSat series. Other notable Japanese micro satellites include WNISAT-1 for Arctic observation and Axel Globe's proposed constellation. Internationally, companies like Planet Labs and OneWeb are developing large micro satellite constellations.
3. Future visions include using large micro satellite constellations to provide global internet access and solve the digital divide issue, particularly in developing countries. Japan
This document presents the results of Screw Driving Sounding (SDS) tests conducted at two sites in Malaysia and compares the SDS data to Standard Penetration Test (SPT) and Mackintosh Probe Test (MPT) data. At a site in Batu Pahat, SDS data correlated well with SPT data, with a coefficient of determination (R2) of 0.721. At a site in Cheras, SDS data correlated well with MPT data, with an R2 of 0.851. The preliminary findings suggest SDS testing has potential for soil characterization in site investigations in Malaysia.
The document discusses different types of orbits used by satellites, including low Earth orbit (LEO), medium Earth orbit (MEO), and geosynchronous orbit (GEO). It then focuses on using LEO satellites to provide affordable, high-speed internet access globally. Several companies are working on large LEO satellite constellations, including SpaceX, OneWeb, Amazon, and Kepler Communications. These companies face hurdles such as meeting service expectations, ensuring satellite reliability, managing space debris, addressing economic uncertainties, and navigating regulation.
The new thrust in the Indian space program aims to harness space technology for national development through various applications and infrastructure. Key goals include supporting socioeconomic development through services like remote sensing, communications, and navigation. The program also seeks to enhance capacity building, increase industry participation, and expand international cooperation. Recent accomplishments demonstrate increased satellite throughput, with ISRO successfully launching over 30 missions in the last three years. The organization is working to further scale up production capabilities and transition more activities to Indian industries.
The document outlines the BIRDS (Joint Global Multi-Nation Birds) project, which aims to build and launch a constellation of 1U CubeSats from five countries including Mongolia and Japan. The project will provide hands-on engineering experience for students and help non-space faring countries enter the space field. It details the satellite design, integration and testing process, ground station setup, operations plan and timeline, with a total cost of around $100,000 USD per satellite.
The document discusses the Square Kilometre Array (SKA) radio telescope project. It provides background on the SKA science drivers and vision to build the largest radio telescope in the world over multiple phases and sites. It describes the SKA organization, design consortia working on different components, notional data flow, and use of agile practices for developing the large amount of software and systems required. The document advocates for taking an agile approach to systems engineering to provide value throughout the telescope's design, construction, and operations.
This document proposes designs for two types of commercial space stations that could be built using modular construction in low Earth orbit within the next 5-10 years. The stations would be assembled from modules launched by SpaceX's Falcon Heavy rocket. Each module would weigh approximately 16 metric tons and provide living/working space. The stations could support activities like research, manufacturing, and space tourism. The total estimated cost to construct either station design is $12.1 billion, though financing and achieving an adequate return on investment present challenges.
This technical report describes the design and development of a waypoint-based rover prototype for coastal surveillance. The objectives are to develop a waypoint system suitable for coastal monitoring using a rover that can move across various surfaces and validate its operational capabilities. The prototype rover is equipped with a GPS, magnetometer, and wireless communication to set waypoints and receive instructions via an Arduino microcontroller. It is intended to improve existing coastal monitoring tools by allowing autonomous operation along preset routes.
C1.01: GOOS: an essential collaborative system enabling societal benefit - Jo...Blue Planet Symposium
A sustained ocean observing system forms a basis, along with capacity development, enabling societal benefit from ocean information. The Global Ocean Observing System (GOOS) is driven by societal requirements, including:
- adapting to and mitigating climate variability and change
- preparing for ocean-related hazards and supporting development of the ocean economy, and
- monitoring and promoting stewardship of ocean health.
GOOS is a key contributor to the GEO Blue Planet task. We are a collaborative programme, connecting a community and organizations working on many aspects of a Framework for Ocean Observations: identifying requirements focused on Essential Ocean Variables, coordinating observing networks and monitoring progress towards targets, and connecting to data and information generation activities that create scientific and societal value.
At the global level, these processes are led by three GOOS Panels focused on physics, biogeochemistry, and biology. The panels evaluate the readiness of the observing system, promoting strategic investment by identifying what is essential, and encouraging the development of new capabilities. They work closely with the ocean observing community. A Strategic Mapping is helping to identify how elements integrate into the system. GOOS development projects are evaluating and where necessary will improve and change parts of the sustained ocean observing system.
The combined satellite and in situ observing networks contributing to GOOS have strengthened in recent years.
At the regional level, GOOS Regional Alliances individually focus on local priorities and requirements. Collectively, they work to develop institutional and human capacity to make and benefit from sustained ocean observations.
GOOS both supports and relies on many partners, including other contributors to the GEO Blue Planet, in seeking to sustain present observations, while integrating new essential ocean observations into a sustained observing system.
Nanosatellite industry overview updated 022014Meidad Pariente
This document provides an overview of the nanosatellite industry as of February 2014. It discusses trends in the industry, including increasing commercialization and constellation deployments. The success rate of nanosatellite missions has increased to over 80% in recent years. While early missions faced reliability issues, components are now very reliable and most failures are due to workmanship errors during assembly. The future of the industry is predicted to include more advanced technologies, commercial dominance over educational projects, and thousands of nanosatellites being launched in the coming years to support various applications.
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Build the Next Generation of Apps with the Einstein 1 Platform.
Rejoignez Philippe Ozil pour une session de workshops qui vous guidera à travers les détails de la plateforme Einstein 1, l'importance des données pour la création d'applications d'intelligence artificielle et les différents outils et technologies que Salesforce propose pour vous apporter tous les bénéfices de l'IA.
Sri Guru Hargobind Ji - Bandi Chor Guru.pdfBalvir Singh
Sri Guru Hargobind Ji (19 June 1595 - 3 March 1644) is revered as the Sixth Nanak.
• On 25 May 1606 Guru Arjan nominated his son Sri Hargobind Ji as his successor. Shortly
afterwards, Guru Arjan was arrested, tortured and killed by order of the Mogul Emperor
Jahangir.
• Guru Hargobind's succession ceremony took place on 24 June 1606. He was barely
eleven years old when he became 6th Guru.
• As ordered by Guru Arjan Dev Ji, he put on two swords, one indicated his spiritual
authority (PIRI) and the other, his temporal authority (MIRI). He thus for the first time
initiated military tradition in the Sikh faith to resist religious persecution, protect
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• He had a long tenure as Guru, lasting 37 years, 9 months and 3 days
Determination of Equivalent Circuit parameters and performance characteristic...pvpriya2
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Historically, mechanical engineering has relied heavily on human expertise and empirical methods to solve complex problems. With the introduction of computer-aided design (CAD) and finite element analysis (FEA), the field took its first steps towards digitization. These tools allowed engineers to simulate and analyze mechanical systems with greater accuracy and efficiency. However, the sheer volume of data generated by modern engineering systems and the increasing complexity of these systems have necessitated more advanced analytical tools, paving the way for AI.
AI offers the capability to process vast amounts of data, identify patterns, and make predictions with a level of speed and accuracy unattainable by traditional methods. This has profound implications for mechanical engineering, enabling more efficient design processes, predictive maintenance strategies, and optimized manufacturing operations. AI-driven tools can learn from historical data, adapt to new information, and continuously improve their performance, making them invaluable in tackling the multifaceted challenges of modern mechanical engineering.
Open Channel Flow: fluid flow with a free surfaceIndrajeet sahu
Open Channel Flow: This topic focuses on fluid flow with a free surface, such as in rivers, canals, and drainage ditches. Key concepts include the classification of flow types (steady vs. unsteady, uniform vs. non-uniform), hydraulic radius, flow resistance, Manning's equation, critical flow conditions, and energy and momentum principles. It also covers flow measurement techniques, gradually varied flow analysis, and the design of open channels. Understanding these principles is vital for effective water resource management and engineering applications.
We have designed & manufacture the Lubi Valves LBF series type of Butterfly Valves for General Utility Water applications as well as for HVAC applications.
Digital Twins Computer Networking Paper Presentation.pptxaryanpankaj78
A Digital Twin in computer networking is a virtual representation of a physical network, used to simulate, analyze, and optimize network performance and reliability. It leverages real-time data to enhance network management, predict issues, and improve decision-making processes.
An In-Depth Exploration of Natural Language Processing: Evolution, Applicatio...DharmaBanothu
Natural language processing (NLP) has
recently garnered significant interest for the
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language. Its applications span multiple domains such
as machine translation, email spam detection,
information extraction, summarization, healthcare,
and question answering. This paper first delineates
four phases by examining various levels of NLP and
components of Natural Language Generation,
followed by a review of the history and progression of
NLP. Subsequently, we delve into the current state of
the art by presenting diverse NLP applications,
contemporary trends, and challenges. Finally, we
discuss some available datasets, models, and
evaluation metrics in NLP.
Prediction of Electrical Energy Efficiency Using Information on Consumer's Ac...PriyankaKilaniya
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Particle Swarm Optimization–Long Short-Term Memory based Channel Estimation w...IJCNCJournal
Paper Title
Particle Swarm Optimization–Long Short-Term Memory based Channel Estimation with Hybrid Beam Forming Power Transfer in WSN-IoT Applications
Authors
Reginald Jude Sixtus J and Tamilarasi Muthu, Puducherry Technological University, India
Abstract
Non-Orthogonal Multiple Access (NOMA) helps to overcome various difficulties in future technology wireless communications. NOMA, when utilized with millimeter wave multiple-input multiple-output (MIMO) systems, channel estimation becomes extremely difficult. For reaping the benefits of the NOMA and mm-Wave combination, effective channel estimation is required. In this paper, we propose an enhanced particle swarm optimization based long short-term memory estimator network (PSOLSTMEstNet), which is a neural network model that can be employed to forecast the bandwidth required in the mm-Wave MIMO network. The prime advantage of the LSTM is that it has the capability of dynamically adapting to the functioning pattern of fluctuating channel state. The LSTM stage with adaptive coding and modulation enhances the BER.PSO algorithm is employed to optimize input weights of LSTM network. The modified algorithm splits the power by channel condition of every single user. Participants will be first sorted into distinct groups depending upon respective channel conditions, using a hybrid beamforming approach. The network characteristics are fine-estimated using PSO-LSTMEstNet after a rough approximation of channels parameters derived from the received data.
Keywords
Signal to Noise Ratio (SNR), Bit Error Rate (BER), mm-Wave, MIMO, NOMA, deep learning, optimization.
Volume URL: https://airccse.org/journal/ijc2022.html
Abstract URL:https://aircconline.com/abstract/ijcnc/v14n5/14522cnc05.html
Pdf URL: https://aircconline.com/ijcnc/V14N5/14522cnc05.pdf
#scopuspublication #scopusindexed #callforpapers #researchpapers #cfp #researchers #phdstudent #researchScholar #journalpaper #submission #journalsubmission #WBAN #requirements #tailoredtreatment #MACstrategy #enhancedefficiency #protrcal #computing #analysis #wirelessbodyareanetworks #wirelessnetworks
#adhocnetwork #VANETs #OLSRrouting #routing #MPR #nderesidualenergy #korea #cognitiveradionetworks #radionetworks #rendezvoussequence
Here's where you can reach us : ijcnc@airccse.org or ijcnc@aircconline.com
Accident detection system project report.pdfKamal Acharya
The Rapid growth of technology and infrastructure has made our lives easier. The
advent of technology has also increased the traffic hazards and the road accidents take place
frequently which causes huge loss of life and property because of the poor emergency facilities.
Many lives could have been saved if emergency service could get accident information and
reach in time. Our project will provide an optimum solution to this draw back. A piezo electric
sensor can be used as a crash or rollover detector of the vehicle during and after a crash. With
signals from a piezo electric sensor, a severe accident can be recognized. According to this
project when a vehicle meets with an accident immediately piezo electric sensor will detect the
signal or if a car rolls over. Then with the help of GSM module and GPS module, the location
will be sent to the emergency contact. Then after conforming the location necessary action will
be taken. If the person meets with a small accident or if there is no serious threat to anyone’s
life, then the alert message can be terminated by the driver by a switch provided in order to
avoid wasting the valuable time of the medical rescue team.
Tools & Techniques for Commissioning and Maintaining PV Systems W-Animations ...Transcat
Join us for this solutions-based webinar on the tools and techniques for commissioning and maintaining PV Systems. In this session, we'll review the process of building and maintaining a solar array, starting with installation and commissioning, then reviewing operations and maintenance of the system. This course will review insulation resistance testing, I-V curve testing, earth-bond continuity, ground resistance testing, performance tests, visual inspections, ground and arc fault testing procedures, and power quality analysis.
Fluke Solar Application Specialist Will White is presenting on this engaging topic:
Will has worked in the renewable energy industry since 2005, first as an installer for a small east coast solar integrator before adding sales, design, and project management to his skillset. In 2022, Will joined Fluke as a solar application specialist, where he supports their renewable energy testing equipment like IV-curve tracers, electrical meters, and thermal imaging cameras. Experienced in wind power, solar thermal, energy storage, and all scales of PV, Will has primarily focused on residential and small commercial systems. He is passionate about implementing high-quality, code-compliant installation techniques.
2. 2Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
2014 Nano / Microsatellite Market Assessment
Developed by:
Ms. Elizabeth Buchen
Director, Engineering Economics Group
elizabeth.buchen@sei.aero | 1+770.379.8006
Mr. Dominic DePasquale
Space Ventures Specialist
dominic.depasquale@sei.aero | 1+770.379.8009
Published by:
SpaceWorks Enterprises, Inc. (SEI)
Atlanta, GA
3. 3Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
SpaceWorks’ 2013 Projection estimated 93 nano/
microsatellites would launch globally in 2013; 92 nano/
microsatellites actually launched, an increase of 269% over
2012
2013
2014+
SpaceWorks’ 2014 Projection reflects a significant increase in
the quantity of future nano/microsatellites needing a launch.
This year’s projection is 2-3 times higher than our 2013
projection in the later years (2017 – 2020), which is driven by
the emergence and continued growth of commercial players in
the 1-50 kg satellite market.
4. 4Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
2014 Nano/Microsatellite Market Assessment Overview
§ The data source for this study is the SpaceWorks Satellite Launch Demand Database (LDDB)
• The LDDB is an extensive database of all known historical (2000 – 2013) and future (2014+) satellite
projects with masses between 0 kg and 10,000+ kg
• Currently 650 future (2014 – 2016) nano/microsatellites (1 – 50 kg) in the LDDB (focus of this study)
• Currently 48 future (2014+) picosatellites (< 1 kg) in the LDDB (not included in this study)
§ SpaceWorks has projected global launch demand in the nano/microsatellite market according to a
Gompertz logistic curve from 2014 to the year 2020
• Note that SpaceWorks places no value judgment on whether developers will successfully meet
their announced launch date or not
§ The nano/microsatellite projection was developed from a combination of two data sets
• Publicly announced nano/microsatellite projects and programs
• Quantitative and qualitative adjustments to account for the expected sustainment of current projects and
programs (e.g. follow-on to EDSN, CubeSat Launch Initiative), as well as the continued emergence and
growth of numerous existing commercial companies
Projections indicate substantial growth in nano/microsatellite launches, with an estimated range of 410 to
543 nano/microsatellites (1-50 kg) that will need launches globally in 2020 (compared to 92 in 2013)
5. 5Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Nano/Microsatellite Definitions and Terminology
§ Many nanosatellites are based on the
“CubeSat” standard
• Developed in by California Polytechnic State
University and Stanford University in 1999
• Consists of any number of 10 cm x 10 cm x 10
cm units
• Each unit, or “U”, usually has a volume of
exactly one liter
• Each “U” has a mass close to 1 kg and not to
exceed 1.33 kg (e.g. a 3U CubeSat has mass
between 3 and 4 kg)
§ This study limits the upper end of microsatellite
mass to 50 kg given the relative large amount
of satellite development activity in the 1-50 kg
range by comparison to the 50-100 kg range.
Satellite Class Mass Range
Femtosatellite 10 – 100 g
Picosatellite < 1 kg
Nanosatellite 1 – 10 kg
Scope of this study 1 – 50 kg
Microsatellite 10 – 100 kg
Small Satellite 100 – 500 kg
Aalborg University’s
AAUSAT4 CubeSat
6. 6Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Nano/Microsatellite Applications and Associated Examples
Scientific Research
Phonesat 1.0
Mass: 1 kg
Launched: 4/2013
Technology
SwampSat
Mass: 1.2 kg
Launched: 11/2013
Earth Observation
Dove 2
Mass: 5.5 kg
Launched: 4/2013
Education
ArduSat
Mass: 1 kg
Launched: 8/2013
Military Application
SENSE-1
Mass: 5 kg
Launched: 11/2013
Astronomy
BRITE-PL
Mass: 7 kg
Launched: 11/2013
Credit: University of Florida Credit: Planet LabsCredit: http://www.nasa.gov/directorates/spacetech/small_spacecraft/phonesat.html
Credit: http://www.dk3wn.info/sat/afu/sat_ardusat.shtml Credit: USAF/SMC
7. 7Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
302
344
380
410
436
487
521
543
0
100
200
300
400
500
600
2009
2010
2011
2012
2013
2014
2015
2016
2017
2018
2019
2020
NumberofSatellites
(1-50kg)
Calendar Year
Full Market Potential
SpaceWorks Projection
Historical Launches
Nano/Microsatellite Launch History and Projection (1 - 50 kg)
* Please see End Notes 1, 2, 4, 5, and 6.
The Full Market Potential dataset is a combination of publically announced launch intentions, market research, and qualitative/quantitative assessments to account for future activities and programs.
The SpaceWorks Projection dataset reflects SpaceWorks’ expert value judgment on the likely market outcome.
Projections based on announced and future plans of developers and programs indicate
between 2,000 and 2,750 nano/microsatellites will require a launch from 2014 through 2020
8. 8Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
0
100
200
300
400
500
600
700
* Assumes two NSF Geospace & Atmospheric CubeSat satellites selected in 2014. NASA CubeSat Launch Initiative total includes the sixteen
missions chosen in February 2014 (in response to August 2013 Announcement of Opportunity) and the timeframe listed is based on when the
already selected CubeSats are scheduled to launch. QB50 total includes two precursor satellites.
Please see End Notes 2, 3, 4, 6, and 7.
Nano/Microsatellite Future Program Summary (1 – 50 kg)
Name of Program/
Satellite Constellation
Timeframe Organization Country Mass (kg)
Launched
to Date
Total
Planned
NSF Geospace &
Atmospheric CubeSat
2010-2015 NSF USA 1-3 7 13
NASA EDSN 2013-2014 NASAARC USA 3 0 8
NASA CubeSat
Launch Initiative
2011-2017 NASA USA 1-12 24 115
SeeMe Payloads 2016 DARPA USA 12 0 6
QB50 2015
Von Karman
Institute /
Various
Various 2 0 52
HUMSAT 2013-2014
University of
Vigo / Various
Various 1 0 9
QB50
HUMSAT
Commercial
(USA)
Other
(Foreign)
SeeMe
NSF
EDSN
CSLI
Other
Programs,
75%
Existing
Large
Programs,
25%
Existing large programs will comprise only 25% of future
nano/microsatellites (compared to 65% in 2013) due to
worldwide growth in the civil and commercial sectors
SpaceWorks Projection
(2014 – 2016)
Large Program Breakdown for Announced Future Satellites
Other
(USA)
NumberofSatellites
(1-50kg)
9. 9Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
3 22
10
366
26
38
88
224
0%
10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
NumberofSatellitesNano/Microsatellite Trends by Sector (1 – 50 kg)
Commercial sector
will contribute
56% of future nano/
microsatellites
Civil
Government
Commercial
Defense/Intelligence
Historical
(2009 – 2013)
SpaceWorks Projection
(2014 – 2016)
* Please see End Notes 2, 6, 7, and 8.
The civil sector remains strong, contributing over one third of future nano/microsatellites,
but it will see reductions compared to 2009-2013 when the sector contributed 63%
10. 10Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Nano/Microsatellite Trends by Purpose (1 – 50 kg)
Technology
Communications
Communications
Total: 202
Historical
(2009 – 2013)
SpaceWorks
Projection
(2014 - 2016)
2%
12%
21%
10%
55%
Reconnaissance
2%
52%
17%
9%
20%
Technology
Scientific
Earth Observation/
Remote Sensing
Reconnaissance
Scientific
Earth Observation/
Remote Sensing
Total: 650
* Please see End Notes 2, 6, and 7.
A smaller proportion of technology development/demonstration nano/microsatellites
will be built in the next few years (20% vs. 55% from 2009 to 2013)
Over half of future nano/microsatellites will be used for
Earth observation and remote sensing purposes (compared to 12% from 2009 to 2013)
11. 11Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%
Percentage Contribution
Nanosatellite Size Trends (1 - 10 kg)
Historical
(2009 – 2013)
SpaceWorks
Projection
(2014 – 2016)
25%
1 kg 3 kg2 kg 4 kg 5 kg 6 kg 7 kg 8 kg 9 kg 10 kg
3%
1 kg 3 kg2 kg 4 kg 5 kg 6 kg 7 kg 8 kg 9 kg 10 kg
* Please see End Notes 2, 6, 7, and 9.
1U (1 kg) CubeSats, while still immensely popular, will comprise less of the market in the
future (35% of future nanosatellites compared to 47% from 2009 to 2013)
25% of future nanosatellites (1-10 kg) are in the increasingly popular 6 kg mass class
(compared to only 3% from 2009 to 2013)
12. 12Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
0
10
20
30
40
50
60
70
80
90
100
2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013
NumberofSatellites
Calendar Year
Historical Nano/Microsatellites Launched: 2000 - 2013 (1 - 50 kg)
1 – 10 kg
11 – 50 kg
A 330% increase in attempted nanosatellite (1-10 kg) deliveries in 2013,
compared to 2012, shows signs of an emerging and growing launch market
Significant growth
in the 1-10 kg
mass range
* Please see End Notes 1 and 2.
13. 13Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Historical Nano/Microsatellite Trends by Launch Vehicle (2000 - 2013)
Launch Vehicle
No. of
Satellites
No. of
Launches
Percentage of
Satellites Launched
Kosmos-3M 50 6 20%
Dnepr-1 34 4 14%
Minotaur I 34 4 14%
PSLV 21 6 9%
H-2 18 5 7%
Space Shuttle 12 6 5%
Falcon 9 11 2 4%
Soyuz 9 5 4%
Delta II 8 3 3%
Long March 7 4 3%
Minotaur IV 8 1 3%
Vega 8 2 3%
Other 8 5 3%
Antares 4 1 2%
Atlas V 5 2 2%
Rokot-KM 6 1 2%
Falcon 1 2 1 1%
M-5 (2) 2 2 1%
Launch Vehicle
No. of
Satellites
No. of
Launches
Percentage of
Satellites Launched
Kosmos-3M 25 9 24%
Dnepr-1 9 2 9%
H-2 9 6 9%
Minotaur I 9 2 9%
PSLV 8 6 8%
Minotaur IV 7 5 7%
Safir 6 6 6%
Soyuz 6 6 6%
Long March 5 5 5%
Other 5 5 4%
Pegasus-XL 3 1 3%
Space Shuttle 3 2 3%
Delta IV Heavy 2 1 2%
KT-1 2 2 2%
Rokot-KM 2 2 2%
Atlas V 1 1 1%
Delta II 1 1 1%
Falcon 1 1 1 1%
Falcon 9 1 1 1%
Launch Vehicles: 2000-2013 for
1-10 kg Satellite Class
Launch Vehicles: 2000-2013 for
11-50 kg Satellite Class
Low cost piggy-back opportunities have historically attracted
small satellite payloads to international launch vehicles
* Please see End Note 2.
14. 14Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Emergence of Commercial Companies: 2013 Case Study
§ SpaceWorks released its annual nano/microsatellite
projections in February of 2013
• According to the projection, 93 satellites (1-50 kg)
were planning to launch in 2013
• 92 satellites (1-50 kg) actually launched in 2013
§ Based on the announced launch data alone, 2014
will see a 52% increase in nano/microsatellites
launched compared to 2013
§ Commercial companies will contribute over one-
fourth of all nano/microsatellites launched in 2014
• This is a significant increase from 2013, where the
commercial sector contributed only 11%
• The continued emergence and growth of commercial
Commercial Company Satellite Class Satellite Application
Dauria Aerospace Nano
Deep Space Industries Nano
GeoOptics, Inc. Micro
ISIS Nano/Micro
Outernet (MDIF) Nano
NanoSatisfi Nano
Planet Labs Nano
Planetary Resources, Inc. Nano/Micro
SpaceQuest, Ltd. Micro
companies (see table) will result in an even greater increase in 2015, with the sector contributing 60% of all nano/
microsatellites launched
§ Many companies have publicly revealed their near-term intentions regarding future launches of nano/
microsatellites and the satellites’ wide spectrum of revenue generating applications
§ Other companies have been more reserved, revealing only small details of their plans
Ship
Tracking
Asteroid
Exploration
Data
Collection
Earth Obs./
Remote Sensing
* Please see End Notes 2, 4, 6, 7, and 10.
Precise quantities aside, strong evidence suggests the commercial sector will
have a meaningful and enduring impact on the nano/microsatellite industry
15. 15Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
2014 Nano/Microsatellite Market Assessment Conclusions
§ The nano/microsatellite market is growing tremendously with the continued use of the CubeSat standard,
microelectronics and other technology development, government programs, and furthering of applications
§ The civil sector remains strong, but the eruption of commercial companies and start-up activities will
continue to influence the nano/microsatellite market; future launches suggest this trend will continue
§ Projections based on both announced and anticipated plans of developers indicate 2,000 – 2,750 nano/
microsatellites will require a launch from 2014 through 2020
§ Nano/Microsatellite CAGR (Compound Annual Growth Rate):
• Historical average growth of 37.2% per year over the last 4 years (2009 – 2013)
• SpaceWorks’ Projection Dataset shows average growth of 23.8% per year over the next 6 years (2014 – 2020)
§ While 1U (1 kg) CubeSats are still widely used, 25% of future nanosatellites (1-10 kg) are in the increasingly
popular 6 kg mass class
§ Applications for nano/microsatellites are diversifying, with increased use in the future for Earth observation and
remote sensing missions
* Please see End Notes 2, 4, 5, 6, and 7.
16. 16Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
Custom analyses and more detailed assessments are
available from SpaceWorks for nano/microsatellites
and larger satellite classes
For additional information or to request a quote,
please contact:
Ms. Elizabeth Buchen
Director, Engineering Economics Group
1+770.379.8006
elizabeth.buchen@sei.aero
17. 17Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
End Notes
1. The number of satellites may not equal the number of launches since many small satellites are multiple-manifested (i.e. more than one satellite co-
manifested on a particular launch vehicle). Historical data includes failed launch attempts.
2. The data used throughout this presentation (both historical and future) may not represent all global nano/microsatellite activities.
3. All NSF satellites thus far have launched through the NASA CSLI. In the table, these historical NSF satellites are included in both the count of
number launched for NSF and the count for CSLI (double counted in this sense). The bar graph of future launches shows only those NSF satellites
that expected, but currently not manifested (thus they are appropriately single counted for future launches).
4. The SpaceWorks Projection and Full Market Potential datasets include some known nano/microsatellite programs for which a specific launch date
has not been announced. The satellites belonging to these programs are distributed across the period (date range) for launches according to the
announced program objectives
5. Future projections from 2017-2020 are determined by Gompertz logistic curve “best fit” regression with market saturation point (asymptote for
number of satellites) set at 525 nano/microsatellites in a year for the SpaceWorks Projection dataset and 580 for the Full Market Potential dataset.
6. The Full Market Potential dataset contains all currently known past and future nano/microsatellites from the SpaceWorks LDDB, with the addition of
an inflating factor for known unknowns plus assumed sustainment of certain current projects and programs (e.g. follow-on to NASAAmes EDSN,
CubeSat Launch Initiative, DARPA SeeMe) and the continued emergence and growth of numerous existing commercial companies. The
SpaceWorks Projection dataset reflects SpaceWorks’ expert value judgment on the likely market outcome.
7. These graphs are based on the SpaceWorks Projection dataset only, and do not include the additional satellites contained in the Full Market
Potential dataset.
8. By some traditional definitions of space industrial sectors, non-defense government space activities are a subsector of the civil sector. Here we
break out non-defense government activities into a separate sector. “Government” refers to those nano/microsatellite development efforts that occur
within/by the government agency or organization (e.g. NASA, JAXA). Civil refers to all other non-defense development activities (e.g. universities,
federally funded research institutions), though the funding source may be a government agency.
9. Nanosatellites are binned by rounding mass to the nearest whole number. Picosatellites less than 1 kg are not included.
10. Satellite application images are credited to the following websites: http://sweetclipart.com/colorable-earth-line-art-709,
http://www.clker.com/clipart-binary-data.html, http://hasloo.com/freecliparts/?p=520, http://bestclipartblog.com/24-ship-clip-art.html.
18. 18Copyright 2014, SpaceWorks Enterprises, Inc. (SEI)
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