Considerations for Eco-LeanSat Satellite Manufacturing and Recycling
Abstract
:1. Introduction
- Eco-design: addressing environmental impacts and fostering green technologies;
- Space debris mitigation: minimizing the production of space debris;
- On-orbit servicing/ADR: removing spacecraft from orbit and demonstrating on-orbit servicing of spacecraft.
2. Sustainability Concept: Implementing a Zero Debris Approach
2.1. The Zero Debris Approach
Implementation Strategy
- ESA Policy Evolution: Recognizing the need for policy alignment with international guidelines, the ESA is updating its policy to incorporate short-term zero debris recommendations. This stepwise approach aims to achieve zero debris by 2030.
- Upgrade Platforms: Efforts are underway to enhance spacecraft platforms by integrating end-of-life technologies effectively. Key technology developments include deorbiting systems, passivation functions, design for demise, and design for removal.
- Removal Services: ESA is actively developing removal services, including technology development, missions, and standards. Embedding removal interfaces in Copernicus Expansion missions is a crucial step towards fail-safe debris disposal.
- Improved Operations: Enhancing space surveillance and tracking, space traffic coordination, collision avoidance, and close-proximity operations is essential for a successful zero debris implementation. The ESA engages with stakeholders through workshops to enhance satellite operations in these critical areas.
- Goal 1: Develop a Framework for Assessing Space Sustainability at NASANASA intends to develop an entity relationship model that specifies all quantities of interest and their interdependencies, which will be operationalized through measurements, modeling, and assessments. This approach will aid with defining the existing space traffic and debris environment, developing metrics to assess the long-term viability of orbital activities, and establishing goal values for these metrics. The goals are to define the framework, determine tolerable and desired risk levels, and publicize NASA’s influence on space sustainability on an annual basis.
- Goal 2: Prioritize Efficient Ways to Minimize UncertaintiesUsing the methodology developed, NASA will identify important uncertainties that pose hazards to robotic spacecraft as well as study the effects of orbiting objects on scientific observations and devise cost-effective solutions to eradicate potential negative effects. The goals include identifying opportunities for breakthrough improvements in sensing and anticipating the operating environment, exploring new operational approaches, and developing prioritized approaches to managing current debris challenges.
- Goal 3: Lower Barriers to Space Sustainability Through Technology Development and TransferBased on the lessons gathered from Goal 2, NASA will invest in technologies that promote space sustainability. These expenditures will enhance the capabilities required for long-term operations in Earth’s orbit and will help other U.S. space operators. The goals include investing in early-stage orbital debris management, expanding investments in space situational awareness and traffic coordination, and facilitating debris-related technological demonstrations with possible transition partners.
- Goal 4: Update or Develop Policies to Support Space SustainabilityNASA will improve space sustainability via policy modifications and advancements. The objectives include updating NASA’s rules and standards based on the results of prior goals, amending debris remediation policies, supporting economic and policy research on space sustainability, and resolving international orbital debris remediation challenges.
- Goal 5: Improve Coordination and Collaboration Outside of NASANASA will continue to lead both domestically and internationally by exploring opportunities for increased information sharing and collaboration with academic institutions, industry, interagency partners, and the global space community. The objectives include collaborating with interagency partners, interacting with space-sustainability-focused communities, exchanging best practices and tools, and capitalizing on technology advancements from the greater space community.
- Goal 6: Enhance NASA’s Internal Organization to Support Space SustainabilityNASA will establish an entity to supervise the day-to-day coordination and accountability for the agency’s space sustainability activities. This organization will guarantee that NASA meets its sustainability goals, prioritizes related work and funding, and maintains a consistent voice in space sustainability issues.
2.2. Towards a Sustainable Orbital Environment
- Manufacturing (comprising components, subsystems, and system integration): It is essential to highlight the advances made in ISO standards for small satellites. The ISO/TC20/SC14 committee [64] began efforts in 2014 to produce standards that define and regulate the use of small satellites, resulting in work item ISO/WD/20991, “Requirements for Small Spacecraft” [65]. This standard seeks to lay the groundwork for the responsible deployment and operation of tiny satellites, with a focus on sustainability and space debris mitigation. In March 2016, the study group presented a report to the IAA, concluding that small satellites should be identified by their design and management philosophy, not their size. The term “lean satellite” has been used to describe satellites that use creative, low-cost ways to enable rapid delivery with small teams. The group developed a scaling system to measure adherence to the lean satellite concept, which was tested on nearly 30 satellites worldwide [66]. In 2019, the Kyushu Institute of Technology (Kyutech), with Japanese government assistance, launched a project to standardize the CubeSat electrical interface [67]. This initiative uses the lean satellite community to get worldwide feedback and build the standard. Activities include editing drafts, coordinating with ISO/TC20/SC14, and organizing international workshops. The standard document, “Space Systems—CubeSat Interface”, is currently being developed. This standard specifies the interface and the documentation required to enable integration and reduce compatibility difficulties, resulting in a substantially shorter process of selecting and testing CubeSat components.
- Operations (involving launch providers and services, space operations, and the ground segment).
- Change of applications.
- Life Extension: A novel proposal that takes into account future missions and emerging technologies. This phase involves evaluating satellite health and operational status in orbit. In case of any failure, two options are considered: (1) in-orbit repair through activities such as rendezvous and docking or (2) active debris removal (ADR), which includes the sustainable waste management techniques mentioned earlier. This proposal also addresses a sustainable final disposal system and the potential for reusing materials for other missions.
- Deep Space Exploration: Enabling the execution of missions that venture beyond Earth’s orbit, thereby expanding the scope of space exploration capabilities.
- Autonomous Removal and Earth Re-Entry: Simplifying the process of retiring satellites at the end of their operational life, either through mechanical structures or autonomous means, thereby contributing to the reduction of space debris and facilitating payload recovery.
- Autonomous Rendezvous Operations: Equipping satellites with the capability to autonomously approach and engage with cooperative or non-cooperative objects in the vastness of space.
- Conducting Experiments: Enabling the broadening of our knowledge and the enhancement of our capabilities across various scientific domains.
- Multi-Satellite Missions: This encompasses the deployment of satellite constellations and fractionated missions [69] that provide extended coverage and increased operational redundancy.
- In-Orbit Manufacturing and Assembly: The ability to craft components or conduct assembly in the space environment, thereby reducing reliance on Earth-based resources and adapting to unforeseen circumstances.
- Satellite Recycling: The potential to recover and repurpose satellites, thereby contributing to cost reduction and the mitigation of space debris concerns.
- Secure Cryptographic Keys: Leveraging the unique quantum properties of light and onboard intelligence to secure space-based communications.
- Active Maneuvers: Empowering satellites to execute more efficient attitude control and optimize their positioning with regard to factors such as solar exposure, darkness, Earth orientation, and more.
- On-Orbit Operations: The capacity to carry out updates to software and hardware while in orbit, ultimately enhancing satellite flexibility and longevity. OSS facilitates the extension of satellite lifespans by allowing for inspection, refueling, maintenance, and upgrades, which improves the performance and return on investment (ROI). It promotes space sustainability by reusing, refurbishing, and recycling materials while also reducing orbital congestion through deorbiting technology and prolonged satellite lifetimes: hence, reducing the demand for new launches. However, current OSS technologies face several challenges, including the lack of a successful demonstration track record, an insufficient legal framework to address liability issues, the cost-effectiveness of replacing satellites versus servicing them, and the need for industry consensus on interoperability standards. Furthermore, the dual-use nature of ISAM technology raises concerns about anti-satellite capabilities, which could jeopardize space sustainability initiatives [70].
2.3. Efforts towards a Sustainable Supply Chain
2.3.1. Highlighting Progress in Applying This Concept
2.3.2. Challenges
2.4. What Actions Can Be Taken Today with Existing Space Debris?
3. Eco-LeanSat Proposal
3.1. Preliminary Context of SmallSat Capability Evolution
3.2. First Period: Early Development of Small Satellites and CubeSats (1999–2003)
- (a)
- (b)
- In 2002, JAXA launched three satellites, two of which were small. The first of these, TSUBASA (MDS-1), was designed to verify the necessary technologies in space based on three keywords: faster operation, lower cost, and increased reliability [119]. The satellite demonstrated primary data collection, allowing scientists to experiment before implementing the payloads in larger satellites. Additionally, the satellite contained complex parts developed by the industry to assess their performance and produce smaller and lighter components at a lower cost. The second satellite was a small research satellite that established small satellite spin bus technologies and offered opportunities for in-space verification [119]. This satellite was unique in the sense that it was “handmade” and was fabricated mainly by young JAXA engineers. The project served as a test case to produce small satellites more efficiently and at a reduced cost.Israel has also explored other types of military small satellites. The Ofeq 5 series was part of the Israeli spy optical surveillance satellites [120]. The first launch of this CubeSat was made on June 20, 2003 [121], in Plesetsk, Russia, on a Eurockot rocket using Russia’s Multiple Mission Orbit Service. The Ofeq series have retrograde orbits due to Israel’s Mediterranean launch path, and they are an upgraded version of the initial Ofeq reconnaissance satellites, which were similar to EROS-A.A group of CubeSats was launched into a sun-synchronous orbit, which included the Danish AAU CubeSat and DTUSat, Japanese XI-IV and CUTE-1, Canadian Can X-1, and Quakesat. The latter used a series of low-frequency ground sensors designed to detect the energy emitted in the LF part of the electromagnetic spectrum before an earthquake occurs [122].
3.3. Second Period: Technology Demonstrations (2004–2009)
- (a)
- In 2005, Japan launched an optical in-orbit communications engineering test satellite called “KIRARI”. This satellite had a large-aperture telescope, a high-power semiconductor laser, and highly sensitive signal detectors. It allowed the testing of operations such as beam acquisition to capture an incoming laser beam, beam tracking to detect and control the angle of the incoming laser, and beam pointing to transmit a laser beam accurately in the right direction [123,124].
- (b)
- In 2006, NASA launched Genesat 1: a technology demonstration and biological experimentation mission. The satellite integrated a miniaturized life support system and a nutrient delivery system for a colony of Escherichia coli bacteria in order to track genetic changes under space conditions [125].
- (c)
- The Constellation of Small Satellites for Mediterranean Basin Observation (COSMO-SkyMed) was launched in 2007. Each satellite of the constellation is equipped with a SAR-2000: a multi-mode SAR (synthetic aperture radar) instrument with programmable swath size, spatial resolution, and polarization configurations. The SAR transmitter/receiver system operates with an electrically steerable multibeam antenna [126].
3.4. Third Period: Technology Demonstrations (2010–2014)
- (a)
- In 2011, ExactEarth acquired small satellites for commercial maritime applications [15]. SmallSat launches were primarily augmented with data transmission capabilities for communication or imaging applications [114]. Another significant milestone was the development of the international CubeSat-based QB50 mission led by the Von Karman Institute for Fluid Dynamics. QB50 consisted of a network of 50 CubeSats built by teams of students from universities around the world to conduct multipoint in situ measurements of the lower thermosphere [133,134].
- (b)
- In 2013, NanoRacks became the first commercial operator to launch from the International Space Station (ISS) [15]. In the same year, the Cosmogia company (now Planet Labs launched its first Dove pathfinder satellite (Dove 1) [15]. (Planet owns and operates a constellation of more than five hundred 3U imaging satellites with a spacial resolution of ~5 m [135,136].) Its goal was to show the performance of a small camera payload and demonstrate the ability to design, produce, and operate satellites in short times and at a low-cost using commercial off-the-shelf components [137]. Planet’s primary Earth observation payload is an electro-optical imaging system operating in the visible band and with a ground resolution of approximately 5 m. Its secondary payload is a low-resolution IR imaging system with a ground resolution of approximately 1 km [138].
- (c)
- A year later, Planet launched 93 additional satellites into orbit. Nearly simultaneously, Spire Global, a space-to-cloud data and analytics company, successfully deployed its first satellite model: the Lemur 1. This satellite was equipped with the STRATOS payload, which collects GNSS-RO (radio occultation) for various Earth observation applications, including climate and space weather research by Spire [15]. The Argentinean SAOCOM 1A (Satélite Argentino de Observación Con Microondas) constellation comprises two L-band synthetic aperture radar (SAR) satellites and offer crucial data for applications like measuring Earth surface changes, crop management, and flood monitoring [139,140].
3.5. Fourth Period: Novel Applications (2015–Present)
3.5.1. CubeSats: Global Advances and Scientific Applications from 2015 to 2018
- (a)
- In 2015, China launched the first quantum communications satellite together with 3Cat-2—the first CubeSat launched by the Universitat Politècnica de Catalunya (UPC), Spain. It was equipped with a GNSS-reflectometry payload [114].
- (b)
- Orbital ATK (now Northrop Grumman) successfully launched its first ISS resupply mission with the Cygnus spacecraft; it carried more than 20 satellites [15]. From 1999 to 2015, around 80% of all CubeSats were developed in the U.S. Japan launched 18 CubeSats, Germany launched 10, Denmark launched 9, and Italy, the UK, and South Korea launched 4 each. Since then, over 30 other countries have launched at least one CubeSat.
- (c)
- In 2016, the International Space Science Institute in Bern, Switzerland, organized a forum to study the evolution of CubeSats as enabling technology platforms. These institutions identified developments aimed at areas such as space physics, focusing on issues like radiation belt variability and complementing missions such as the Van Allen probes [141]. Additionally, in the fields of planetary sciences and astrophysics, research focused on describing new measurement techniques enabled by CubeSats.In this period, the CubeSat concept became a powerful tool. Because they can be launched easily, the revisit time can be reduced, and also, they can address specific scientific questions for which traditional satellite approaches are not suitable. In this period, space exploration was more accessible, and scientific and technological developments were encouraged in order to innovate satellite systems and their payloads. According to a study conducted by the U.S. National Academies of Sciences, Engineering, and Medicine, the most significant improvement during this time was the precise control of the CubeSat’s attitude [114]. Progress and developments in other satellite subsystems, such as solar panels, organic solar cells, hydrogen cells, and power sources [142], as well as the optimization of communication systems with larger data transmission rates [114], including deployable antennas, optical communications, and inter-satellite links, are noteworthy.
- (d)
- Similarly, between 2016 and 2018, important research efforts were directed towards propulsion technologies for small satellites, enabling them to achieve new scientifically valuable orbits for specialized experiments or to control their trajectories with other platforms. Plasma thrusters and ion engines designed for CubeSat-type structures have been developed [143,144], and today, thanks to these advances, notable projects like CAPSTONE (Cis-lunar Autonomous Positioning System Technology Operations and Navigation Experiment) [145] have successfully placed spacecraft in a near-rectilinear halo orbit (NRHO).Recent advances in satellite technology have prompted state policies owing to the high capacities developed in satellites. An example was the announcement on 21 October 2016 by the White House (U.S.) of the “Harnessing the Small Satellite Revolution” initiative, building on a growing wave of private sector interest in miniaturized spacecraft for applications ranging from remote sensing and communications to satellite inspection and repair. One of the opportunities that was raised was NASA’s purchase of up to USD 30 million of Earth observation data collected by small satellites and the creation of a new Small Spacecraft Virtual Institute based at the Ames Research Center in Silicon Valley and with the aim of documenting best practices, lessons learned, and standards for all phases of small-satellite development [146].In the same year, China launched the satellite Tianyuan-1: the country’s first in-space refueling system for orbital satellites [147]. Aolong-1 was the world’s first active orbital debris removal experimental project. It was equipped with a robotic arm to simulate the grabbing of abandoned satellites and other large pieces of debris in space and could take them to the atmosphere for burning during reentry [148].
- (e)
- In 2017, OneWeb inaugurated a modern satellite production facility, which increased the number of small satellite launches [15], and the Polar Satellite Launch Vehicle (PSLV)-37 program of the Indian Space Research Organization (ISRO) deployed a record number of 104 satellites in a single launch [15]. One year later, NASA’s Jet Propulsion Laboratory launched Mars Cube One (MarCO) [149]: a technology demonstration mission consisting of two 6U CubeSats, MARCO-A and MARCO-B, which were the first over-interplanetary CubeSats and acted as a data relay for the Mars InSight lander for a short period of time. The MarCO pair conducted communications and navigation while flying independently of the planet Mars [149].
- (f)
- In the same year, Sun-Synchronous Orbit (SSO)-A from SpaceFlight Industries carried 64 satellites from 17 countries into orbit [150].Regarding the development of new payloads, in 2017, the first Finnish satellite was launched, Aalto-1, with the Aalto Spectral Imager (AaSI): the first hyperspectral imaging system compatible with nanosatellites and the radiation monitor (RADMON) and electrostatic plasma brake (EPB) missions. The latter was a novel deorbiting technology that employed Coulomb drag between the ionospheric plasma and a long, charged tether [151,152,153]. A similar experiment was conducted on board ESTCube-1 [154,155].
- (g)
- In 2018, HyperScout-1 became the first hyperspectral imager for nanosatellites [156]. It is also relevant to mention the TUBSAT-1 mission (1991), which was one of the pioneering satellites for multi-purpose imagery (ocean and land) through the use of high-resolution optical imagers, data collection, and hyperspectral imagers [157].
3.5.2. Satellite Technology Breakthroughs: 2019–2020 Achievements and Developments
- (h)
- In 2019, Capella Space launched the world’s first sub-50 kg SAR satellite (Denali) for a technology demonstration mission. Later versions were designed to operate a constellation of 36 satellites. These satellites were equipped with an X-band SAR boasting a 0.5 m resolution, enabling all-weather imaging through an antenna spanning nearly 100 square feet. These satellites offer hourly images of any location on the surface of the Earth [158].AstroDigital launched the world’s first 16U CubeSat (Palisade) in the same year. It was a technology demonstration satellite with an onboard propulsion system [159]. Also, India developed the Cartosat-3 satellite, which provides very-high-resolution panchromatic imagery with a resolution of 0.28 m and multispectral imagery in four spectral bands with a spatial resolution of 1.12 m; it has a nominal swath of ~17 km.
- (i)
- In 2020, the UPC Federated Satellite System (FSSCat) mission marked a significant milestone by employing AI for the first time for cloud detection. FSSCat consisted of two 6-unit CubeSats: one of them was equipped with UPC’s Flexible Microwave Payload-2 (FMPL-2), featuring an L-band microwave radiometer and a GNSS reflectometer implemented in a Zynq—7045 FPGA for sea ice and soil moisture monitoring. Additionally, the second CubeSat included Cosine’s HyperScout-2 visible + near-infrared + thermal infrared hyperspectral imager and included the PhiSat-1 AI board in a Movidius processor. Notably, FSSCat was the first CubeSat-based mission that contributed to the Copernicus program [161]. The application of AI in CubeSat missions has revolutionized the efficiency and accuracy of data processing. By employing AI algorithms, CubeSats can conduct real-time data analysis, make autonomous decisions, and optimize satellite operations, leading to enhanced mission performance and reduced operational costs. For the FSSCat mission, AI was utilized to select data for download based on cloud coverage, optimizing data transmission. This integration of AI in CubeSats exemplifies how advanced technologies enhance the efficiency and effectiveness of space exploration endeavors.
3.5.3. Space Technology Innovations: Advancements and Sustainability
3.5.4. CubeSats and Beyond: Advances and Future Initiatives
4. Identified Small Satellite Features
- Disruptive Technologies: satellite missions that test new technological capabilities [183];
- Biology and Science: missions involving scientific experiments that explore the behavior of microorganisms in a space environment;
- Communication/Data Transfer: missions primarily aimed at developing new communication methods in space;
- Support: satellites serving as assistance for other satellites with payloads, focusing on supporting primary objectives;
- Earth Observation, Earth sciences and interplanetary probes [185];
- Military Security, Intelligence Surveillance and Reconnaissance (ISR);
- Navigation [186];
- Science, Technology and Education: this classification serves educational purposes, primarily targeting leadership in universities and research centers, with objectives centered around scientific and technological demonstrations;
- Sustainable Space: satellite missions focused on facilitating initial space pollution mitigation efforts and establishing a foundation for ongoing space sustainability initiatives;
- In-orbit Activities: missions aiming to utilize existing satellite capabilities for operations in the space environment;
- Unconventional Satellite Missions: showcasing novel capabilities and structures within satellite technology.
- (a)
- Active Debris Removal (ADR): Space debris, which includes decommissioned satellites and other fragments, presents a growing threat to the safety and functionality of operational satellites. The implementation of effective active debris removal (ADR) methods is vital for establishing and maintaining a sustainable space environment. In Table A3, this is categorized as Active Debris Removal (ADR)/Docking, and we delve into state-of-the-art ADR technologies and strategies, such as deorbiting with no pre-installed docking interface, capture systems with integrated propulsion, self-destructing magnetic tugboats, space transportation systems, and space debris “Gobblers”, among others. This examination underscores the significance of proactive debris management for mitigating collision risks and preserving orbital space for future satellite deployments.
- (b)
- Transport Logistics: Efficient logistics and transportation systems are important for ensuring the successful launching, deployment, and repositioning of satellites. In Table A1, categorized under “Management and Manufacturing Techniques”, we delve into cutting-edge logistics solutions, including technologies like orbit-reconfigurable satellites, radiation-resistant components, 3D printing, and other innovative approaches. These solutions are purposefully designed to not only reduce the environmental impact of satellite launches but also to optimize satellite placement for maximum efficiency.
- (c)
- Mission Extension: Extending the operational life of satellites is not only an economically sound approach, but it also environmentally responsible. We delve into innovative mission extension technologies, such as satellite servicing and in-orbit refueling, as sustainable methods for prolonging the lifespans of satellites and reducing the necessity for new deployments. In Table A2, we showcase a range of developments (e.g., disruptive technologies, communication and data transfer advancements, and innovations in military security and intelligence surveillance and reconnaissance (ISR)). These developments encompass innovative payloads aimed at optimizing satellite performance and ensuring the continued success of missions.
- (d)
- Repair and Construction: Satellite repair and in-orbit construction capabilities are imperative for mitigating the environmental impact caused by outdated and malfunctioning satellites. In Table A4, we explore the development of autonomous construction and repair techniques, encompassing on-orbit assembly and component replacement [187,188,189]. These approaches are instrumental for extending the operational lifespan of satellites while concurrently minimizing the generation of space debris [190].
5. Conclusions and Future Research
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Abbreviations
ADR | Active Debris Removal |
CD | Compliant With Direct Re-entry |
COSMIC | Cleaning Outer Space Mission through Innovative Capture |
CWFB | Compliant With attempt False Before |
CWO | Compliant WithOut attempt |
CWTB | Compliant With attempt True Before |
EO | Earth Observation |
ESA | European Space Agency |
ISAM | In-orbit Servicing, Assembly, and Manufacturing |
JAXA | Japanese Space Agency |
LEO | Low Earth Orbit |
MASTER | Meteoroid and Space Debris Terrestrial Environment Reference |
MRM | Modular Refueling Module |
NCWO | Not Compliant WithOut attempt |
NCWFB | Not Compliant With attempt False Before |
NCWTB | Not Compliant With attempt True Before |
ReMaP | Reuse Market Place |
R&M | Reliability and Maintainability |
S2WG | Sustainability Working Group |
WSTF | White Sands Test Facility |
Appendix A
- Table A1. Management and Manufacturing.
- Table A2. Disruptive Technologies, Planetary Defense, Biology and Science, Communication/Data Transfer, Support, Earth Observation, Earth Sciences and Interplanetary Probes, and Military Security, Intelligence Surveillance and Reconnaissance (ISR).
- Table A3. Navigation, Science, Technology and Education, Sustainable Space, Maneuvers, On-orbit activities, and Unconventional Satellite Mission Proposals.
- Table A4. Supply Chain Stage Trends for Satellite Development.
Development Type | Category | Item | Mission | Feature | Agency/Institution | Country-Launch Year |
---|---|---|---|---|---|---|
Management and manufacturing | Lean methodologies | An orbit reconfigurable satellite | GomX-4* | Reconfigurable Field Programable Gate Array (FPGA) in flight. | GomSpace- ESA | Denmark (2018) |
ArgoMoon* | Fourth-generation flash-based FPGA on a single chip [179]. | ASI (Italian Space Agency)- ESA | Italy (2022) | |||
LINUSS 2* | With a new architecture, users can enhance capabilities and assign new missions through a software update. | Lockheed Martin Space Operations | USA (2022) | |||
WISA Woodsat | The world’s first wooden satellite. | WISA Plywood- ESA | Finland (2023) | |||
DAVE | Technological demonstration of mechanical dampers in microgravity. | Cal Poly | USA (2018) | |||
Virginia CubeSats Constellation | Measure orbital decay to form a database of atmospheric drag for small satellites. | University of Virginia & Hampton University | USA (2019) | |||
EagleSat-1 | Embry-Riddle | USA (2017) | ||||
MakerSat-0 | Measure deterioration of polymers used in 3D printing due to exposure to the space environment. | Northwest Nazarene University | USA (2017) | |||
RadFxSat | To measure the effect of ionizing radiation in memory integrated circuits, especially in CMOS. | AMSAT | USA (2017) | |||
ARGUS-2 | Vanderbilt University | USA (2015) | ||||
3D-printed | LINUSS 2* | Validating capabilities 3D-printed spacecraft components [196] | Lockheed Martin Space Operations | USA (2022) | ||
Radiation-resistant components | ArgoMoon* | Hardened components by design against radiation-induced SEUs. | ASI (Italian Space Agency)- ESA | Italy (2022) | ||
LINUSS 2* | High-power radiation-hardened computer. | SHREC research | USA (2022) | |||
Compact Satellite Bus/ Dispenser/Deployer | ION CubeSat Carrier | Capable to host a combination of CubeSats that fits the volume. | D-Orbit | Italy (2020) | ||
PPOD (for LightSail-1) | Poly Picosatellite Orbital Deployer. | CalPoly | USA (2013) | |||
CSD | Canisterized Satellite Dispenser. | RocketLab | USA (2022) | |||
LINUSS 2* | Docking adapter bus to add new mission capabilities after launch. | Lockheed Martin Space Operations | USA (2022) | |||
Solar Panels / Sail | NanoSail D. Square, kite-like, rigid solar sails | Solar sail drag device for deorbiting satellites. | NASA | USA (2006) | ||
Dcubed | Origami Solar Arrays. | Dcubed | Germany | |||
Miura-ori (proposal) | Miura-ori Origami principle – efficient way to pack solar panels. | JAXA | USA & UK (2020) | |||
Self-folding mechanism for self-reconfiguration CubeSat. | Oxford Space System | |||||
University of Liverpool | ||||||
Ikaros* Spinning disk solar sails | Lightweight, reflective membrane propellant by the sun’s radiation. | JAXA | Japan (2010) | |||
Antennas | RemoveDebris* | Helical antennas deployable. | University of Surrey - Surrey Space Centre | UK (2018) | ||
ESAIL | Hold Down and Release Mechanisms [197] | Oxford Space Systems- ESA | USA (2020) | |||
NORsat-2 | Novel Engineering Techniques for Origami-Inspired (Yagi) Antenna Deployment. | Norwegian Space Agency (NOSA) | Norway (2017) | |||
NovaSAR-1 | Deployable wrapped rib SAR antenna and RF system. | SSTL (Surrey Satellite Technology Ltd.), UK, and Airbus DS | UK (2018) | |||
RainCube* | Ultra-compact deployable Ka-band Cassegrain antenna. | NASA JPL | USA (2018) | |||
Flight software | Lunar IceCube | The computer language with the lowest error rate. | Morehead State University, NASA | USA (2022) | ||
Cameras | Cislunar Explorers* | Three onboard cameras are used to capture images of the Sun, Moon, and Earth. | Cornell University | USA (2024) | ||
GomX-4* | Hyperspectral imaging | GomSpace- ESA | Denmark (2018) | |||
Payloads: Radar | RainCube* | Ka-band radar technologies. | NASA JPL | USA (2018) | ||
Ofeq-5 satellite* | Synthetic-Aperture Radar (SAR). | Israel Defence Force | Israel (2002) | |||
CryoSat-2* | SAR Interferometric Radar Altimeter. | ESA | France (2010) | |||
ESA’s Hera mission* | First radar probe of an asteroid. | ESA | France (2024) | |||
MicroSAR* | Can detect relatively small vessels in a large area simultaneously. | Space Norway- Oxford Space Systems | Norway (2025) | |||
Design | Cislunar Explorers* | Two L-shaped satellites (6U CubeSat). | Cornell University | USA (2024) | ||
Thrust/ Propulsion/ Propellant | GomX-4* | Highly miniaturized cold-gas. | Nanospace of Uppsala | Denmark (2018) | ||
LunIR* | Low thrust electric propulsion technology. | Lockheed Martin Space- NASA | USA (2022) | |||
Lunar IceCube* | Miniature electric RF ion engine system. | Morehead State University, NASA | USA (2022) | |||
Cislunar Explorers* | Water electrolysis propulsion system. | Cornell University | USA (2024) | |||
ArgoMoon* | Hybrid micropropulsion system (mono-propellant and cold gas propulsion). | ASI (Italian Space Agency)- ESA | Italy (2022) | |||
Team Miles | Plasma thrusters. | Team Miles | USA (2022) | |||
Mono-propellant deorbit stage (MPDS)* | Designed to quickly and precisely deorbit. | SpaceWorks | USA (2023) | |||
Ground Station | LINUSS 2* | Multi-core hardware to process more data in orbit. | Lockheed Martin Space Operations | USA (2022) |
Development Type | Category | Item | Mission | Feature | Agency/Institution | Country-Launch Year |
---|---|---|---|---|---|---|
Disruptive technologies | Use of disruptive technologies | Blockchain technology. | GomX-4* | Blockchain technology. | GomSpace- ESA | Denmark (2018) |
SIRION PATHFINDER 2 | Test IoT communications using blockchain technology. | EchoStar Satellite Services | USA (2018) | |||
Artificial Intelligence (AI) | FSSCAT* | Image processing [198] | Universitat Politècnica de Catalunya | Spain (2020) | ||
Quantum technologies | MOZI HAO (MICIUS QKD) | Test ultra-secure quantum communications in orbit. | China Academy of Sciences (CAS) | China (2016) | ||
TeQuantS project* | Quantum space-to-Earth communication. | ESA with Thales and Leonardo [199] | France (2026) | |||
Test cloud computing infrastructure | TYVAK 0129 (PATHFINDER RISK REDUCTION) | Prove out RF-enabled swarming formations and space-to-space networking. | NASA Ames Research Center | USA (2019) | ||
Cloud Computing and Storage Platform | FSSCAT* / 3Cat- 5B | Image processing [198] | Universitat Politècnica de Catalunya | Spain (2020) | ||
Nebula-ION platform | Uplink and run software and artificial intelligence and machine learning (AI/ML) apps. | D-Orbit | Italy (2021) | |||
5G and 6G | SpaceX- 2019-074A | Technology standard for broadband cellular networks [200] | SpaceX | USA (2019) | ||
Planetary defense | Against near-Earth objects (NEOs) | Asteroid | DART Mission (Double Asteroid Redirect Test) | Asteroid Trajectory deflection [201] | NASA | USA (2021) |
Hera’s mission | First test of asteroid deflection, with the first rendezvous with a binary asteroid system. | ESA | France (2024) | |||
Biology and Science | Samples | HAYABUSA 2 | Rock samples taken from the Ryugu asteroid. | JAXA | Japan (2014) | |
Tests on living organisms | Multi-cellular organism | WormSail | First multi-cellular organism on CubeSat flight. | University of Nottingham | UK (2024) | |
Radiation studies | BioSentinel | First study of the biological response to space radiation outside LEO [202]. | NASA | USA (2022) | ||
Communication/ Data transfer | Inter-Satellite Linking (ISL) | ISL and station keeping capabilities | GomX-4* | Linked through a new version of the SDR (Software Defined Radio). | GomSpace- ESA | Denmark (2018) |
Long-distance | Lunar- Earth | ArgoMoon* | X-Band transponder. | ASI (Italian Space Agency)- ESA | Italy (2022) | |
Optical communication | Optical communication | ArgoMoon* | Rangefinder (RF) controls the distance from target. | ASI- ESA | Italy (2022) | |
Interplanetary | Mars-Earth | MarCO | Data relay satellite. | NASA JPL | USA (2018) | |
Quantum | Quantum Science Satellite (QSS) | MOZI HAO (MICIUS QKD) | Test ultra-secure quantum communications in orbit. | China Academy of Sciences (CAS) | China (2016) | |
Support | Inspection | Without the involvement of the ground segment | ArgoMoon* | Transmit telemetry and data through different antennas in satellite. | ASI (Italian Space Agency)- ESA | Italy (2022) |
Long-term Services | Astronaut lunar missions | CAPSTONE* | Calculated orbital stability planned for the Lunar Gateway space station. | Advanced Space, LLC. -NASA | USA (2022) | |
Other missions | Companion satellite | LICIACube* | Image the collision DART and Asteroid impact. | ASI | Italy (2021) | |
Earth Observation and Sciences, Interplanetary Probes | Earth Observation | Artic | GomX-4* | Arctic Radiation experiment. | GomSpace- ESA | Denmark (2018) |
Earth | GRACE* | Earth’s gravity field and ionosphere. | NASA | USA (2002) | ||
CryoSat-2* | Polar sea ice studies. | ESA | France (2010) | |||
Interplanetary observation | Asteroid | Near-Earth Asteroid (NEA) | Asteroids flying within 0.5 AU of Earth are to be investigated with high resolution camera. NEA Scout target, to be encountered in November 2023. | NASA | USA (2022) | |
Sun | HELIOS mission | First close-in measurements of the Sun’s surface and solar wind. | NASA | USA (1978) | ||
ESA’s Cluster quartet | Study Earth magnetic field the energetic particles of the solar wind. | ESA | (2000) | |||
CubeSat for Solar Particles (CuSP) | Sun dynamic particles and magnetic fields. | Southwest Research Institute and NASA | USA (2022) | |||
Proba-3* | Sun’s ghostly corona, or surrounding atmosphere. | ESA | France (2024) | |||
Lunar | LunaH-Map | Investigate presence of water-ice. | Arizona State University- NASA | USA (2022) | ||
Lunar IceCube* | Water distribution on the Moon from lunar orbit. | NASA | USA (2022) | |||
Luna-27 | Explore lunar south pole. | Roscosmos | Russia (2025) | |||
OMOTENASHI | Measurements of the radiation environment. | JAXA- Lockheed Martin Space - NASA | Japan/ USA (2022) | |||
LunIR* | Low-energy trajectory control technologies Earth-Moon. | Lockheed Martin Space- NASA | USA (2022) | |||
Luna-26 | Lunar orbital mapping mission. | Roscosmos | Russia (2024) | |||
Mars | MarCO | Communication link to Earth. | NASA JPL | USA (2018) | ||
Venus | Ikaros* | Venus flyby. | JAXA | Japan (2010) | ||
Military security; Intelligence Surveillance; Reconnaissance (ISR) | Security | Synthetic-Aperture Radar (SAR) | PAZ | SAR satellite with ship identification secondary function. | Hisdesat Strategic Services S.A | Spain (2018) |
RainCube* | Ka-band radar technologies. | NASA JPL | USA (2018) | |||
Ofeq-5 satellite* | Synthetic-Aperture Radar (SAR). | Israel Defence Force | Israel (2002) | |||
CryoSat-2* | SAR Interferometric Radar Altimeter. | ESA | France (2010) | |||
MicroSAR* | Can detect relatively small vessels in a large area simultaneously. | Space Norway- Oxford Space Systems | Norway (2025) | |||
Cybersecurity | Quantum technologies | TeQuantS project* | Secure cryptographic keys using the quantum properties of light. | ESA with Thales and Leonardo | France (2026) | |
Weapon | Anti-satellite weapons (ASAT) | Cosmos 2504 | Test version of inspection satellite. | Russian Ministry of Defence | Russia (2015) | |
ISR | Intelligence Surveillance and Reconnaissance | TYCHE | Intelligence Surveillance and Reconnaissance (ISR). | UK Space-based | UK (2025) |
Development Type | Category | Item | Mission | Feature | Agency/Institution | Country- Launch Year |
---|---|---|---|---|---|---|
Navigation | Optical navigation | Laser Infrared Crosslink | CLICK A | Optical laser communications with a single 3-unit (3U) spacecraft. | MIT Lincoln Laboratory | USA (2022) |
Interplanetary | Cislunar Explorers* | Navigate completely autonomously, with minimal control from Earth. | Cornell University | USA (2024) | ||
X-ray pulsars | Interplanetary | XPNAV-1* | Determine its location in the solar system within 5 kilometers. | Aerospace Science and Technology Corp | China (2016) | |
Science, Technology and Education | Novel Instrument | InfraRed Spectrometer | Lunar IceCube* | Broadband InfraRed Exploration Spectrometer (BIRCHES). | Morehead State University, NASA | USA (2022) |
X-ray Telescope | XPNAV-1* | Test background noise of the universe. | China Aerospace Science and Technology Corp | China (2016) | ||
Space radiation- Telescope | Foresail-1* | Near-Earth radiation environment. | Helsinki University of Technology | Finland (2022) | ||
Sustainable Space | Active Debris Removal (ADR)/ Docking | Life extension | MEV-1* Mission Extension Vehicle (MEV) | Attached to INTELSAT 901 to provide 5 year life extension. | Space Logistics LLC (Northrop Grumman) | USA (2019) |
Deorbit/ with no docking interface pre-installed | ClearSpace-1 | Mission to de-orbit space debris with non-cooperative platforms | ESA | France (2025) | ||
Service, Inspection and Removal | DART | Demo of Autonomous Rendezvous Tech. | NASA | USA (2005) | ||
ADRAS-J1 | Removing large-scale debris from orbit. | Astroscale (Japan) | Japan (2024) | |||
ATV Europe’s Automated Transfer Vehicle | Dispose of Space Station waste. | ESA | (2018) | |||
Capture system /propulsion system | MEV-1* Mission Extension Vehicle (MEV) | A satellite in a graveyard orbit was captured and returned to operational status. | Space Logistics LLC (Northrop Grumman) | USA (2019) | ||
Green propellant | Mono-propellant deorbit stage (MPDS)* | High-thrust chemical propulsion stage utilizing environmentally-friendly liquid propellants. | SpaceWorks | USA (2023) | ||
Capture Method- Magnetic Capture | ELSA-d CHASER | Demonstrates magnetic capture in space. | Astroscale | UK- Japan (2021) | ||
Capture Method- Net | RemoveDebris* | Wrapped and entangled the target. | University of Surrey - Surrey Space Centre | UK (2018) | ||
Capture Method- Harpoon | RemoveDebris* | Tethered Harpoon test. | ||||
Capture Method- Claw | ClearSpace-1* | Clearspace-1 will capture and safely deorbit a large derelict object. | ESA | France (2025) | ||
Capture Method- Tether | Dragracer A, B (Alchemy, Augury) | Terminator Tape deorbiting device. | TriSept Corp | USA (2020) | ||
Laser Orbital Debris Removal (LODR) | EOS Space Systems Space Debris Management | High energy laser pulser radiation. | EOS Company | Australia (2022) | ||
Self-destructing- magnetic tugboat | In study- proposal | Magnetic tugboat debris capture system [203] | ESA- Institut Supérieur de l’Aéronautique et de l’Espace | France (2017) | ||
Self-destructing-plasma brake | Foresail-1* | Bring spacecraft back into the atmosphere. | Helsinki University of Technology | Finland (2022) | ||
Spinning Magnets | In study- proposal | Dexterous magnetic manipulation of conductive non-magnetic objects. | University of Utah | USA (2021) | ||
Mechanic capture | ASTRO - ORBITAL EXPRESS 1 | Robotic arm for servicing missions. | DARPA Satellite Operations (Op.) | USA (2007) | ||
Reusable vehicles | Space Transportation Systems | Space Rider | Combining reusability, in-orbit operations, and transportation [204] | ESA | France (2023) | |
Implement technics | Gobble up space debris | ClearSpace-1* | The satellite will capture the small SwissCube satellite using a conical net before destroying it in the atmosphere. | ESA | Switzerland (2025) | |
Maneuvers | Formation flying | Fly in close formation | TerraSAR-X and TanDEM-X | SAR Interferometry. | DLR – (German Aerospace Center) | Germany (2007) |
Maneuver | Collision Avoidance Maneuver | Proba-3* | Rendezvous experiment in elliptical orbit [205] | ESA | France (2024) | |
Cluster | Cluster formations | ESA’s Cluster quartet | Feet of 4 spacecraft to study plasma phenomena in 3 dimensions. | ESA | Germany (2000) | |
Constellations | Satellite constellations | Starlink | Satellite Internet access. | SpaceX | USA (2019- 2022) | |
Fractionated | Picosatellites’s formation | ANDESITE | Ad-hoc Network Demonstration for Extended Satellite-based Inquiry and other Team Endeavours [206] | Center for Space Physics (CSP) | USA (2020) | |
Retrograde orbit | Lunar | CAPSTONE* | Near polar lunar orbit. | Advanced Space, LLC. -NASA | USA (2022) | |
Earth | Ofeq-9 | Satellite operates in retrograde low Earth orbit. | Israel Defence Force | Israel (2010) | ||
Deep space | Lunar | ArgoMoon* | Propulsive maneuver to close in a geocentric orbit. | ASI- ESA | Italy (2022) | |
On-orbit activities | Servicing missions | Cargo delivery, Satellite retrieval | DART | Autonomous rendezvous operations. | NASA | USA (2005) |
Demonstrating new technologies | Hera’s mission | First probe to rendezvous with binary asteroid system. | ESA | France (2024) | ||
Assembly and Manufacturing | OSAM-1 | Demonstration of manufacturing using 3D printing of 10m beams. | NASA | USA (2025) | ||
Unconventional satellite mission proposals | HAPS (High Altitude Pseudo-Satellite) | Stratospheric platform for COMMS or EO | Ecosat Airships | Solar Airship for communications and observation applications. | Capgemini Engineering | Spain (2021) |
High-altitude platform services. | Geo-synchronous high-altitude payload platform | Sitallite | Communication platform within a 1000 km diameter range [207] | VanWyn, Inc. | Canada (2021) |
Supply Chain Stage | Category | Trend | Description | Characteristics | Company/ Institution |
---|---|---|---|---|---|
Manufacturing | Methodologies | Agile and Lean methodologies- Six Sigma | Applications of methods for low-cost, fast delivery, and waste minimization | • Small size | Kysushu Institute of Technology |
• Use of non-space-qualified COTS units | |||||
Vertical Integration in Satellite Manufacturing | • Efficient manufacturing practices. | SpaceWorks | |||
• Development and production costs of the constellation, amortized across the number of operational satellites. | |||||
New engineering methods and technologies | 4.0 Industry | Low-cost, mass-production, data-driven, reduce lead time business model | • Reusable Launchers | Capgemini-engineering | |
• LEO satellites constellations | |||||
• Digital transformation | |||||
• Agility methods/ Flexibility | |||||
• Cloud computing | |||||
• Digitalize the manufacturing processes | |||||
• 3D- Printing | |||||
• Digital Twins | |||||
• Artificial Intelligent | |||||
• IOT & connectivity | |||||
• Virtual & augmented reality | |||||
• AIT expertise & tools | |||||
• Product Lifecycle Management (PLM) | |||||
• Integration between design and manufacturing | |||||
Materials | New and current | Flexible carbon-fiber | Tailor-made composites for tougher space structures | ESA | |
Space infrastructure | Robots | Self-assemble test | Small cubes with no external moving parts can self-propel, stack, and form various shapes in experiments [136] | Massachusetts Institute of Technology (MIT) | |
Robotic arm to build satellites in space | • Length of 11.3 meters, the symmetrical, two-handed intelligent robot arm | Airbus | |||
• Control computer in the middle of the arm give the robot arm its versatility. | |||||
3D- Printing | Portable Onboard Printer 3D | Producing a system of automated additive manufacturing aboard the International Space Station | Capgemini-engineering | ||
Launch Services | In-space transportation services | ION Satellite Carrier deployer | Satellite transports across orbits into its final operational slot. | • Onboard software to process incoming commands, perform mission operations, process raw data, and downlink information | D-Orbit |
• Multiple form factor support: capacity (a 64 1U and multiple combinations of CubeSats, or microsatellites up to 160 kg. | |||||
DPODs and DCUBEs dispensers | • Ability to perform orbital maneuvers: | ||||
• Precise deployment | |||||
Dispensers- RUAG Space | Satellite transports | • 1.7-meter central cylinder structure and a height of 5.5 meters. | Airbus | ||
• Automated Potting Process | |||||
• Multi-layer thermal insulation | |||||
Orbital Transfer Vehicles | Sherpa Program | Transportation for LEO, trans-lunar and low-lunar orbits, or beyond to GEO | • Executing multiple deployments, | Spaceflight | |
• Providing independent and detailed deployment telemetry, and flexible interfaces. | |||||
• Propulsion technology | |||||
Separation System | CarboNIX | Synchronous spring pusher system deploys satellites smoothly and evenly | • Scalable separation system that is available in sizes of 8″, 15″ and 24″ diameter for microsatellites weighting from 10 up to 500 kg. | Exolaunch | |
• Reduce the risk of damaging sensitive satellites optical payloads and electronic components | |||||
Cluster Capabilities | EXOports | Multiport Adapter | • Cluster to be built on a single 15” or 24” ESPA or SpaceX Dispenser Ring port. | Exolaunch | |
Satellite operation/ Sustainability stage | Spacecraft Docking and Connection Device | FuseBlox™ | Soft and hard capture with near-zero momentum transfer and provide high-reliability electrical power and data connectivity | • Self-aligning grapple technique accommodates small spacecraft rendezvous misalignments while device symmetry enables four secure mated configurations | SpaceWorks |
• Modular Capacity for expanding in-space infrastructure | |||||
• Supports gigabit ethernet and MIL-STD-1553 data connections | |||||
• Enabling architectures for space-based solar power | |||||
• In-space assembly and manufacturing | |||||
Docking Plate | In-orbit servicing, refueling, refurbishments and relocation. | • Demonstrate proactive responsible space practice and space sustainability | Astroscale | ||
• Lightweight, compact and minimally intrusive. | |||||
Refueling Satellites in Space | Refueling technology. | Gas Stations in Space | • End-to-end refueling service using its Rapidly Attachable Fluid Transfer Interface (RAFTI) | Lockheed Martin | |
• Drop-in replacement for existing satellite fill-and-drain valves | |||||
Life extension/ Sustainability stage | Recycling space debris into raw materials | Refine metal space debris | Space applications with recycling materials | • Provider of refined material for the construction of large orbital stations, the retrofit and repair of satellites, and assembly of reusable spacecraft. | CisLunar Industries (CLI); Space Foundry Airbus and the European Commission |
• Reusable space tugs will deliver large debris items, to be processed and refined to customer specifications. | |||||
Active Debris Removal (ADR)/ | Self-Removal | Self-Removal of Spacecraft (TeSeR) program | • Development of a prototype of a “cost-efficient but highly reliable” removal module. | ||
• Three different removal technologies: solid propulsion, drag augmentation systems and electrodynamic tether. |
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Primary Mission Group | Small SatMarket [13] | Bryce [13] | Seradata [14] | SpaceWorks [15] |
---|---|---|---|---|
Communications | 23% | 11% | 42% | 13% |
Technology Development | 28% | 40% | 25% | 26% |
Scientific | 23% | 8% | 12% | 13% |
Novel Applications/ Other–Unknown | 3% | 3% | 1% | 2% |
Earth Observation/ Remote Sensing | 23% | 38% | 20% | 46% |
Technology | 2012 Technology Review [130] | 2017 Technology Review [131] | Justification |
---|---|---|---|
Atmospheric chemistry instruments | Problematic | Feasible | PICASSO, IR sounders |
Atmospheric temperature and humidity sounders | Feasible | Feasible | — |
Cloud profile and rain radars | Unfeasible | Feasible | JPL RainCube demo |
Earth radiation budget radiometers | Feasible | Feasible | SERB, RAVAN |
Gravity instruments | Feasible | Feasible | No demo mission |
Hi-res optical imagers | Unfeasible | Feasible | Planet Labs |
Imaging microwave radars | Unfeasible | Problematic | Ka-Band 12 U design |
Imaging multispectral radiometers (Vis/IR) | Problematic | Feasible | AstroDigital |
Imaging multispectral radiometers (W) | Problematic | Feasible | TEMPEST |
Lidars | Unfeasible | Problematic | DIAL laser occultation |
Lightning imagers | Feasible | Feasible | — |
Magnetic field | Feasible | Feasible | InSPIRE |
Multiple direction/ polarization radiometers | Problematic | Feasible | HARP Polarimeter |
Ocean color instruments | Feasible | Feasible | SeaHawk |
Precision orbit | Feasible | Feasible | CanX-4 and CanX-5 |
Radar altimeters | Unfeasible | Feasible | Bistatic LEO-GEO/ MEO |
Scatterometers | Unfeasible | Feasible | CYGNSS (GNSS-R) |
Features | Characteristics Identified in Small Satellites Missions | Challenges and Contributions to a Sustainable Space |
---|---|---|
Technology miniaturization | More powerful and smaller systems | Reduced volume of space debris |
Multiple mission objectives | Satellites with multiple or complementary mission objectives (i.e., constellations) | Flexibility for multi-purpose and reconfigurable missions |
Involves high-risk missions | Uses for scientific experiments in risky orbits (i.e., inter-planetary or asteroid) | Satellite missions with high risk but with reliability and reusable satellites |
Low-cost trend | Multidisciplinary projects; university, government, and space companies working together; exchanging knowledge and experiences | Use new materials and reduce manufacturing times through innovative methodologies (e.g., additive manufacturing) |
Novel developments | Promote more open space access through standardized platforms and reduced satellite sizes | Development of new capabilities for space architectures |
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Buitrago-Leiva, J.N.; Camps, A.; Moncada Niño, A. Considerations for Eco-LeanSat Satellite Manufacturing and Recycling. Sustainability 2024, 16, 4933. https://doi.org/10.3390/su16124933
Buitrago-Leiva JN, Camps A, Moncada Niño A. Considerations for Eco-LeanSat Satellite Manufacturing and Recycling. Sustainability. 2024; 16(12):4933. https://doi.org/10.3390/su16124933
Chicago/Turabian StyleBuitrago-Leiva, Jeimmy Nataly, Adriano Camps, and Alvaro Moncada Niño. 2024. "Considerations for Eco-LeanSat Satellite Manufacturing and Recycling" Sustainability 16, no. 12: 4933. https://doi.org/10.3390/su16124933
APA StyleBuitrago-Leiva, J. N., Camps, A., & Moncada Niño, A. (2024). Considerations for Eco-LeanSat Satellite Manufacturing and Recycling. Sustainability, 16(12), 4933. https://doi.org/10.3390/su16124933