SmallSat Europe 2025 Technical Proceedings
Technical papers presented at SmallSat Europe 2025, 27–28 May 2025, RAI Amsterdam, the Netherlands. Listed in program order.
Extending a Mole-Based Design Framework to Enable the Design of Versatile Antagonistic SMA Actuator Architectures
Joachim Schmidt, Leon Christians · DCubed
SSE25-001SmallSat Europe 2025 Technical ProceedingsTalkPDF 5 pp · 1.2 MB
1. Motivation/Background Adaptive space structures enable reversible shape reconfiguration between two or more operational states, allowing spacecraft instruments to dynamically adapt to mission phases and optimize performance. …
AI based satellite system architecture to detect and classify ship activities
Renan Menezes, Gleisson Bezerra, Lidia Sato, Luis Loures Costa · Instituto Tecnológico de Aeronáutica (ITA)
SSE25-002SmallSat Europe 2025 Technical ProceedingsTalkPDF 10 pp · 768 KB
Maritime Domain Awareness (MDA) is vital for global security, enabling the monitoring of maritime activities to counter threats such as piracy, smuggling, and illegal, unreported, and unregulated (IUU) fishing. Traditional maritime …
V-LEOS: Investigating mission concepts for industrialised satellite platforms for Very Low Earth Orbit applications
Jan-Christian Meyer, Ashvij Narayanan, Andreas Wiegand · Berlin Space Technologies GmbH; Astos Solutions GmbH
SSE25-003SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 243 KB
Satellite applications in very low earth orbit (VLEO) have been investigated in the literature for a long time. One of the very few realised missions is GOCE to measure Earths gravity potential. It is evident that there is a discrepancy …
Small Satellite Spectrum Access: Navigating the Path to WRC-27
Alexis Martin · River Advisers
SSE25-004SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 288 KB
The World Radiocommunication Conference in 2027 (WRC-27) presents a significant opportunity for the small satellite community to secure and defend critical spectrum access, vital to their operations and growth. Although the event is still …
Small satellite deployable thin membrane antenna review
Mayank, Ville Lunden, Tuukka Kuuramaa, Samuli Nyman, Jaan Praks · Aalto University
SSE25-005SmallSat Europe 2025 Technical ProceedingsTalkPDF 5 pp · 430 KB
Deployable thin membrane antennas play a pivotal role in enhancing the communication and mission capabilities of small satellites. These antennas offer a lightweight and compact solution to achieve high gain and wide bandwidth, addressing …
Multi-Orbit Design Tool
Charilaos Kourogiorgas · Atheras Analytics
SSE25-006SmallSat Europe 2025 Technical ProceedingsTalkPDF 10 pp · 1.5 MB
Atheras Analytics has developed a multi-orbit design tool that is able to optimise the design of a satellite system that consists of satellites at multiple orbits operating at Ka- and Q/V-bands. The need for broadband internet access …
Practical path towards net-zero debris
Perttu Yli-Opas · Aurora Propulsion Technologies
SSE25-007SmallSat Europe 2025 Technical ProceedingsTalkPDF 3 pp · 189 KB
Reaching the target of net-zero debris requires the whole space ecosystem to be built around robustness. In this paper, we conduct a thorough analysis of the long-term sustainability of in-orbit operations from different perspectives, …
Design and Integration of a High-Resolution Multispectral Optical Payload for Next-Generation Earth Observation Missions
Massimiliano Rossi, Fabio Emilio Zocchi, Giovanni Bianucci, Ronan Rodrigues, Gabriele Grisoni and 3 more · Media Lario S.r.l.
SSE25-008SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 1.2 MB
This paper reports the design, manufacturing, and integration of an optical multispectral payload for Earth observation, capable of achieving high spatial resolution with a Ground Sampling Distance (GSD) of less than 1 meter. The payload …
Multi-functional ultra-thin TMD solar cells for robust high-specific-power in space
Oliver Trojak, Koosha Nassiri Nazif, Eric Pop, Nina Vaidya · University of Southampton; Stanford University
SSE25-009SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 746 KB
Ultra-thin solar cells based on transition metal dichalcogenides (TMDs) offer several advantages over conventional solar technologies for space applications, including space radiation tolerance and high specific power. Due to the …
First flight and commissioning of a compact intelligent space camera for in-orbit visual operations
Aubrey Dunne, Juan Romero-Cañas, Peter O’Connor, Rosana Rodriguez-Bobada, Sandi Romih and 1 more · Ubotica Technologies
SSE25-010SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 241 KB
Satellite autonomy has the promise of reducing operational latency and costs, whilst simultaneously enabling reactivity and improved duty cycles, by converting satellites into intelligent robotic agents. Multiple approaches to achieving …
HEMPT – New EP Technology for SmallSats and LEO Constellations using Xenon, Krypton and Argon
Angelo Genovese · Thales Deutschland
SSE25-011SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 870 KB
The business unit Electron Devices of Thales Deutschland started the development of a new electric propulsion technology, the High Efficiency Multistage Plasma Thruster (HEMPT) at the end of the 90’s. After having carried out several basic …
Space Payload for Inertial De-spin Efficient Effects (SPIDEE) Enables Repeatable Orbital Debris Remediation Missions
Kalia Crowder, Simon Lee, Victor Aguero, David Smith, Adam Orris · Cambrian Works, Inc.
SSE25-012SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 1.7 MB
The Space Payload for Inertial De-spin Efficient Effects (SPIDEE) is an electroadhesion-based general purpose in-space attachment payload ideally suited for docking, augmentation, mobility, and in-space assembly missions that does not …
High resolution thermal imaging on a small satellite
Mike Goddard, Steven Knox, Harbinder Rana, James Bell, John Gilby and 14 more · Surrey Satellite Technology Ltd
SSE25-013SmallSat Europe 2025 Technical ProceedingsTalkPDF 22 pp · 1.7 MB
The DarkCarb instrument has been specifically designed to provide high-resolution thermal video imagery from a small satellite in support of a range of emerging commercial, government and scientific applications. So far, such capability …
Chickadee: A new nanosat format for hands-on education and technology maturation
Supriya Chakrabarti, Sunip K. Mukherjee, Mitchell E Bailey · University of Massachusetts, Lowell
SSE25-014SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 364 KB
We describe Chickadee, a new nanosat format that occupies the optional extra volume of CubeSat launchers. For 1U CubeSats, it provides roughly the same volume and mass allotment within a 0.6 U cuboid. An approximately 0.28 U short …
First in-orbit results of the QUBE mission hosting a laser communication terminal for experiments towards quantum key distribution from CubeSats
Benjamin Rödiger, René Rüddenklau, Roland Haber, Lisa Elsner · German Aerospace Center (DLR); Center for Telematics
SSE25-015SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 324 KB
OSIRIS4QUBE is an optical laser terminal for CubeSats to transmit experimental quantum states and is developed by the German Aerospace Center (DLR). It is based on the classical laser communication terminal OSIRIS4CubeSat which was …
Passive wire-driven deployable baffle for space debris monitoring
Mattia Longato, Mark Honeth, Guglielmo Saverio Aglietti, Vladimir Yotov, Samira Hosseini and 1 more · Te Pūnaha Ātea – Space Institute, University of Auckland; Vyoma GmbH
SSE25-016SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 1.3 MB
Using telescopic deployable structures can significantly reduce the large empty volume taken up by some types of optical payloads, thereby positively impacting launch vehicle options and mission costs. However, these structures add …
Demonstrating low-power iodine-fed Hall thruster propulsion system
Alfio E. Vinci, Dmytro Rafalskyi, Francesco M. Bianchi, Heeral Bhatt, Thibault Dubois and 1 more · ThrustMe
SSE25-017SmallSat Europe 2025 Technical ProceedingsTalkPDF 3 pp · 401 KB
Several thousands of Earth satellites launched to date feature an onboard propulsion system based on Hall thruster technology. These devices are key characters for in-orbit maneuvering thanks to their remarkable thrust-to-power ratio and …
A deterministic algorithm for station keeping with a fixed-thruster geostationary spacecraft
Florian BIBOUD, Emil Vinterhav, Maria Hoflund · Vinterstellar
SSE25-018SmallSat Europe 2025 Technical ProceedingsTalkPDF 26 pp · 725 KB
Geostationary satellites are indispensable for telecommunications, weather forecasting, and Earth observation due to their ability to maintain a fixed position relative to the Earth’s surface. However, sustaining this position requires …
Non-Destructive Qualification Testing for Aerospace Structures Using A Predictive Vibration Method
Samaher Shaheen, David Nguiffo, Forest Siewert, Elizabeth Rodriguez, Dennis O’Connor and 1 more · California State University, Chico
SSE25-019SmallSat Europe 2025 Technical ProceedingsTalkPDF 9 pp · 902 KB
Vibrational analysis is an important method for evaluating the structural performance of 3D-printed metal components in aerospace applications. Aerospace-grade materials are selected for their ability to resist extreme conditions, and …
Development of a 2-axis compliant joint for the orientation of payloads on small satellites: Material characterization and finite element analysis of 3D printed PolyEtherKetoneKetone (PEKK) and PolyEtherEtherKetone (PEEK)
Morgane Domerg, Benjamin Ostré, Yoann Joliff, Yves-Henri Grunevald · MAPIEM Laboratory, University of Toulon; CES WORKS
SSE25-020SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 666 KB
To orient payloads such as cameras, antennas or sensors on small satellites, a 2-axis polymer-based joint of ±45° rotation range per axis is in development [1]. This mechanism can extend opportunities for satellite buses to individually …
Green Propulsion to the Rescue- Solving the SmallSats Regulatory Paradox
Neta Palkovitz, Sindu Shankar · Dawn Aerospace
SSE25-021SmallSat Europe 2025 Technical ProceedingsTalkPDF 5 pp · 194 KB
SmallSats and especially CubeSats have been suffering from a bad reputation with regulators worldwide. The simplified standardized way to achieving space missions created a revolution in the space industry, which meant many more states …
Less is More: CORSA’s Edge Foundation Model for Constrained AI
Xenia Ivashkovych, Bart Beusen, Nick Witvrouwen, Tanja Van Achteren · VITO Remote Sensing
SSE25-022SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 307 KB
The disparity between data capture in space and Earth’s downlink capabilities is well-documented and poses a significant challenge for space industry stakeholders, academics, and public institutions alike. The consequences of this …
Seeing: A family of Earth Observation Payloads
Eric Ruch · Safran Reosc
SSE25-023SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 1.1 MB
Safran Reosc has developed the SEEING imagers, a family of instruments for earth observation. This family includes several payloads from medium resolution with a wide field of view, to very high resolution with a ground sampling distance …
How to fight fire from space!
Henrique Moura, Phil Reiter · imec, University of Antwerp
SSE25-024SmallSat Europe 2025 Technical ProceedingsTalkPDF 16 pp · 3.1 MB
Wildfires are destructive natural disasters that severely impact ecosystems, wildlife, and air quality. They emit large quantities of greenhouse gases, thus accelerating climate change. In the U.S., wildfires have become more frequent and …
Building dynamic Satcom ground infrastructure with agile cloud computing
Alan Campbell, Rus Healy · AWS
SSE25-025SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 456 KB
The ground is changing for satellite communication systems. Operators are seeking to move towards digital teleport infrastructure to reduce physical infrastructure, enable seamless modem upgrades, and avoid vendor lock. The new Waveform …
Isar Aerospace and the Spectrum Launch Vehicle — At the forefront of Future European Launch Services
Sam Arne Whalley, Johanna Pardo · Isar Aerospace SE
SSE25-026SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 540 KB
The European space industry is at a critical juncture in its development. After the past years of rapid growth, the industry has necessitated innovative launch solutions to meet the ever-increasing demand for both efficient and …
Novel nuclear fusion enhanced water-fueled electric propulsion offers outstanding potential for future space exploration
Wes Faler · Miles Space, Inc.
SSE25-027SmallSat Europe 2025 Technical ProceedingsTalkPDF 52 pp · 4.9 MB
The patented Poseidon™ thrusters use pulsed electrostatic acceleration, a virtual cathode, and pressure drops to create thrust from water vapor using a novel propulsion method. No neutralizer is needed as the exhaust is inherently neutral. …
Orchestrated Ground – Software-Defined, Virtual, Cloud-Native
Marke Clinger, Bruno Destrez · Kratos Defense & Security Solutions, Inc.
SSE25-028SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 359 KB
To address market trends and provide solutions to the issues they create for smallsat operators and GSaaS providers, Kratos developed a new age space strategy built on three key pillars, digitization, virtualization and orchestration. …
The Compact and Radiation Hard Star Tracker – ASTRO© CL
Martin Grimm, Sebastian Colditz, Reinhard Berger, Steffen Hahn, Steffen Schwarz and 1 more · Jena-Optronik
SSE25-029SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 463 KB
The ASTRO© CL is Jena-Optronik’s compact star tracker, which is optimized for small satellites and constellations. The core driver of the ASTRO© CL design is bringing radiation robustness to compact constellation class star trackers. This …
mN class Metal Plasma Thruster for CubeSats and SmallSATS
MAHADEVAN Krishnan · Alameda Applied Sciences Corporation
SSE25-030SmallSat Europe 2025 Technical ProceedingsTalkPDF 18 pp · 1.2 MB
The Metal Plasma Thruster (MPT) is a new class of electric propulsion technology suitable for CubeSats and Small Sats. The thruster uses inert, solid metal pucks as propellant. It uses 45V/~100A/~1ms pulses to convert ~10 µg/pulse of the …
Dedicated Ground Segment Design for Small Satellites
Stefan-Vlad Tudor, Giovanni Zanotti · Leaf Space
SSE25-031SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 269 KB
The growing number of CubeSat and small platform being launched provides a large quantity of opportunities for various kinds of missions, from Earth observation, telecommunications, service delivery, and to scientific research. The …
The VIBES Program: Revolutionizing Earth Observation through Consumer Electronics
Tim Gust, Antonio Garcia, Benny Rievers, Patrik Sieverding, Alexander Koch and 1 more · Institute of Aerospace Technology Bremen; ZARM, University of Bremen; DLR Institute for Satellite Geodesy and Inertial Sensing
SSE25-032SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 319 KB
The satellite research program VIBES (Visionary Ingenuity Boosting European Spacecraft) was established in 2021 at the Institute of Aerospace Technology (IAT) of the City University of Applied Sciences Bremen. VIBES aims at bringing the …
Development of Thermal Control Systems for The Space-borne Optical Payload for New Possibilities and Opportunities for Nanosatellites Applications
Jin-Soo Chang, Minwook Joo, Ohgan Kim, Dong-Jun Choi, Sehyun Seong and 1 more · TelePIX Co., Ltd.
SSE25-033SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 1.2 MB
Based on the many years of accumulated development experiences of space program, TelePIX has successfully developed Space-borne Optical Payload (SOP) for a 6U-class Nanosatellite platform. SOP consists of the Data Processing and Handling …
Making space astronomy instrumentation more affordable with LUVCam
Jean-Christophe Fronteddu · University of Toronto
SSE25-034SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 1.8 MB
The cost of quality scientific instruments has limited access to space-based astronomy. The Little UV Camera (LUVCam) project intends to rectify this and make space astronomy more accessible. LUVCam is a low-cost alternative to existing …
“Andes OBC”: a COTS-Based On-Board Computer for Small Satellite Missions
Sebasthian Ogalde, Eduardo Novoa Carrasco, Ilaria Merli, Jorge Olmos, Carlos E. González · Andes Aerospace; Universidad de Santiago de Chile
SSE25-035SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 477 KB
Andes OBC is an onboard computer (OBC) for CubeSat satellite missions built on commercial off-the-shelf components (COTS). A core feature of its design is full redundancy of every component, implemented to significantly enhance operational …
Design of an ADCS enabled by the development of a digital twin of CubeSat equipped with robotic manipulator
Bartlomiej Koszek, Alvaro Roman Sanchez · KU Leuven
SSE25-036SmallSat Europe 2025 Technical ProceedingsTalkPDF 15 pp · 377 KB
In this research, the authors develop a digital twin of a small satellite equipped with a robotic manipulator to inform the design of an attitude determination and control system (ADCS) for this type of mission. The significance of …
Modular Horizons: Open-Source Innovation in CubeSat Design with the VIBES Program
Isabel Alejandra Parga García, Maik Bleckmann, Tim Gersting, Enes Basata, Tim Gust and 1 more · Hochschule Bremen – City University of Applied Sciences
SSE25-037SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 536 KB
The satellite research program VIBES (Visionary Ingenuity Boosting European Spacecraft) of the Institute of Aerospace Technology (IAT) at the City University of Applied Sciences Bremen with the aim of bringing the consumer electronics …
IBIS and µIBIS radiation hardened single chip true digital Sunsensors and their development path
Johan Leijtens, Frank Stelwagen · Lens R&D B.V.; Systematic Design B.V.
SSE25-038SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 591 KB
Since November 2018, Lens R&D B.V. has been developing a single chip true digital Sunsensor in cooperation with Systematic design B.V. The activities employed in frame of an ESA ARTES AT (advance technology) contract and supported by the …
In-orbit validation of satellite attitude control system through VCUB1 mission
Lara Oliveira, Mairon Wolniewicz, Mariana Barbosa, Andrei Freiberger · Visiona Space Technology
SSE25-039SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 448 KB
The VCUB1 mission is the first Earth observation and data collection satellite developed by a private company in Brazil, Visiona Space Technology. VCUB1 is a 6U satellite with a 3U primary optical payload, capable of performing TDI images …
SatNOGS-COMMS: An Open-Source Communication Subsystem for CubeSats
Manolis Surligas, Agis Zisimatos, Dimitris Moustroufis, Daniel Bita, Victoria Malyshkina and 1 more · Libre Space Foundation
SSE25-040SmallSat Europe 2025 Technical ProceedingsTalkPDF 12 pp · 841 KB
SATNOGS-COMMS is an open-source, open-hardware communications subsystem for CubeSats, developed by the Libre Space Foundation in collaboration with the European Space Agency (ESA). This innovative system combines advanced hardware and …
VCUB1 Conception of Operation
Júlia Saraiva, Priscila Yamada · Visiona Space Technology
SSE25-041SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 852 KB
VCUB1 is the first Earth observation and data collection satellite designed by the Brazilian private sector. The mission VCUB1 successfully completed was to validate the software of three critical subsystems: Attitude and Orbit Control …
Qualification challenges of an SADM using the slipring technology
Adrien GUIGNABERT · Comat
SSE25-042SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 794 KB
The qualification sequence went through the typical path of mechanical and thermal vacuum environments followed by a lifetime operational test under high vacuum and thermal conditions. Functional tests were regularly performed in order to …
Proposal for a Fully Integrated 1U Ion Thruster Using Water as Propellant
Hiroto Saito, Yuichi Nakagawa, Daiki Tomita, Jun Asakawa · Pale Blue Inc.
SSE25-043SmallSat Europe 2025 Technical ProceedingsTalkPDF 3 pp · 396 KB
Space development in the private sector is flourishing, especially in the low-Earth orbit constellation market with small to medium-sized satellites weighing less than several hundred kilograms. Generally, satellites orbiting in low Earth …
Auriga Star Tracker new features
Lionel Oddos-Marcel · Sodern
SSE25-044SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 685 KB
Since February 2019, Sodern’s Auriga star tracker reached TRL9 as part of the successful launch of the first six satellites of the OneWeb constellation. This CMOS multi-head star tracker is now the reference in the market with more than …
Control Moment Gyroscopes – Pros and Cons
Thomas Yen, Afan Huang, Julien Hennequin, Sam Lee · Tensor Tech
SSE25-045SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 442 KB
Control Moment Gyroscopes (CMGs) are advanced attitude control devices used in satellite Attitude Determination and Control Systems (ADCS). Leveraging gyroscopic torque, CMGs provide precise and efficient angular momentum management, …
Refuelling a Sustainable Future in LEO- Introducing LOOP
Neta Palkovitz, Josh Rodenbaugh, Jeroen Wink · Dawn Aerospace
SSE25-046SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 203 KB
Main Author: Dr. Neta Palkovitz The rapidly growing space economy demands innovative solutions for in-orbit refuelling and servicing to achieve sustainability, resilience, and scale of satellite and spacecraft operations. Dawn Aerospace’s …
Vibration Testing of CubeSats: Ensuring Mission Success
Carmine Salzano · PCB Piezotronics
SSE25-047SmallSat Europe 2025 Technical ProceedingsTalkPDF 18 pp · 1.9 MB
The Importance of Vibration Testing in Satellite Development is crucial and there are several reasons listed below: • Qualification Testing: All spacecraft must pass minimum qualification and acceptance testing to be launched. Test …
Innovative Satellite Bus Structures Using Thermoplastic Materials
Hamed Akhavan, João Manuel Cardoso, Caio Adler, Rúben Emanuel Ferreira, João Pedro Alves and 1 more · INEGI
SSE25-048SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 1.6 MB
This study considers the innovative use of reusable thermoplastic materials as a sustainable alternative to aluminum in the construction of satellite bus structures, aligning with circular economy principles. By integrating thermoplastics …
Proposal of water Hall effect thruster system suitable for small satellite
Yuichi Nakagawa, Akira Iwakawa, Kazuya Yaginuma · Pale Blue Inc.
SSE25-049SmallSat Europe 2025 Technical ProceedingsTalkPDF 3 pp · 396 KB
Hall Effect thruster is one of the most popular electric propulsion systems, and it is commonly driven by xenon or other noble gases. It has more than 1000 s of specific impulse, and a relatively high thrust-to-power ratio, typically more …
SIDLOC: Spacecraft Identification and Localization
Manolis Surligas, Agis Zisimatos, Aris Nikas, Manthos Papamatthaiou, Thanos Patsas and 4 more · Libre Space Foundation
SSE25-050SmallSat Europe 2025 Technical ProceedingsTalkPDF 5 pp · 280 KB
SIDLOC (Spacecraft Identification and Localization) is a new transmission scheme proposed by Libre Space Foundation, in collaboration with ESA, SIDLOC aims to improve space safety and mission success rate by establishing an open beaconing …
Edge Computing for Automated Hazard Alerting from Orbit
Sarvesh Garimella · MyRadar
SSE25-051SmallSat Europe 2025 Technical ProceedingsTalkPDF 2 pp · 4.9 MB
This paper will detail multiple advances made to use small satellites for hazard alerting with detail provided about wildfire detection and alerting from Low Earth Orbit (LEO). Historically, satellite observations have been constrained by …
Flight heritage and design updates of the ENPULSION propulsion systems
David Krejci, Alexander Reissner · ENPULSION
SSE25-052SmallSat Europe 2025 Technical ProceedingsTalkPDF 4 pp · 1.7 MB
The first flight ever flight of a Field emission electric propulsion (FEEP) thruster occurred in 2018 using a ENPULSION NANO thruster. Since then, more than 200 heritage ENPULSION NANO systems, 20 higher power MICRO systems and 25 novel …
Reliable Software Development of a Nanosat Attitude Determination and Control System in a Space-Representative Simulator
Mikel Samson, Rhimas Van de Putte, Wim De Munter, Tjorven Delabie, Andrew Hyslop and 1 more · arcsec; European Space Agency
SSE25-053SmallSat Europe 2025 Technical ProceedingsTalkPDF 16 pp · 3.0 MB
The significant growth of the Nanosatellite market is driven by its core advantages: low cost, fast development cycles, and scalability. However, as the market matures and the (scientific) mission potential evolves, the demands for system …
ICARUS – Virtual-Reality based training for Assembly, Integration and Testing
Daniel Twigt, Stefan Brouwer, Petra Ten Hove, Laurens Mathot, Manav Lakhwani Daswani and 4 more · ATG-Europe; ISISPACE; Royal Netherlands Aerospace Centre (NLR)
SSE25-054SmallSat Europe 2025 Technical ProceedingsTalkPDF 6 pp · 667 KB
Satellite Assembly, Integration, and Testing (AIT) is a critical phase in satellite manufacturing, ensuring the functionality and reliability of space-bound assets. AIT engineering requires a diverse skill set including the system …
Control Moment Gyroscopes: a new opportunity in small satellites for enhancing satellite services, profitability and enabling new optical communication
Marco Ruano, Victor Gómez · Sanzar
SSE25-055SmallSat Europe 2025 Technical ProceedingsTalkPDF 3 pp · 153 KB
The growing market for small satellites requires agile, efficient and compact attitude control systems (ACS) to improve mission performance, enable optical satellite communication (quantum) and improve data observation, increasing …
Effects of gravitational time dilation in short-duration balloon satellite flights
Paula Fekete, George Zhang, Johnathon Wilmoth · US Military Academy at West Point
SSE25-056SmallSat Europe 2025 Technical ProceedingsTalkPDF 12 pp · 811 KB
This study investigates the possibility of detecting of gravitational time dilation using chip-scale atomic clocks (CSACs) during high-altitude balloon flights. Leveraging the principles of general relativity, we aim to measure time …
Sub-decimetre orbit determination for LEO satellites in real time: Demonstration of Precise Point Positioning onboard Norsat-TD
Bart Kevers, James Bartle, Jonathan Ward, Gencer Yilmaz, Scott Glazier · Fugro Innovation and Technology; Fugro GB Marine Limited; Fugro Australia Pty Ltd
SSE25-057SmallSat Europe 2025 Technical ProceedingsTalkPDF 8 pp · 1.2 MB
Satellites in Low Earth Orbit (LEO) are commonly equipped with GNSS (Global Navigation Satellite Systems) receivers to obtain real-time positioning, velocity, and time (PVT). Although the highest possible PVT accuracy is obtained by …
Cold sprayed Niobium – first results on material properties for in-space propulsion nozzles
Markus Brotsack, Reeti Singh, Ján KONDÁS · Impact Innovations GmbH
SSE25-058SmallSat Europe 2025 Technical ProceedingsTalkPDF 7 pp · 980 KB
Space propulsion applications require lightweight materials that can withstand high stresses at elevated temperatures. Niobium has a very low density compared to other refractory metals but high strength, i.e. a high strength-to-weight …