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ESA has traditionally specified space systems using a document-based approach, and is now in a transition process towards the digitalisation of systems engineering activities. At the same time, space industry companies have their own internal set of best practices and experience with Model-Based Systems Engineering (MBSE).
To solve this problem, ESA initiated this study led by CGI in partnership with OHB to identify a way to harmonise the different MBSE approaches from industry and compile the information into a concise book.
CGI Deutschland B.V.
RUAG Space Germany GmbH
A GSTP De-Risk Framework with RUAG Space Germany designed and demonstrated a novel, compact and robust sensor head for angular sensors for space mechanisms, using modern and advanced materials and manufacturing methods.
The final performance tests provided evidence in terms of high precision manufacturability of ceramic packages.
The robust design was found to be suitable for the harsh space environment
RUAG Space Germany GmbH
This study aimed to demonstrate the feasibility, use and functionality of carbon fibre-reinforced flexible epoxy (CFRFE) materials for self-deployable space structures (such as deployable tape-spring hinges) by designing, simulating, manufacturing, testing and correlating a classic (100% carbon fibre-reinforced plastic -rigid resin- CFRP) deployable tape-spring hinge and a CFRFE deployable tape-spring hinge and compare their mechanical and dynamic behaviours.
INGENIERIA PROSIX SL
The project aimed to establish a structured approach to an optimised part or component by applying Concurrent Design methods. It intended to incorporate all necessary disciplines and competencies that are required for a potential spacecraft part. Within the activity, advanced manufacturing included various novel techniques, not only additive manufacturing. It means that the Concurrent Design approach was developed for the engineering of units to be built with a broad range of advanced manufacturing technologies.
OHB System AG
Motivation: This study aimed to develop promising robotic fabrication methodologies for a fibre-based in-situ robotic fabrication process, for application in a lunar habitat as an alternative to existing additive manufacturing methodologies. Previous work has verified that fibre composite fabrication processes are capable of a high degree of automation and structural performance.
Universität Stuttgart
<p>Augmented reality (AR) displays are image-forming systems that use a set of optical, electronic, and mechanical components to generate images somewhere on the optical path between an observer’s eyes and the physical object to be augmented.</p><p>AR provides a live direct or indirect view of a physical, real-world environment and augments (or supplements) this view with computer-generated input such as sound, video, graphics, 3D objects or GPS data.</p><p>AR improves users’ experience by enabling them to interact with and learn from whatever they are
TERMA A/S
Recently, a variety of satellite constellations, some of them featuring over a thousand satellites, were announced. While similar concepts for large constellations already existed in the past, existing satellite constellations hardly ever feature triple-digit satellite quantities. At the time of writing, the world’s largest constellation is operated by Planet Labs and consists of 190+ Dove spacecraft.
TU Braunschweig
The DTN-EO study was initiated in order to research the performance of DTN in future missions, particularly Earth observation and constellation-type missions. In the original proposal, ESA stipulated three scenarios which were to be tested: Earth observation, constellation, and exploration missions. These scenarios built upon each other, starting with an Earth observation-centric mission such as the Sentinel missions, before moving to a large constellation. Ultimately, the DTN network from the first two scenarios was expanded to represent a deep-space exploration mission.
GMV
While the vast majority of space debris still stems from explosion events of satellites and rocket upper stages, current forecasts state that collisions, such as those between the Cosmos 2251 and Iridium 33 satellites in 2009, will play a dominant role in the mid-term future when a critical spatial density of satellites has been reached. In order to assess the risks emanating from space debris, a deeper understanding of the formation and residence time of breakup debris in orbit is essential for operational activities.
Fraunhofer Gesellschaft
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