33 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 33 total) CFRP grid-stiffened upper interstage structure Achievements and status: Both cylinders have been manufactured up to spec and shipped to the end-user. Both cylinders have been accepted by the end-user Benefits: Tailored lattice design parameters to optimise the design for the defined load cases. Mass savings in comparison to traditional monolithic designs of around 50% (of the composite part, without mounted equipment) Netherlands GSTP GT27-172MS ATG EUROPE B.V. 2023 - 2025 CFRP grid-stiffened upper interstage structure Pre-Phase A System Study of a Commercial-Scale Space-Based Solar Power (SBSP) System for Terrestrial Needs The growth of the human population, industrialization of developing countries and rising living standards for the population are continuously increasing global energy demand, that in the next 30 years is forecast to double. Italy Preparation 23-P-M- TEC-01 THALES ALENIA SPACE ITALIA SPA 2023 - 2023 Pre-Phase A System Study of a Commercial-Scale Space-Based Solar Power (SBSP) System for Terrestrial Needs LPSS-380 Separation System Development Activity addresses the necessity of developing a competitive European Sep Spain GSTP G627-083MS AIRBUS DEFENCE AND SPACE S.A.U. 2017 - 2023 LPSS-380 Separation System Development Human-In-the-Loop Flight Vehicle Engineering for Exploration Missions This activity will achieve a preliminary design of a flight vehicle for future Moon exploration missions involving astronauts in the loop to improve robustness and reliability of the flight system. The nominal scenario starts in Near-rectilinear Halo Orbit (NRHO) and ends with pinpoint landing close to the Moon South pole. The vehicle will be designed to allow astronauts to interact, monitor and command the flight vehicle in order to react to uncertainties, errors and contingencies. Italy TDE T318-601MP THALES ALENIA SPACE ITALIA SPA 2019 - 2023 Human-In-the-Loop Flight Vehicle Engineering for Exploration Missions Aerocapture demonstration mission The AERODEM is an ESA demonstration mission that will implement an aerocapture phase in order to provide an atmospheric ∆V instead of a standard chemical one for orbiting a SpaceCraft around Mars. The aerocapture technique currently studied relies on a discrete event drag modulation technique that modifies only once the aerocapture module ballistic coefficient by separating / retracting the heatshield. France Preparation 21-P-M-HRE-06-b ArianeGroup 2022 - 2023 Aerocapture demonstration mission Miniaturised distributed optical fibre sensors (DOFS) based on photonic integrated circuits (PICs) for space applications Distributed optical fibre sensors (DOFS) are highly suitable for monitoring temperature, vibration and strain using physical principles such as Raman, Rayleigh and Brillouin backscatter. They convert a standard telecom infrastructure to a sensor network providing thousands of virtual sensors per km using the intrinsic light/glass interaction during propagation. United Kingdom Discovery ETD 2020-03-b Worthy Photonics 2020 - 2023 Miniaturised distributed optical fibre sensors (DOFS) based on photonic integrated circuits (PICs) for space applications Development of a Flexible Thermal Protection System for Deployable Inflatable Heatshields and Hypersonic Decelerators Deployable and inflatable heatshield concepts have a very high potential to extend European capabilities for future Martian lander missions. Such concepts would allow to approach landing zones in the Martian highlands which cannot be reached with current state-of-the-art entry, descent and landing (EDL) technology, mainly due to the very low density of the Martian atmosphere. Alternatively, a deployable or inflatable heatshield concept could allow for an increased landed mass in the Martian lowlands. ; ; United Kingdom TDE T721-615MT VORTICITY LTD 2020 - 2023 Development of a Flexible Thermal Protection System for Deployable Inflatable Heatshields and Hypersonic Decelerators Damping behaviour in AM material based parts Vibration is one of the main issues when it comes to the design of space hardware and as such, it should be considered in the early phases of spacecraft design. When this factor is overlooked, a later identification of vibration and shock issues causes a deep impact on the performance of the spacecraft. Often the only solutions available, such as a dedicated damper, are detrimental for design, cost and schedule of the mission. ; Germany GSTP GT1A-007MS SPACE STRUCTURES GMBH 2020 - 2023 Damping behaviour in AM material based parts Control/structure co-design for planetary spacecraft with large flexible appendages Classical control design techniques used for flexible spacecraft are based on single axis design approaches to control the rigid-body motion complemented by low-pass and notch filters to suppress the resonant peaks of the low-frequency flexible modes. These techniques are inherently relying on a priori knowledge of the structural flexible modes and introduce significant conservatism in the control and structural design, dictated by the need to separate the controller bandwidth from the flexible modes frequency. United Kingdom TDE T205-121SA AIRBUS DEFENCE AND SPACE LIMITED 2020 - 2022 Control/structure co-design for planetary spacecraft with large flexible appendages De-risk assessment: LESSON - LargE Scale Struts prOductioN The production process of full-CFRP struts, was before only suitable for low volume production rates (~10 struts/month) and including worker safety critical processes. This approach had to be reviewed and changed to enable production rates >100/month and improve worker safety. The activity focused on the: Germany GSTP G617-241TAfl SPACE STRUCTURES GMBH 2020 - 2022 De-risk assessment: LESSON - LargE Scale Struts prOductioN Pagination 1 2 3 4 ›› Next page Last » Last page Filter by Programme GSTP (18) TDE (8) Discovery (5) Preparation (2) Filter by Start Year 2020 (11) 2021 (4) 2014 (3) 2017 (3) 2019 (3) 2015 (2) 2018 (2) 2023 (2) 2013 (1) 2016 (1) 2022 (1) Filter by End Year 2022 (9) 2021 (7) 2023 (7) 2019 (3) 2020 (3) 2016 (1) 2017 (1) 2018 (1) 2025 (1) Filter by Keywords 20-Structures & Pyrotechnics (2) 32-Clean Space (2) 38-Advanced Manufacturing (2) 1-Avionics and Processing (1) 1-Launchers (1) 1-Systems (1) 3-Platforms / Others (1) 6-EnVision (1) aerobreaking (1) aerocapture (1) Ariadna (1) athmospheric drag (1) bio-inspired (1) Biomimetics (1) Biomimicry (1) Distributed optical fibre sensors (1) DOFS (1) Earth observation (1) HAPS (1) in-space manufacturing (1) inflatable (1) inflatable structure (1) ISRU (1) lunar base (1) lunar caves (1) lunar habitat (1) Mars (1) Moon base (1) moon village (1) Optical (1) Orbital capture (1) Orbit insertion (1) Payload (1) photonic integrated circuits (1) PICS (1) Re-entry (1) Robotics (1) UAV (1) Filter by Contractor AIRBUS DEFENCE AND SPACE LIMITED (2) ATG EUROPE B.V. 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