437 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 437 total) De-risk assessment: Ceramic Packages for Magneto-resistive Sensors 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 Germany GSTP G617-241TAo RUAG Space Germany GmbH 2017 - 2020 De-risk assessment: Ceramic Packages for Magneto-resistive Sensors Improvement, Automated Source-code-based Testing State-of-the-art in automated unit/integration testing is a semi-automated approach for which the test environment is established manually, while execution of tests is automated. In contrast to that, the FAST approach already automates building of the test environment and the stimulation of the software, complemented by recording of input-output vectors, observed properties, anomalies and evaluation by metrics and filtering algorithms. Germany GSTP G617-154SW Dr. Rainer Gerlich BSSE System and Software Engineering 2015 - 2020 Improvement, Automated Source-code-based Testing Enabling technologies for piezo-based deformable mirrors in active optics correction chains The increasing need for higher resolution of space optical imaging has prompted the study of novel technologies that can improve the imaging performance beyond what is currently achievable by classical optical systems. Active/adaptive optics is a very promising example of such technologies, allowing to correct for in-flight effects (such as thermo-elastic deformations, radiation effects on optical materials, gravity release, microvibrations, etc.) which impact the optical quality of space instruments. Germany GSTP G617-276MM OHB System AG 2018 - 2020 Enabling technologies for piezo-based deformable mirrors in active optics correction chains Passive damped deployment of full composite structures 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. Germany Discovery ITI76 INGENIERIA PROSIX SL 2018 - 2020 Passive damped deployment of full composite structures Maritime Adaptive GNSS Safety concept (MAGS) The MAGS project focused on developing a Maritime Adaptive GNSS Safety Concept to support mariners, particularly within the vicinity of ports. Germany Discovery 15/113 DLR 2018 - 2020 Maritime Adaptive GNSS Safety concept (MAGS) De-risk assessment: Adjustable Cryo PCM blanket Achievements and status: Space applications: 10 Space applications identified. 2 Space applications assessed with ESATAN Derivation of requirements: Development requirements have been established and demonstrator requirements derived. Investigations freezing point depression: Molecular Dynamics Simulations and DSC Breadboard Tests have shown, that freezing point depression according to Gibbs Thomson is not feasible in the required scale. Thermal Performance Test: Phase Change could not be clearly detected. Germany GSTP G617-241TAbx RST ROSTOCK SYSTEM-TECHNIK GMBH 2019 - 2020 De-risk assessment: Adjustable Cryo PCM blanket Preliminary Activities for a Mars Balloon Probe . Germany GSTP G637-001TFg Mars Society Deutschland e.V. 2017 - 2020 Preliminary Activities for a Mars Balloon Probe Material Characterization Service Efficiency Increasing This activity aims at increasing the efficiency and decreasing the turnaround time of material testing capabilities in novel cryogenic fluids, notably liquid hydrogen (LH2). Germany GSTP GT17-151MS ENERGIE TECHNOLOGIE GMBH 2018 - 2020 Material Characterization Service Efficiency Increasing De-risk assessment: Lithographic Manufacturing of Monolithic Ceramics for Stable Structures in Space N/A Germany GSTP G617-241TAv Airbus Defence and Space GmbH 2017 - 2020 De-risk assessment: Lithographic Manufacturing of Monolithic Ceramics for Stable Structures in Space Design of space hardware using a CDF like methodology (AMCDF) 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. 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