484 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 484 total) ISS Crew Procedures Web Based Authoring For ISS, on board astronaut's procedures are following a standard to allow for efficient and flexible flight operations. The standard - ODF (onboard data file) Stds - prescribes semantic and format of any all on board crew procedures. The procedure documents are in XML format, with an ISS specific schema used. Ireland GSTP GT17-107SW SKYTEK 2018 - 2019 ISS Crew Procedures Web Based Authoring De-risk assessment: Development of novel light source for implementations in high precision frequency metrology N/A Ireland GSTP G617-241TAah PILOT PHOTONICS LTD. 2018 - 2019 De-risk assessment: Development of novel light source for implementations in high precision frequency metrology Optopyrotechnics Technology for Next Generation Launchers Launchers have a large number of pyrotechnic functions that are vital for a range of critical functions from engine ignition, control of the propulsion system, passivation, stage and fairing separation and in the case of emergency launcher destruction. Today European launchers rely on conventional pyrotechnics that are activated by passing an electric current through a bridge wire which results in local heating. Optopyrotechnics is a replacement technology that uses laser pulses to ignite the key pyro functions. ; Norway GSTP G614-007MM KONGSBERG DEFENCE AND AEROSPACE AS 2014 - 2019 Optopyrotechnics Technology for Next Generation Launchers High stability laser for interferometric Earth Gravity measurements in the context of a Next Generation Gravity Mission (NGGM) Potential concepts and their related technologies for a Next Generation Gravity Mission (NGGM) as a follow-up to the GOCE mission are currently being studied. The mission will be designed to monitor the variations of the Earth?s gravity field to a level that allows the study of mass transport processes not only in solid Earth but also at the Earth surface layer and in the lower atmosphere. Germany GSTP G611-017MM SPACETECH GMBH 2015 - 2019 High stability laser for interferometric Earth Gravity measurements in the context of a Next Generation Gravity Mission (NGGM) De-risk assessment: ORBITA In-orbit diagnostics Current technologies for measuring the ion velocity of ion thrusters (and therefore their efficiency) are based on slow measurements that can take up to 8 hours against seconds for new technologies based on fluorescence, optical fibre spectrometry or laser spectroscopy. ORBITA aims to select and enhance one of these technologies to develop a diagnostic device capable of performing real-time measurements of thruster plumes. United Kingdom GSTP G617-241TAh AVS Added Value Solutions UK Ltd. 2017 - 2019 De-risk assessment: ORBITA In-orbit diagnostics Q-Switched Optical Master Oscillator QOMA 2 The building block shall maintain the two novel but proven technologies of the previous activity pumping at 885 nm as well as multisegmented high dopping crystals). The new technical objectives of this activity are: extending its energy up to 10-15mJ, with a repetition rate from 50 Hz up to 100 Hz maintaining same pulse length, beam spatial and temporal stability and M2. To that purpose, a more powerful pumping-diode stack shall be used as well as a specially designed Nd:YAG multi-segmented crystal rod of higher diameter and increased doping concentration. France GSTP G617-184MM Raymetrics S.A. 2015 - 2019 Q-Switched Optical Master Oscillator QOMA 2 Advanced manufacturing and integration techniques for TT C transponders/transceivers The use of the VLSI technologies (through high density, low power consumption digital ASICs) together with RF miniaturisation techniques (Analogue ASIC, MMIC,System on a chip etc.) are being used in many devices in order to develop lighter and smaller transponders. Particular examples of these are: The TTC subsystem for the future deep space missions, such as Bepi-Colombo. Lander and orbiter proximity link transponders/transceivers. Italy GSTP G617-037ET THALES ALENIA SPACE ITALIA SPA 2016 - 2019 Advanced manufacturing and integration techniques for TT C transponders/transceivers Xenon Micro-Pressure Regulator The state-of-the-art in Xenon feeding systems, specifically pressure control devices, which reduce the gas pressure from storage level, usually upwards of 100bar, to the pressures acceptable by the thrusters? XFC (i.e. circa 2 bar) is the Bang-bang pressure regulation unit (BPRU); such an equipment was, as an example, used in the Smart-1 mission. The BPRU allows extra safety, never allowing contact between the high and low pressure stages. Portugal TDE, GSTP G617-147MP OMNIDEA - ENGENHARIA DE SISTEMAS LD 2014 - 2019 Xenon Micro-Pressure Regulator Electron Beam Welding for Safety Critical Space Applications The precision welding of metallic joints plays an important role in the production of components for space applications. In order to meet the demanding levels required, metallic joints must be produced which have the correct dimensional tolerance, are free from defects and exhibit the correct mechanical and corrosion performance. In particular, in propulsion systems all valves and pipes have welds which must be leak tight and prevent safety hazardous propellants from leaking. United Kingdom GSTP G617-132QT TWI LIMITED - THE WELDING INSTITUTE 2015 - 2019 Electron Beam Welding for Safety Critical Space Applications Mission Preparation Environment (MORE) Evolution A recently completed activity in the offline preparation environment for managing the database, procedure and other "static" configuration data, has demonstrated a considerable advances through innovative concepts combined with latest technology, resulting in the MORE framework, specifically including the MORE Data Store (MDS). The success of this study has raised new questions about vunerability of the online system to local, dynamic configuration changes. 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