260 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 260 total) Contactless asteroid orbit modification system MOSAIC and bindary asteroid orbit modification KABOOM KABOOM We study a low-cost interplanetary mission to demonstrate the capability of artificially modifying the orbit of a small (250 ton) binary asteroid body. The targeting spacecraft survives the slow (~1 m/s) impact to carry out the orbit modification measurement afterwards. Methodology: Spain Discovery 2012-5 Politechnico di Milano 2012 - 2013 Contactless asteroid orbit modification system MOSAIC and bindary asteroid orbit modification KABOOM UHF Antenna for Environmental Satellites A successful test campaign has been performed over the UHF antenna. The UHF ANTENNA has been tested from the RF point of view and all required performances were compliant. The vibration test campaign can be considered successful since: No damage was detected during the overall vibration and shock (qualification levels) test sequence: Spain GSTP AO06-20EE SENER TAFS, S.A.U. 2012 - 2013 UHF Antenna for Environmental Satellites Deep Space Navigation with Pulsars (parallel 2) The XNAV concept has been analysed in detail. The performances obtained from simulations have been validated successfully using real data from XMM-Newton space telescope. The performances obtained using real data are not in line with the XNAV performances (100 m for the Crab pulsar) due to limitations in the XMM-Newton instrument operations. We have been forced to use a source much fainter than the Crab pulsar and surrounded by a background much stronger than expected. Spain Discovery 2012-13 GMV 2012 - 2013 Deep Space Navigation with Pulsars (parallel 2) Contactless Earth-bound object modification system COBRA and binary asteroid orbit modification system BEAST BEAST aims to modify the orbital period of the small secondary object of a binary asteroid by kinetic impact. BEAST analyses a commercial LEO platform accommodating as payload the impactor and GNC system with total mission cost below 150 M€. The objective of the Cobra mission is to use a conventional chemical thruster to modify the orbit of a man-made object through plume impingement. The proposed concept uses a standard satellite platform with a modified payload to suit mission needs. Spain Discovery 2012-4 GMV 2011 - 2013 Contactless Earth-bound object modification system COBRA and binary asteroid orbit modification system BEAST EO processing library (former: End-to-end simulation framwork for EO missions) Spain Discovery 2011-31 GMV 2011 - 2013 EO processing library (former: End-to-end simulation framwork for EO missions) Requirement and I/F definition for future OBCP building block The OBCP-BB study has performed the following tasks: Assessment of current OBCP implementations for Space systems, considering both Application procedures (OBAPs) and Operation procedures (OBOPs), and providing some statistics figure about the OBCPs used in different ESA missions and projects Assessment of the ECSS-E-ST-70-01C standard particularly in the context of the specification of the OBCP software building block in the FSW Reference Architecture. The analysis has covered both the OBCP concept and the system capabilities defined by the ECSS standard. Spain GSTP G522-001SW GMV AEROSPACE AND DEFENCE, SA 2011 - 2012 Requirement and I/F definition for future OBCP building block Smart Telemetry Demonstration Spain Discovery 2011-19 DEIMOS SPACE SL 2011 - 2012 Smart Telemetry Demonstration Feasibility Study of an All European Klystron for deep Space Communications Spain Discovery 2010-41 AURORA SOFTWARE AND TESTING SL 2010 - 2012 Feasibility Study of an All European Klystron for deep Space Communications SSA RADAR AND OPTICAL SENSOR DATA FUSION FOR ORBIT DETERMINATION OF GTO AND GEO OBJECTS The main conclusions of the project are: Spain GSTP G532-003GR GMV AEROSPACE AND DEFENCE, SA 2011 - 2011 SSA RADAR AND OPTICAL SENSOR DATA FUSION FOR ORBIT DETERMINATION OF GTO AND GEO OBJECTS CFI Space Debris 10/01a Spain Discovery 2010-7 UNIVERSIDAD POLITECNICA DE MADRID 2010 - 2011 CFI Space Debris 10/01a Pagination « First First page ‹‹ Previous page … 15 16 17 18 19 20 21 22 23 … ›› Next page Last » Last page Filter by Programme Discovery (124) 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