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Replacement of hydrazine for orbital and launcher propulsion systems
ID: 640376
Anfangsdatum: 2015-01-01, Enddatum: 2017-12-31
"The project deals with the replacement of hydrazine within space propulsion systems. It improves significantly the ADN-based propellants currently existing and enables the replacement of hydrazine within the whole operational area of currently used hydrazine propulsion...
Programme: H2020-EU.2.1.6.1.
Record Number: 193718
Last updated on: 2017-09-04
Periodic Reporting for period 1 - Rheform (Replacement of hydrazine for orbital and launcher propulsion systems)
"Propellants are chemical substances used in a rocket engine to generate thrust. One of the most used liquid propellants for space propulsion systems is hydrazine. Hydrazine is typically used as monopropellant, which means that it reacts without a separate oxidizer hydrazine...
Programme: H2020-EU.2.1.6.1.
Record Number: 185767
Last updated on: 2016-06-29
Feasibility and Definition of a Triple Core Lockstep ARM System-on-Chip for Space Applications
ID: 640354
Anfangsdatum: 2015-02-01, Enddatum: 2017-02-28
Computers are used in a variety of space-borne equipment for numerous on-board applications and processors are at the core of these equipment. However, currently existing space-grade processors are not suitable to be used in the next generation spacecraft computing platforms...
Programme: H2020-EU.2.1.6.1.
Record Number: 193716
Last updated on: 2017-09-04
Periodic Reporting for period 1 - MaMMoTH-Up (Massively extended Modular Monitoring for Upper Stages)
Today, the amount of telemetry data from the sensors in the upper stages of a launch vehicle is very restricted, due to limited on-board-processing capacities combined with limited data bandwidth to ground. As a result, no detailed information about the various phases of the...
Programme: H2020-EU.2.1.6.1.
Record Number: 190254
Last updated on: 2016-11-14
Massively extended Modular Monitoring for Upper Stages
ID: 637616
Anfangsdatum: 2015-05-01, Enddatum: 2018-04-30
Today, the amount of telemetry data from the sensors in the upper stages of a launch vehicle is very restricted, due to limited on-board-computing capacities combined with limited data bandwidth to ground. As a result, no detailed information about the various phases of the...
Programme: H2020-EU.2.1.6.1.
Record Number: 193510
Last updated on: 2017-09-11
advanced Concept for laser uplink/ downlink CommuniCation with sPace Objects
ID: 637595
Anfangsdatum: 2015-06-01, Enddatum: 2017-09-30
C3PO: advanced Concept for laser uplink/ downlink CommuniCation with sPace Objects represents a radical improvement in performance of existing ground to low earth orbit communication systems in terms of weight reduction, on-board power consumption, data rate and communication...
Programme: H2020-EU.2.1.6.1.
Record Number: 193508
Last updated on: 2017-08-29
Ground Demonstration of Plant Cultivation Technologies and Operation in Space for Safe Food Production on-board ISS and Future Human Space Exploration Vehicles and Planetary Outposts
ID: 636501
Anfangsdatum: 2015-03-01, Enddatum: 2018-12-31
Humanity’s plans to further explore space require the development of bio-regenerative life support systems and in particular plant cultivation. Plants contribute to all major life support functions by producing food and oxygen, reducing carbon dioxide and recycling water and...
Programme: H2020-EU.2.1.6.1.
Record Number: 193405
Last updated on: 2017-09-11
Periodic Reporting for period 1 - EDEN ISS (Ground Demonstration of Plant Cultivation Technologies and Operation in Space for Safe Food Production on-board ISS and Future Human Space Exploration Vehicles and Planetary Outposts)
A critical component of future human exploration to other worlds will be the sustainable supply of edible food for crew members without constant resupply from Earth. Developing innovations regarding food cultivation in closed-loop systems are becoming an essential integral...
Programme: H2020-EU.2.1.6.1.
Record Number: 190324
Last updated on: 2016-11-14
Hybrid Propulsion Module for transfer to GEO orbit
ID: 634534
Anfangsdatum: 2015-02-01, Enddatum: 2018-01-31
Independent access to space is a key component of the European Space Policy. The competition is increasing in this area both for the full launching systems and the key subsystems. Cost-effectiveness becomes the main driving factor.HYPROGEO ambition is to study a propulsion...
Programme: H2020-EU.2.1.6.1.
Record Number: 193294
Last updated on: 2017-09-04
Periodic Reporting for period 1 - HYPROGEO (Hybrid Propulsion Module for transfer to GEO orbit)
Independent access to space is a key component of the European Space Policy. The competition is increasing in this area both for the full launching systems and the key subsystems. Cost-effectiveness becomes the main driving factor.HYPROGEO ambition is to study a propulsion...
Programme: H2020-EU.2.1.6.1.
Record Number: 190152
Last updated on: 2016-11-08
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List retrieved on: 2017-10-20
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