5 projets européens trouvés
Recherche sur 125080 projets européens
TERMINÉ
Consortium for Hall Effect Orbital Propulsion System (CHEOPS)
Date du début: 1 nov. 2016, Date de fin: 30 avr. 2020,
CHEOPS proposes to develop three different Hall Effect Thruster electric propulsion systems: a dual mode EPS for GEO applications, a low power for LEO applications and a >20 kW high thrust EPS for exploration applications. Each of these will be developed according to market needs and drivers applying incremental technology changes to existing EPS products. The development approach will follow the ...
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14
Participants partenaires
TERMINÉ
Pulsed Chemical Rocket with Green High Performance Propellants (PulCheR)
Date du début: 1 janv. 2013, Date de fin: 31 déc. 2015,
PulCheR (Pulsed Chemical Rocket with Green High Performance Propellants) is a new propulsion concept in which the propellants are fed in the combustion chamber at low pressure and the thrust is generated by means of high frequency pulses, reproducing the defence mechanism of a notable insect: the bombardier beetle.The radical innovation introduced by PulCheR is the elimination of any external pres ...
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11
Participants partenaires
TERMINÉ
SPAce exploration Research for Throttleable Advanced eNgine (SPARTAN)
Date du début: 1 mars 2011, Date de fin: 31 août 2014,
The SPARTAN research aims at developing a throttable propulsion technology, which is mandatorily needed for any planetary soft and precision landing. It relies on the hybrid engine technology, exploiting its capability of being throttled and its proper performances.This research is complementary to ESA TRP and Piedmont Regional development programs. It implements and strengthens the technological ...
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8
Participants partenaires
TERMINÉ
In-line characterisation of nanoparticles using a combination of analytical techniques in real time (In-Sight)
Date du début: 1 mai 2011, Date de fin: 30 avr. 2014,
In-Sight is a SME-driven project on the in-line characterisation of nanoparticles during nanomaterial manufacturing. This in-line characterisation is the ultimate goal. Within the time-span of the project (3 years) it is our objective to show that a combination of analytical techniques that are capable of real time measurements will provide valuable information for the nanoparticle user. It is our ...
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10
Participants partenaires
TERMINÉ
HeliconPlasmaHydrazine.COmbinedMicro (HPH.com)
Date du début: 1 déc. 2008, Date de fin: 31 mai 2012,
The objective of the research program is to design, optimize and develop a space plasma thruster based on helicon-radio-frequency technology and its application to a nano-satellite for attitude and position control. Moreover a detailed feasibility study will be also conducted to evaluate the possibility of using the plasma thruster to heat and decompose a secondary propellant. The feasibility stud ...
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