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Results 1 - 10 of 1316
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Consortium for Hall Effect Orbital Propulsion System
ID: 730135
Start date: 2016-11-01, End date: 2020-04-30
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...
Programme: H2020-EU.2.1.6.2.
Record Number: 206269
Last updated on: 2017-05-17
Characterization of Wall Temperature Effect during Transition of Hypersonic flow over a Cone By Experiments And Numerical Simulations
ID: 263182
Start date: 2011-06-01, End date: 2013-05-31
The development of secure and re-usable re-entry vehicle requires the complete control of the heat distribution on its Thermal Protection System (TPS). During the most critical re-entry phase, the hypersonic flow along the vehicle initiates a laminar boundary layer inside of ...
Programme: FP7-SPACE
Record Number: 99134
Last updated on: 2017-05-26
Mejores escudos térmicos para fenómenos peligrosos
Las naves espaciales se calientan intensamente cuando reingresan en la atmósfera terrestre. Un grupo de científicos se encuentra estudiando un fenómeno que conduce a un aumento súbito y enorme del flujo de calor con el fin de diseñar un mejor sistema de protección térmica.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-03-01
Available languages: DE, EN, ES, FR, IT, PL
Better heat shields for dangerous phenomena
Spacecraft are subject to massive heating on re-entry into the Earth's atmosphere. Scientists are studying a phenomenon leading to a sudden and sharp increase in heat flux for better design of thermal protection.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-03-01
Available languages: DE, EN, ES, FR, IT, PL
Des boucliers thermiques améliorés pour les phénomènes dangereux
Les engins spatiaux sont soumis à un échauffement considérable lorsqu'ils pénètrent à nouveau dans l'atmosphère terrestre. Des scientifiques étudient un phénomène entraînant une augmentation soudaine et marquée des flux de chaleur afin d'améliorer la conception de la protection thermique.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-03-01
Available languages: DE, EN, ES, FR, IT, PL
Lepsze osłony termiczne chroniące przed niebezpiecznymi zjawiskami
Pojazdy kosmiczne wchodzące w atmosferę ziemską ulegają silnemu nagrzewaniu. Naukowcy badają zjawisko powodujące gwałtowny wzrost strumienia cieplnego, aby projektować skuteczniejsze osłony termiczne.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-05-20
Available languages: DE, EN, ES, FR, IT, PL
Scudo termico migliore per fenomeni pericolosi
I veicoli spaziali sono soggetti a riscaldamento molto elevato al rientro nell'atmosfera terrestre. Alcuni scienziati stanno studiando un fenomeno che causa un aumento improvviso e netto del flusso di calore per progettare meglio la protezione termica.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-03-01
Available languages: DE, EN, ES, FR, IT, PL
Bessere Hitzeschilde gegen gefährliche Phänomene
Raumflugkörper werden bei ihrem Wiedereintritt in die Erdatmosphäre sehr stark aufgeheizt. Wissenschaftler untersuchen ein Phänomen, das zu einer plötzlichen und starken Zunahme des Wärmestroms führt, zwecks besserer Gestaltung des Wärmeschutzes.
Programme: FP7-SPACE
Record Number: 90591
Last updated on: 2013-03-01
Available languages: DE, EN, ES, FR, IT, PL
Final Report Summary - TRANSHYBERIAN (Characterization of Wall Temperature Effect during Transition of Hypersonic flow over a Cone By Experiments And Numerical Simulations)
Executive Summary: The development of secure and re-usable re-entry vehicle requires the complete control of the heat distribution on its Thermal Protection System (TPS). During the most critical re-entry phase, the hypersonic flow along the vehicle initiates a laminar bound...
Programme: FP7-SPACE
Record Number: 140207
Last updated on: 2014-07-08
Laser Ignition Technology for Rocket Engines
ID: 262874
Start date: 2011-06-01, End date: 2013-05-31
Lasers ignition of propellants offers a number of advantages as compared to existing ignition systems. The maturity and miniaturization of laser ignition devices have paved the way from laboratory experiments demonstrating the basic principle to component/subsystem validation...
Programme: FP7-SPACE
Record Number: 99132
Last updated on: 2017-05-26
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List retrieved on: 2017-05-28
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