Development of an intrusive technique for particles collection in rockets plume-Reference-Cited by-同舟云学术

Development of an intrusive technique for particles collection in rockets plume

Published:2019-05 Issue: Volume:158 Page:361-374
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Carlotti Stefania,Maggi Filippo^ORCID,Ferreri Alessandro,Galfetti Luciano,Bisin Riccardo,Saile Dominik^ORCID,Gülhan Ali,Groll Christopher,Langener Tobias

Funder

EMAP (Experimental Modeling of Alumina Particulate in Solid Booster) project, an ESA

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. D. Reydellet, Performance of Rocket Motors with Metallized Propellants.

2. Thermal radiation from the exhaust plume of an aluminized composite propellant rocket;Carpenter;J. Spacecraft Rockets,1964

3. Impact of rocket exhaust plumes on atmospheric composition and climate–an overview;Voigt;EUCASS Proceedings Series–Advances in AeroSpace Sciences,2013

4. Ozone decomposition kinetics on alumina: effects of ozone partial pressure, relative humidity and repeated oxidation cycles;Sullivan;Atmos. Chem. Phys.,2004

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