Experimental Investigation of a Monopropellant Thruster Using Nitrous Oxide

Nitrous oxide is a monopropellant with potential for use in propulsion systems for orbit correction, positioning and attitude control of satellites. This paper presents experimental results with a 2N thruster prototype employing nitrous oxide gas decomposed by a rhodium oxide catalyst supported on a...

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Détails bibliographiques
Publié dans:Journal of Aerospace Technology and Management
Auteurs principaux: Luciano Hennemann, José Carlos de Andrade, Fernando de Souza Costa
Format: Artigo
Langue:Inglês
Publié: Ministério da Defesa 2014
Sujets:
Ingeniería
KEYWORDS
Nitrous oxide
Satellite propulsion
Propulsive efficiency
Rhodium oxide catalyst
Accès en ligne:https://www.redalyc.org/articulo.oa?id=309432631002
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