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Heat Transfer Measurements in a Water-Cooled Rocket Combustion Chamber Operated with Oxygen/Methane Mixtures at the Masc...

Vingert, Lucien Grenard, Philippe Lévy, Frédéric Nicole, Aurélie Dorey, Luc-Henry Benito, Miguel Martin

A test series aimed at investigating wall temperatures and heat fluxes in a subscale rocket engine combustion chamber operated with oxygen and methane was achieved at the Mascotte test facility. A total of nearly one hundred and fifty stabilized operating points were reached, enabling to cover a wide operating domain, ranging from subcritical to su...

A Rocket Engine under a Magnifying Glass

Vingert, L. Ordonneau, G. Fdida, N. Grenard, P.

Even though the technology of cryogenic rocket engines is well mastered today, and has been applied successfully in many launchers all over the world, research activities on the various elementary or coupled processes involved in these complex systems are still relevant and useful for future developments, cost reduction, and knowledge improvement.T...

Publication search with LIQUID ROCKET ENGINE as keyword

Heat Transfer Measurements in a Water-Cooled Rocket Combustion Chamber Operated with Oxygen/Methane Mixtures at the Masc...

A Rocket Engine under a Magnifying Glass

Publication search
with LIQUID ROCKET ENGINE as keyword