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Mascotte

Our main pages on this subject:

1.ONERA - Fundamental and Applied Energetics (DEFA) - References
 Research on the combustion of cryogenic propellants on the Mascotte test bench...
 
2.Mascotte, a cryogenic combustion research test bench - ONERA / DEFA-EN
 Mascotte, a cryogenic combustion research test bench - ONERA / DEFA-EN... Mascotte, a Test Bench for Cryogenic Propellant Combustion Studies... The Mascotte test bench was developed at Onera for studying combustion processes involved in space launcher cryogenic propellant engines like the Vulcain engine of Ariane 5 or the SSME of the space shuttle....
 
3.A cryogenic combustion research test bench - Operation with Oxygen / Hydrogen - ONERA / DEFA-EN
 Mascotte, a Test Bench for Cryogenic Propellant Combustion Studies... The present version of Mascotte can reach 80 bar with adapted combustor and nozzle.... A vast experimental program has been run since the first firing test of Mascotte on January 26, 1994, generating a large database for validating models and computation codes....
 
4.A Cryogenic Combustion Research Test Bench, LOX / Methane Configuration - ONERA / DEFA-EN
 Mascotte, a Test Bench for Cryogenic Propellant Combustion Studies...
 
5.Mascotte, perspectives and references - ONERA / DEFA-EN
 Mascotte, perspectives and references - ONERA / DEFA-EN... Mascotte, a Test Bench for Cryogenic Propellant Combustion Studies... In oxygen / hydrogen operation, the Mascotte cryotechnic combustion test bench provides pressures and flow mass rates comparable to those of a Vulcain injection element....
 
6.Mascotte Test Bed - ONERA's Science Pictures
 Mascotte Test Bed - ONERA's Science PicturesWho are we ?Science Pictures... Mascotte Test Bed copyright © ONERA 1996-2006. 2000 Hz pulsed laser sheet visualization of liquid oxygen on a Mascotte test bed. (). Pictures.
 
7.fluxen.doc
 Fluxmeters were originally worked out to meet the experimental needs of Onera's research teams using combustion chambers (Prepha program and Mascotte chamber) and to validate numerical simulation results....
 
8.No title
 This sensitivity is close to stable between 300 and 860 °C and corresponds to a piezoelectric charge constant (d33) of the Pt / AlN / Pt transducers of about 2.2 pC.N-1. The sensors were then integrated in the Mascotte cryogenic stand where their thermomechanical strength was tested.... Fig. 1 - Unsteady pressure sensors (on Mascotte stand combustion chamber)...
 
9.Launchers (LANC3)
 Test of a miniaturised combustion chamber on the MASCOTTE facility... To increase their reliability, comprehension tests at reduced scale are conducted on an experimental setup called MASCOTTE, during which elementary phenomena (atomisation, vaporisation, combustion, etc.) are investigated by laser instrumentation near the injectors....
 
10.Launchers (LANC3)
 Test of a miniaturised combustion chamber on the MASCOTTE facility...
 

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