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Electron Beam Fluorescence (EBF) free stream probe (FSP) test campaign preparation

Elias, Paul Quentin and Packan, Denis and Fertig, M. and Mohamed, Ajmal (2017) Electron Beam Fluorescence (EBF) free stream probe (FSP) test campaign preparation. Project Report. ONERA.

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Abstract

The Electron Beam Fluorescence (EBF) technique has been shown to provide inflow measurement of the gas number density and gas temperature, in conditions typical of reentry flows. While the earlier implementation where primarily designed for wind-tunnel measurements, some recent development have shown that the technique could be miniaturized in a Free Stream Probe, whose dimension are compatible with in-flight experiments. The main objective of this task is to upgrade, miniaturize and calibrate an existing prototype to perform measurements in the VKI Plasmatron wind tunnel facility with a flight compatible design. This document describes the current status of the design of the miniaturized EBF FSP and the test campaign preparation. It will be complemented by forthcoming revision of this note further describing the finalized design of the FSP.

Item URL in elib:https://elib.dlr.de/116876/
Document Type:Monograph (Project Report)
Title:Electron Beam Fluorescence (EBF) free stream probe (FSP) test campaign preparation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Elias, Paul QuentinONERAUNSPECIFIED
Packan, DenisONERAUNSPECIFIED
Fertig, M.markus.fertig (at) dlr.deUNSPECIFIED
Mohamed, AjmalONERAUNSPECIFIED
Date:15 November 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:42
Publisher:ONERA
Status:Published
Keywords:Elektronenstrahl Fluoreszenz CFD Navier-Stokes
Institution:ONERA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Fertig, Dr. Markus
Deposited On:13 Dec 2017 10:54
Last Modified:13 Dec 2017 10:54

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