Compact air separation system for space launcher

Compact air separation system for space launcher

A compact air separator demonstrator based on centrifugally enhanced distillation has been studied. The full size device is meant to be used on board of a Two Stage To Orbit vehicle launcher. The air separation system must be able to extract oxygen in highly concentrated liquid form (LEA, Liquid Enr...

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Bibliographic Details
Main Author: Bizzarri, Didier
Other Authors: Hendrick, Patrick
Format: Doctoral Thesis
Language:fr
Published: Universite Libre de Bruxelles 2008
Subjects:
Sciences de l'ingénieur
Mécanique
Launch vehicles (Astronautics)
Mass transfer
Two-phase flow
Oxygen > Separation
Lanceurs (Astronautique)
Transfert de masse
Ecoulement diphasique
Oxygène > Séparation
mass transfer/tranfert de matière
demonstrator/démonstrateur
heat transfer/transfert de chaleur
prototype
two phase flow/écoulement biphasique
HTU
HETP
pressure drop/pertes de charge
flooding/noyage
centrifugal/centrifuge
RDS
two stage to orbit/lanceur biétage
TSTO
air launch/lanceur aéroporté
in-flight oxygen collection/collecte d'oxygène en
compact distillation device/ appareil compact de d
high specific surface/surface spécifique élevée
porous material/matériaux poreux
distillation
experimental study/étude expérimentale
system study/étude système
liquid air/air liquide
liquid oxygen/oxygène liquide
Online Access:http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/210488

Internet

http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/210488

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