Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Louis Souverein"'
Publikováno v:
Turbo Expo 2021: Virtual, Online, Virtual Conference and Exhibition
Turbo Expo 2021
Turbo Expo 2021
Axial turbine stages for gas generator cycle type rocket engines typically employ highly-loaded supersonic stator vanes. Consequently, the flow pattern downstream of the vanes is characterized by shock waves which induce high-frequency excitation on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f9d2e116479736c06da604df3621df0f
https://doi.org/10.1115/gt2021-59580
https://doi.org/10.1115/gt2021-59580
Publikováno v:
Volume 2E: Turbomachinery.
Turbopumps constitute an essential component of high thrust liquid rocket engines. They are characterized by a compact design, providing a large shaft power at high rotation rates. This is necessary to deliver the propellants at high pressure into th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70cef8d6b4ff309b61323a52910b0589
https://doi.org/10.1115/gt2020-15428
https://doi.org/10.1115/gt2020-15428
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5bc32b63b5d6db56f6dfacc7f3f525d
https://doi.org/10.2514/6.2013-4163
https://doi.org/10.2514/6.2013-4163
Autor:
Katharina Quering, Georg Obermaier, Richard Arnold, Louis Souverein, Andreas Goetz, Jean-Noel Caruana
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
FLPP Storable is a technology demonstration project with the main objective of readying the technologies for a development application for a pressure fed, medium thrust engine with a thrust level of 5 kN and a chamber pressure of 15 bar. The FLPP Sto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e97e164ea1969703d968a62670357f08
https://doi.org/10.2514/6.2012-3932
https://doi.org/10.2514/6.2012-3932