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Development and Operational Conditions of VINCI Altitude Simulation Test Bench P4.1

Schäfer, Klaus and Zimmermann, Herbert and Pauly, Clement (2008) Development and Operational Conditions of VINCI Altitude Simulation Test Bench P4.1. In: 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008-07-21 - 2008-07-23, Hartford, CT (USA).

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Abstract

Since February 2005 the new high altitude simulation test facility P4.1 for the VINCI® upper stage engine is operational in Lampoldshausen, the European test centre for rocket propulsion. VINCI® is an expander cycle upper stage engine of 180 kN thrust developed by SNECMA Moteurs. The paper deals with the operational conditions of the altitude simulation especially the behavior of the super sonic center body diffusor. High nozzle expansion ratios, different test configurations and the r-ignition conditions drive the challenges of the high altitude simulation P4.1.

Item URL in elib:https://elib.dlr.de/58016/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Development and Operational Conditions of VINCI Altitude Simulation Test Bench P4.1
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schäfer, KlausUNSPECIFIEDUNSPECIFIED
Zimmermann, HerbertUNSPECIFIEDUNSPECIFIED
Pauly, ClementUNSPECIFIEDUNSPECIFIED
Date:2008
Journal or Publication Title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:high altitude simulation upper stage engine
Event Title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Event Location:Hartford, CT (USA)
Event Type:international Conference
Event Dates:2008-07-21 - 2008-07-23
Organizer:44th AIAA/ASME/SAE/ASEE
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Antriebsystemtechnik - Raketenantriebtests (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Kummer, Erika
Deposited On:06 Apr 2009
Last Modified:31 Jul 2019 19:24

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