Stark, Ralf and Génin, Ch. (2012) Optimisation of a Rocket Nozzle Side Load Reduction Device. In: Proceedings. 48th AIAA Joint Propulsion Conference, 2012-07-30 - 2012-08-01, Atlanta, GA, USA. doi: 10.2514/6.2012-3970.
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Abstract
The flow during transient startup and shutdown in all rocket engines operated on sea level under ambient conditions will separate inside the supersonic part of the nozzle. A separated nozzle flow is circumferential asymmetric distributed and induces high side loads. DLR carried out a cold flow subscale test campaign to study devices that can reduce the side loads during transient operation of a thrust optimised parabolic nozzle. A detailed parametrical study was performed and experimental data demonstrate the potential of the device to reduce the side loads.
Item URL in elib: | https://elib.dlr.de/77680/ | ||||||||||||
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Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||||
Title: | Optimisation of a Rocket Nozzle Side Load Reduction Device | ||||||||||||
Authors: |
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Date: | 2012 | ||||||||||||
Journal or Publication Title: | Proceedings | ||||||||||||
Refereed publication: | Yes | ||||||||||||
Open Access: | No | ||||||||||||
Gold Open Access: | No | ||||||||||||
In SCOPUS: | No | ||||||||||||
In ISI Web of Science: | No | ||||||||||||
DOI: | 10.2514/6.2012-3970 | ||||||||||||
Status: | Published | ||||||||||||
Keywords: | nozzle flow, side loads, flow separation | ||||||||||||
Event Title: | 48th AIAA Joint Propulsion Conference | ||||||||||||
Event Location: | Atlanta, GA, USA | ||||||||||||
Event Type: | international Conference | ||||||||||||
Event Start Date: | 30 July 2012 | ||||||||||||
Event End Date: | 1 August 2012 | ||||||||||||
Organizer: | AIAA | ||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||
HGF - Program: | Space | ||||||||||||
HGF - Program Themes: | Space Transportation | ||||||||||||
DLR - Research area: | Raumfahrt | ||||||||||||
DLR - Program: | R RP - Space Transportation | ||||||||||||
DLR - Research theme (Project): | R - Antriebsystemtechnik - Schubkammertechnologie (old) | ||||||||||||
Location: | Lampoldshausen | ||||||||||||
Institutes and Institutions: | Institute of Space Propulsion > Rocket Propulsion | ||||||||||||
Deposited By: | Nürnberger-Genin, Chloe | ||||||||||||
Deposited On: | 08 Oct 2012 20:26 | ||||||||||||
Last Modified: | 24 Apr 2024 19:44 |
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