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Influence of Rocket Design Parameters on Engine Nozzle Efficiences.

Hagemann, G. and Manski, D. (1994) Influence of Rocket Design Parameters on Engine Nozzle Efficiences. In: 3th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27 - 29.

Full text not available from this repository.

Abstract

Using a modified version of JANNAFs Two-Dimensional Kinetic Program (TDK), parametric calculations of rocket nozzles were performed. Efficiencies of energy release in rocket engines are defined. The domain of nozzle losses is classified by two-dimensionality, frictionand kinetic. Their dependencies versus characteristic nozzle design parameters were investigated. In addition, the influence of shocks isthe nozzle and cooling effects of the efficiencies has been considered. The losses are determined using nozzle shapes of SSME andVulcan engines which are characteristic for future rocket launchers. The nozzle design parameters are parametrically derived versus thrust, chamber pressure, mixture ratio, nozzle area ratio, and nozzle geometry. All these parameters are systematically varied, and their effects on nozzle efficiencies are pesented. These efficiencieswill be used as a data base for further system analyses of future rocket launchers.

Item URL in elib:https://elib.dlr.de/24823/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994, pages=9,
Title:Influence of Rocket Design Parameters on Engine Nozzle Efficiences.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hagemann, G.UNSPECIFIEDUNSPECIFIED
Manski, D.UNSPECIFIEDUNSPECIFIED
Date:1994
Journal or Publication Title:3th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27 - 29
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA 94-2756
Status:Published
Keywords:Raketentriebwerke, Wirkungsgrade, Thermodynamik, Chemische Kinetik, Stroemung, Duesen
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):UNSPECIFIED
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Institut für Chemische Antriebe und Verfahrenstechnik
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:35

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