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Influence of Rocket Design Parameters on Engine Nozzle Efficiencies.

Manski, D. and Hagemann, G. (1996) Influence of Rocket Design Parameters on Engine Nozzle Efficiencies. Journal of Propulsion and Power, Vol.12,No.1, pp. 41-47.

Full text not available from this repository.

Abstract

Lampoldshausen 970219.

Item URL in elib:https://elib.dlr.de/25013/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1996,
Title:Influence of Rocket Design Parameters on Engine Nozzle Efficiencies.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Manski, D.UNSPECIFIEDUNSPECIFIED
Hagemann, G.UNSPECIFIEDUNSPECIFIED
Date:1996
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol.12,No.1
Page Range:pp. 41-47
Status:Published
Keywords:Raketen, Triebwerke, Duesen, Wirkungsgrade, Verluste, Kinetik, Reibung
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):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:40

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