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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.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=1996,
Title:Influence of Rocket Design Parameters on Engine Nozzle Efficiencies.
Authors:
AuthorsInstitution or Email of Authors
Manski, D.UNSPECIFIED
Hagemann, G.UNSPECIFIED
Date:1996
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
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 assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:40

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