elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Thermomechanical Optimization of the Cooling System for Rocket Combustion Chambers

Josien, N. (1998) Thermomechanical Optimization of the Cooling System for Rocket Combustion Chambers. DLR-Interner Bericht. 645-98/21. 78 S.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/25126/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1998,
Title:Thermomechanical Optimization of the Cooling System for Rocket Combustion Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Josien, N.UNSPECIFIEDUNSPECIFIED
Date:1998
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:78
Status:Published
Keywords:LH2/O2, rocket engine, optimization, sizing, adaptivity
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):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 05:42

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.