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Abbrandrate von festen Brennstoffen bei Hybridraketentriebwerken

Koch, Patrick (2013) Abbrandrate von festen Brennstoffen bei Hybridraketentriebwerken. Other.

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Item URL in elib:https://elib.dlr.de/82035/
Document Type:Thesis (Other)
Additional Information:Studienarbeit
Title:Abbrandrate von festen Brennstoffen bei Hybridraketentriebwerken
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Koch, PatrickUNSPECIFIEDUNSPECIFIED
Date:27 March 2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:135
Status:Published
Keywords:AHRES, HRT, SPLab, CEA-Code
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Vorhaben AHRES (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Steinberg, Silke
Deposited On:24 Apr 2013 15:49
Last Modified:24 Apr 2013 15:49

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