Doekhie, Sandra (2012) Continuous Detonation Wave Engine: Literature Study. DLR-Interner Bericht. SART-TN021-2012. Diploma. DLR. 74 S. (Unpublished)
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Abstract
The Continuous Detonation Wave Engine (CDWE) is a new concept of rocket engine based on rotating detonation waves. The detonation process is characterized by a faster burn rate and a higher energy release rate as compared to deflagration, which produces an extreme pressure and temperature rise. Due to the rapidity of the process, it is more similar to a constant volume process than a constant pressure process typical of conventional combustion. Therefore, engines based on detonations can have a higher thermodynamic efficiency and specific impulse compared to conventional engines.
Item URL in elib: | https://elib.dlr.de/82526/ | ||||||||
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Document Type: | Monograph (DLR-Interner Bericht, Diploma) | ||||||||
Title: | Continuous Detonation Wave Engine: Literature Study | ||||||||
Authors: |
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Date: | November 2012 | ||||||||
Refereed publication: | No | ||||||||
Open Access: | No | ||||||||
Gold Open Access: | No | ||||||||
In SCOPUS: | No | ||||||||
In ISI Web of Science: | No | ||||||||
Number of Pages: | 74 | ||||||||
Status: | Unpublished | ||||||||
Keywords: | CDWE, Continuous, Rotating, Detonation, Wave, Engine, Chapman Jouguet, ZND, PDE | ||||||||
Institution: | DLR | ||||||||
Department: | SART | ||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||
HGF - Program: | Space | ||||||||
HGF - Program Themes: | Space Transportation | ||||||||
DLR - Research area: | Raumfahrt | ||||||||
DLR - Program: | R RP - Space Transportation | ||||||||
DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old) | ||||||||
Location: | Bremen | ||||||||
Institutes and Institutions: | Institute of Space Systems > Space Launcher Systems Analysis | ||||||||
Deposited By: | Dumont, Etienne | ||||||||
Deposited On: | 04 Jun 2013 10:05 | ||||||||
Last Modified: | 04 Jun 2013 10:05 |
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