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Use of Mixed-Mode Propulsion for Reusable Single-Stage-to-Orbit Rocket Launchers.

Krülle, G. and Manksi, D. (1993) Use of Mixed-Mode Propulsion for Reusable Single-Stage-to-Orbit Rocket Launchers. Russian-Ukrainian-German Symposium on Space Transportation and Propulsion; May 26 - 28, 1993; München-Ottobrunn, DASA.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/24783/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1993,
Title:Use of Mixed-Mode Propulsion for Reusable Single-Stage-to-Orbit Rocket Launchers.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Krülle, G.UNSPECIFIEDUNSPECIFIED
Manksi, D.UNSPECIFIEDUNSPECIFIED
Date:1993
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Raketenantriebe, Mixed-Mode-Propulsion, SSTO`s
Event Title:Russian-Ukrainian-German Symposium on Space Transportation and Propulsion; May 26 - 28, 1993; München-Ottobrunn, DASA
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):UNSPECIFIED
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Institut für Chemische Antriebe und Verfahrenstechnik
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:34

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