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Untersuchungen der Nutzlastkapazität der Trägerrakete "Sojus/ST" für den Startplatz Kourou
Klevanski, J. and Sippel, M. (2002) Untersuchungen der Nutzlastkapazität der Trägerrakete "Sojus/ST" für den Startplatz Kourou. Project Report, DLR-Interner Bericht. 647-2002/06, 27 S.
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Abstract
This study regards the payload-capacity of the Russian liquid-fuel Launcher "Sojuz/ST" from the launchpad Kourou as a medium-class launcher. Based on published technical data, the "Sojuz/ST" is simulated in geometry and mass estimation, propulsion, and trajectory analysis, including stage re-entry after engine cut-off. Several variations of the upper stages are considered: Variations of Block I with and without the "Fregat"-stage or as an alternative a hypothetical cryogenic upper stage. Reference-mission is an elliptical GTO and also an ascent to circular SSO. The achieved results allow to evaluate the possibilities to use this vehicle as a potential replacement for the Ariane 4.
| Document Type: | Monograph (Project Report, DLR-Interner Bericht) | ||||||
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| Additional Information: | LIDO-Berichtsjahr=2002, | ||||||
| Title: | Untersuchungen der Nutzlastkapazität der Trägerrakete "Sojus/ST" für den Startplatz Kourou | ||||||
| Authors: |
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| Date: | 2002 | ||||||
| Number of Pages: | 27 | ||||||
| Status: | Published | ||||||
| Keywords: | Soyuz, Kourou, propulsion data, performance analysis | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Space | ||||||
| HGF - Program Themes: | W RP - Raumtransport | ||||||
| DLR - Research area: | Space | ||||||
| DLR - Program: | W RP - Raumtransport | ||||||
| DLR - Research theme (Project): | E -- no assignement | ||||||
| Location: | Lampoldshausen | ||||||
| Institutes and Institutions: | Institute of Space Propulsion | ||||||
| Deposited By: | Monika Lohmiller | ||||||
| Deposited On: | 16 Sep 2005 | ||||||
| Last Modified: | 06 Jan 2010 13:58 |
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