Martin Sippel, Sven Stappert, Leonid Bussler, Sholto Forbes-Spyratos Space Launcher Systems Analysis (SART)

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_1580839

The SpaceLiner ultra-high-speed rocket-propelled passenger transport is in Phase A conceptual design after successful completion of the MRR. The ongoing concept evolution is addressing system aspects of the next configuration release 8. The space transportation role of the SpaceLiner concept as a TSTO-launcher is further refined and suitable precursor steps are investigated. The critical separation of the passenger cabin and rescue capsule and its subsystems are one topic of the paper. The separation process is critically investigated taking into account multi-body dynamics and advanced CFD-simulations. Potential intercontinental flight routes, considering range-safety and sonic boom constraints as well as good reachability from major business centers, are evaluated Extensions to this trajectory model are implemented to investigate the attitude dynamics and related controllability issues of the asymmetric launcher configuration.

Download the Full Paper from the DLR website >

Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.