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Dominant Suborbital Space Tourism Architectures

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sword-2019-10-24T18:00:30.original.xml (130 B)
Original SWORD entry document
Author(s)
Guerster, Markus
•
Crawley, Edward F
Date Issued
September 2019
Journal
Journal of Spacecraft and Rockets
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Citation
Guerster, Markus and Edward F. Crawley. "Dominant Suborbital Space Tourism Architectures." Journal of Spacecraft and Rockets 56, 5 (September 2019): dx.doi.org/10.2514/1.a34385
Version
Author's final manuscript
Abstract
In the early stages of maturity of a system built for a specific function, it is common for the solutions to lie in a broad architectural space, in which numerous concepts are being developed, built, and tested. As the product matures, certain concepts become more dominant. This pattern can currently be observed in the suborbital tourism industry, in which the obvious question is what system architecture will provide the best combination of cost and safety and in the long run become the dominant architecture. This paper addresses this question by defining a broad architectural space of thousands of possibilities and exploring it comprehensively. We identified 33 feasible architectures, 26 of which had not been proposed earlier. A genetic algorithm optimizes each architecture with respect to the launch mass (a proxy for cost) and operational safety. The launch mass has been calculated in a design analysis framework consisting of four modules: weight/size, propulsion, aerodynamics, and trajectory. A validation of this framework shows relative differences below 7%. A quantitative safety analysis is developed and validated with a survey of 11 leading experts. We identify six dominant architectures. These form a set from which optimal variants are likely to come.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
Creative Commons Attribution-Noncommercial-Share Alike
http://creativecommons.org/licenses/by-nc-sa/4.0/
Persistent DSpace Link
https://hdl.handle.net/1721.1/126666
DOI of Published Version
https://doi.org/10.2514/1.a34385
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