Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8057733 | Aerospace Science and Technology | 2018 | 8 Pages |
Abstract
Suborbital vehicles are innovative and unconventional aerospace concepts that are characterized by a high level of complexity and a lack of optimized baseline. The present focuses on the development of a flexible multi-objective modeling and simulation environment that provides the capabilities to rapidly evaluate the flying, economic, and safety performance of suborbital vehicles at a conceptual design level. One of the goals of this environment is to enable the exploration of large design spaces and facilitate the mapping between high-level requirements and the identified optimized concept. The environment is broken down into six modules: weight/size, aerodynamics, trajectory, propulsion, economics, and safety. By leveraging empirical models, physics-based approaches, and surrogate modeling techniques, it enables the rapid and parametric assessment and optimization of a multitude of design concepts. It is the first environment of this sort to support informed design space exploration of suborbital vehicles and allow for new trends to be identified and crucial observations to be made.
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Aerospace Engineering
Authors
Christopher P. Frank, Olivia J. Pinon-Fischer, Dimitri N. Mavris,