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Novel synthesis optimisation framework based on performance prediction model for a space propulsion system

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The optimisation framework significantly increases specific impulse by 6% and reduces mass by 15.8%.
Objective functions aimed at enhancing specific impulse and minimizing mass were defined early in the optimisation process.
The methodology involves defining the problem, employing the design of experiments tool, and optimizing metamodels.
This approach supports the development of more efficient space propulsion systems through advanced optimisation techniques.

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This research develops a synthesis optimisation framework, improving specific impulse and reducing mass in space propulsion systems.

Mughari et al. (2025) studied this question.

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