This paper shows a preliminary design of a cold gas engine, equipped with an aerospike nozzle, for space applications. This work is part of the MACARONIS project, which aims to develop, manufacture and qualify a ceramic aerospike nozzle for future space missions. Two designs are developed, one consisting of a single fluid line and one featuring redundant components. A genetic algorithm was created to optimize the two conï¬ gurations.
Preliminary design of a cold gas aerospike engine experiment
Tesser, Giorgio
2019/2020
Abstract
This paper shows a preliminary design of a cold gas engine, equipped with an aerospike nozzle, for space applications. This work is part of the MACARONIS project, which aims to develop, manufacture and qualify a ceramic aerospike nozzle for future space missions. Two designs are developed, one consisting of a single fluid line and one featuring redundant components. A genetic algorithm was created to optimize the two conï¬ gurations.File in questo prodotto:
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/28811