The propellant storage compartments (propellant tanks) are one of the parts that have undergone noted evolution in the design nature (mainly the shape and the structural properties) as well as the development process. To achieve high system performance for a given propulsion system, inert mass reduction as well as efficient volume utilization can be considered as the main attributes to concern the designer. Additive Manufacturing (AM) techniques on the other hand have played a major role in the recent years in altering the propulsion system design process to achieve higher overall propulsion performance due to the technical advantages of AM in reducing mass, enhancing heat transfer through enabling complex geometries and using high performance alloys. With new chances of increasing propulsion performance come new challenges on using AM propellant tanks, and chemical compatibility with green propellants is one. This paper tends to highlight main chemical properties of HNP225, AF-M315E, and LMP-103S green EIL monopropellants and material compatibility data with main materials used in some AM processes.

CubeSat Green Propellants AM Tanks: Efficient Designs, Propellant Management, and Chemical Compatibility / Nosseir, Ahmed E. S.; Pasini, Angelo; Igarashi, Shinji; Matsuura, Yoshiki; Cervone, Angelo. - SP2022_221(2022). (Intervento presentato al convegno International Conference on Space Propulsion tenutosi a Estoril, Portugal nel 09-13 May 2022).

CubeSat Green Propellants AM Tanks: Efficient Designs, Propellant Management, and Chemical Compatibility

Ahmed E. S. Nosseir
Primo
;
2022-01-01

Abstract

The propellant storage compartments (propellant tanks) are one of the parts that have undergone noted evolution in the design nature (mainly the shape and the structural properties) as well as the development process. To achieve high system performance for a given propulsion system, inert mass reduction as well as efficient volume utilization can be considered as the main attributes to concern the designer. Additive Manufacturing (AM) techniques on the other hand have played a major role in the recent years in altering the propulsion system design process to achieve higher overall propulsion performance due to the technical advantages of AM in reducing mass, enhancing heat transfer through enabling complex geometries and using high performance alloys. With new chances of increasing propulsion performance come new challenges on using AM propellant tanks, and chemical compatibility with green propellants is one. This paper tends to highlight main chemical properties of HNP225, AF-M315E, and LMP-103S green EIL monopropellants and material compatibility data with main materials used in some AM processes.
2022
Proceedings of the 8th Edition of the International Conference on Space Propulsion
Paris, France
Association Aéronautique et Astronautique de France (3AF)
Nosseir, Ahmed E. S.; Pasini, Angelo; Igarashi, Shinji; Matsuura, Yoshiki; Cervone, Angelo
CubeSat Green Propellants AM Tanks: Efficient Designs, Propellant Management, and Chemical Compatibility / Nosseir, Ahmed E. S.; Pasini, Angelo; Igarashi, Shinji; Matsuura, Yoshiki; Cervone, Angelo. - SP2022_221(2022). (Intervento presentato al convegno International Conference on Space Propulsion tenutosi a Estoril, Portugal nel 09-13 May 2022).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11572/394891
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