Mathematical modelling of bipropellant combined propulsion subsystems

Dixon, Chris; Marshall, J.

doi:10.2514/6.1990-2303

26th Joint Propulsion Conference 1990

DOI: 10.2514/6.1990-2303

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Mathematical modelling of bipropellant combined propulsion subsystems

Chris Dixon¹,

J. Marshall²

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2009

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A Propellant Loading Analysis Program of Bipropellant Propulsion System

Chae

Han²,

Yu³

2009

Journal of the Korean Society for Aeronautical & Space Scie

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It proposes an simple and intuitive method that calculates the equilibrium pressures of a propellant tank by appling the mass conservation principle on the helium in the liquid propellant and in an ullage volume of the propellant tank. A propellant loading analysis program is developed and validated against the existing reference data. And it has applied to the present developing program, COMS Chemical Propulsion Subsystem and the results are compared, it may use to develop a technology of the next geostationary complex satellite's propulsion system.

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A Propellant Loading Analysis Program of Bipropellant Propulsion System

Chae

Han²,

Yu³

2009

Journal of the Korean Society for Aeronautical & Space Scie

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Mathematical modelling of bipropellant combined propulsion subsystems

Cited by 1 publication

References 2 publications

A Propellant Loading Analysis Program of Bipropellant Propulsion System

A Propellant Loading Analysis Program of Bipropellant Propulsion System

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