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Aerospace
Technical Paper

Modeling of a Real LHP and Integration in a System Level Analysis

2006-01-2228

07/17/2006

Event
International Conference On Environmental Systems
Authors
G. Xin Shandong University
L. Cheng Shandong University
W. Du Shandong University
T. Luan Shandong University
Y. Qu Shandong University
S. Zinna Bergamo University
M. Marengo Bergamo University
M. Molina
J. Burger
Abstract
Content
An LHP-based thermal control system for cryocoolers on the Alpha Magnetic Spectrometer (AMS-02) has been designed and analyzed by means of the system level model based on Sinda/Fluint. It is integrated with the International Space Station (ISS) model by means of a time-varying sink temperature definition, and the performance of LHP-based thermal control is investigated. A parametric analysis is carried out also to understand the influence of critical parameters on the operation of LHP.
Meta Tags
Topics
Spacecraft
Control systems
Simulation and modeling
Terminology
Magnetic materials
Affiliated or Co-Author
Shandong University
Bergamo University
Details
DOI
https://doi.org/10.4271/2006-01-2228
Pages
8
Citation
Xin, G., Cheng, L., Du, W., Luan, T. et al., "Modeling of a Real LHP and Integration in a System Level Analysis," SAE Technical Paper 2006-01-2228, 2006, https://doi.org/10.4271/2006-01-2228.
Additional Details
Publisher
SAE International
Published
Jul 17, 2006
Product Code
2006-01-2228
Content Type
Technical Paper
Language
English