Loop Heat Pipe Technology With Flexible Lines Design And Development. DESTINY⁺ LHP Development Case Study

Loop Heat Pipes (LHP) are one of the most extended components used for thermal control subsystems in space technology, among other passive solutions (e.g., Heat Pipes, thermal straps) or active solutions (e.g., Mechanically Pumped Fluid Loop). One of the drivers in the design of an LHP is the transport lines definition and dimensioning. Transport lines are flexible or rigid elements that join the different components of the loop. Flexibility in the transport lines might be required for several purposes, such as system integration, deployable systems or mechanical decoupling of fixed interfaces and movable parts. The introduction of flexible lines can be addressed by metallic flexible hose designs or by rigid pipes in a certain configuration to allow flexibility. This paper presents the evolution of the development strategy for the LHPs for Destiny+ Thermal Control System due to the challenges encountered when introducing flexible hoses in the design at performance and validation level. A trade-off related to the advantages and limitations of the different potential solutions is reviewed, focusing on the mechanical and thermal implications of the design parameters for the flexible line sections. Furthermore, the development approach under severe fatigue conditions for a design considering rigid lines in flexible configuration is presented, including the validation at mechanical level and the results of the thermal test campaign.

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Publication Details

Published
2025-07-13
DOI
https://doi.org/10.32865/2346/102808
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
0.00

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article

Loop Heat Pipe Technology With Flexible Lines Design And Development. DESTINY⁺ LHP Development Case Study

R. Marino, Kenichiro Sawada, Takeshi Takashima, Yuki Akizuki et al.
Spacecraft Design and Technology
article

Loop Heat Pipe Technology With Flexible Lines Design And Development. DESTINY⁺ LHP Development Case Study

R. Marino, Kenichiro Sawada, Takeshi Takashima, Yuki Akizuki, Pedro Arturo Martínez Hernández, Sergio de Vera
article en

Abstract

Loop Heat Pipes (LHP) are one of the most extended components used for thermal control subsystems in space technology, among other passive solutions (e.g., Heat Pipes, thermal straps) or active solutions (e.g., Mechanically Pumped Fluid Loop). One of the drivers in the design of an LHP is the transport lines definition and dimensioning. Transport lines are flexible or rigid elements that join the different components of the loop. Flexibility in the transport lines might be required for several purposes, such as system integration, deployable systems or mechanical decoupling of fixed interfaces and movable parts. The introduction of flexible lines can be addressed by metallic flexible hose designs or by rigid pipes in a certain configuration to allow flexibility. This paper presents the evolution of the development strategy for the LHPs for Destiny+ Thermal Control System due to the challenges encountered when introducing flexible hoses in the design at performance and validation level. A trade-off related to the advantages and limitations of the different potential solutions is reviewed, focusing on the mechanical and thermal implications of the design parameters for the flexible line sections. Furthermore, the development approach under severe fatigue conditions for a design considering rigid lines in flexible configuration is presented, including the validation at mechanical level and the results of the thermal test campaign.

Japan Aerospace Exploration Agency
Openalex Percentile: Top 50%
Spacecraft Design and Technology
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