Published February 2018 | Version v1
Journal article

On-orbit demonstration of oscillating heat pipe with check valves for space application

  • 1. Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505 (Japan)
  • 2. Tohoku University, Sendai, Miyagi 980-8579 (Japan)

Description

Highlights: • The on-orbit experiment of the OHP with check valves was conducted. • The OHP operated successfully with no degradation for almost four years on orbit. • Vapor-liquid behavior on orbit was clarified experimentally and numerically. - Abstract: An Oscillating Heat Pipe (OHP) has high heat transport capability and enables effective heat transport even from narrow spaces, and thus is being targeted for application in the thermal management system of future spacecraft with larger heat dissipation. A Flat-plate Heat Pipe (FHP), which is an OHP with check valves sandwiched between thin aluminum alloy plates, has been developed. For applying FHPs to the thermal management system of spacecraft, the heat transfer characteristics of FHPs under microgravity conditions should first be examined. The on-orbit experiment on the FHP has been conducted since 2012 as one of the Small Demonstration Satellite-4 (SDS-4) missions. The FHP operated successfully on orbit with good heat transfer performance matching that on the ground, and with no degradation being observed for almost four years. Conversely, it was confirmed that the initial vapor-liquid distribution strongly affected the startup characteristics of FHPs, and that certain initial conditions caused startup difficulty. This paper describes the on-orbit experimental results and discusses the vapor-liquid behavior in FHPs based on those experimental results and numerical simulation.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.applthermaleng.2017.11.032

Additional details

Identifiers

DOI
10.1016/j.applthermaleng.2017.11.032;
PII
S1359431117340267;

Publishing Information

Journal Title
Applied Thermal Engineering
Journal Volume
130
Journal Page Range
p. 552-560
ISSN
1359-4311
CODEN
ATENFT

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
50071884
Subject category
S42: ENGINEERING;
Descriptors DEI
ALUMINIUM ALLOYS; COMPUTERIZED SIMULATION; ENERGY LOSSES; HEAT PIPES; HEAT TRANSFER; ORBITS; SPACE VEHICLES; THERMAL DIFFUSIVITY; VALVES
Descriptors DEC
ALLOYS; CONTROL EQUIPMENT; ENERGY TRANSFER; EQUIPMENT; FLOW REGULATORS; LOSSES; PHYSICAL PROPERTIES; SIMULATION; THERMODYNAMIC PROPERTIES; VEHICLES

Optional Information

Notes
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