Abstract

When using superfluid helium in low gravity environments, porous plug phase separators are commonly used to vent boiloff gas while confining the bulk liquid to the tank. Invariably, there is a flow of superfluid film from the perimeter of the porous plug down the vent line. For the Soft X-ray Spectrometer onboard ASTRO-H (Hitomi), its approximately 30-liter helium supply has a lifetime requirement of more than 3 years. A nominal vent rate is estimated as ~ 30 ug/s, equivalent to ~ 0.7 mW heat load. It is therefore critical to suppress any film flow whose evaporation would not provide direct cooling of the remaining liquid helium. That is, the porous plug vent system must be designed to both minimize film flow and to ensure maximum extraction of latent heat from the film. The design goal for Hitomi is to reduce the film flow losses to <2 ug/s, corresponding to a loss of cooling capacity of <40 uW. The design adopts the same general design as implemented for Astro-E and E2, using a vent system composed of a porous plug, combined with an orifice, a heat exchanger, and knife-edge devices. In this paper, design, on-ground testing results and in-orbit performance are described.

Highlights

  • ASTRO-H (Hitomi)[1] is the sixth Japanese x-ray astronomy satellite

  • We describe design and performance of the porous plug and superfluid film flow suppression system for the soft x-ray spectrometer (SXS)

  • One possible explanation for this possible excess vent rate is that the ΔT across the porous plug was smaller than anticipated, due for example to a higher than expected vent line impedance which may lead to an increase of the film flow, there remains uncertainties in the estimations due to the limited lifetime of the spacecraft and the resolution of the thermometers of the porous plug

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Summary

Introduction

ASTRO-H (Hitomi)[1] is the sixth Japanese x-ray astronomy satellite. It was launched on February 17, 2016, and was decommissioned due to loss of the attitude control on March 26, 2016. The soft x-ray spectrometer (SXS)[2] onboard Hitomi is an x-ray microcalorimeter operated at 50 mK, providing a nondispersive energy resolution of

Overview
Porous Plug
Orifice
Heat Exchanger
Knife-Edge Devices
Ground Measurements
Mass Flow Rate
Film Flow Rate
Temperature Profiles
Flow Rate Test Before Launch
Volume of the Superfluid Helium
Findings
Conclusion
Full Text
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