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Porous Plug Phase Separator and Superfluid Film Flow Suppression System for the Soft X-Ray Spectrometer Onboard HitomiWhen 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.
Document ID
20190027246
Acquisition Source
Goddard Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Ezoe, Yuichiro
(Tokyo Metropolitan University Hachiouji, Japan)
DiPirro, Michael
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Fujimoto, Ryuichi
(Kanazawa University Kanazawa, Japan)
Ishikawa, Kumi
(Japan Aerospace Exploration Agency (JAXA) Sagamihara, Kanagawa, Japan)
Ishisaki, Yoshitaka
(Tokyo Metropolitan University Hachiouji, Japan)
Kanao, Kenichi
(Sumitomo Heavy Industries Ltd. Ehime, Japan)
Kimball, Mark
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mitsuda, Kazuhisa
(Japan Aerospace Exploration Agency (JAXA) Sagamihara, Kanagawa, Japan)
Mitsuishi, Ikuyuki
(Nagoya University Nagoya, Japan)
Murakami, Masahide
(Tsukuba Univ. Ibaraki, Japan)
Noda, Hirofumi
(Tohoku University Sendai, Japan)
Ohashi, Takaya
(Tokyo Metropolitan University Hachiouji, Japan)
Okamoto, Atsushi
(Japan Aerospace Exploration Agency (JAXA) Tsukuba, Ibaraki, Japan)
Satoh, Yohichi
(Japan Aerospace Exploration Agency (JAXA) Tsukuba, Ibaraki, Japan)
Sato, Kosuke
(Science Univ. of Tokyo Japan)
Shirron, Peter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Tsunematsu, Shoji
(Sumitomo Heavy Industries Ltd. Ehime, Japan)
Yamaguchi, Hiroya
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Yoshida, Seiji
(Japan Aerospace Exploration Agency (JAXA) Sagamihara, Kanagawa, Japan)
Date Acquired
July 12, 2019
Publication Date
October 27, 2017
Publication Information
Publication: Journal of Astronomy and Teelescopes in Space
Publisher: SPIE
Volume: 4
Issue: 1
Subject Category
Instrumentation And Photography
Report/Patent Number
GSFC-E-DAA-TN68369
Report Number: GSFC-E-DAA-TN68369
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Porous
Plug
Liquid Helium
Cryogenics
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