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Proceedings of SPIE | 2010

Design of a 3-stage ADR for the soft x-ray spectrometer instrument on the ASTRO-H mission

Peter J. Shirron; Mark O. Kimball; Donald Wegel; Edgar Canavan; Michael DiPirro

The Japanese Astro-H mission will include the Soft X-ray Spectrometer (SXS) instrument, whose 36-pixel detector array of ultra-sensitive x-ray microcalorimeters requires cooling to 50 mK. This will be accomplished using a 3-stage adiabatic demagnetization refrigerator (ADR). The design is dictated by the need to operate with full redundancy with both a superfluid helium dewar at 1.3 K or below, and with a 4.5 K Joule-Thomson (JT) cooler. The ADR is configured as a 2-stage unit that is located in a well in the helium tank, and a third stage that is mounted to the top of the helium tank. The third stage is directly connected through two heat switches to the JT cooler and the helium tank, and manages heat flow between the two. When liquid helium is present, the 2-stage ADR operates in a single-shot manner using the superfluid helium as a heat sink. The third stage may be used independently to reduce the time-average heat load on the liquid to extend its lifetime. When the liquid is depleted, the 2nd and 3rd stages operate as a continuous ADR to maintain the helium tank at as low a temperature as possible - expected to be 1.2 K - and the 1st stage cools from that temperature as a single-stage, single-shot ADR. The ADRs design and operating modes are discussed, along with test results of the prototype 3-stage ADR.


TRANSACTIONS OF THE CRYOGENIC ENGINEERING CONFERENCE—CEC: Advances in Cryogenic Engineering | 2010

OPTIMIZATION OF A TWO‐STAGE ADR FOR THE SOFT X‐RAY SPECTROMETER (SXS) INSTRUMENT ON THE ASTRO‐H MISSION

Peter J. Shirron; Mark O. Kimball; Donald Wegel; Franklin Miller

NASA/Goddard Space Flight Center has begun developing the Soft X‐ray Spectrometer (SXS) instrument that will be flown on the Japanese Astro‐H mission. The SXS’s 36‐pixel detector array will be cooled to 50 mK using a two‐stage adiabatic demagnetization refrigerator (ADR). A complicating factor for its design is that the ADR will be integrated into a superfluid helium dewar at 1.3 K that will be coupled to a 1.8 K Joule‐Thomson (JT) stage through a heat switch. When liquid helium is present, the coupling will be weak, and the JT stage will act primarily as a shield to reduce parasitic heat loads. When the liquid is depleted, the heat switch will couple more strongly so that the ADR can continue to operate using the JT stage as its heat sink. A two‐stage ADR is the most mass efficient option and it has the operational flexibility to work well with a stored cryogen and a cryocooler. The stages are operated independently, and this opens up a very large parameter space for optimizing the design. This paper discusses the optimization process and most relevant trades considered in the design of the SXS ADR, and its expected performance.


Cryogenics | 2010

ADR design for the Soft X-ray Spectrometer instrument on the Astro-H mission

Peter J. Shirron; Mark O. Kimball; Donald Wegel; Franklin Miller


Cryogenics | 2012

Design and predicted performance of the 3-stage ADR for the Soft-X-ray Spectrometer instrument on Astro-H

Peter J. Shirron; Mark O. Kimball; Bryan L. James; Donald Wegel; Raul M. Martinez; Richard L. Faulkner; Larry Neubauer; Marcelino Sansebastian


Cryogenics | 2012

Mechanical design of a 3-stage ADR for the Astro-H mission

Bryan L. James; Raul M. Martinez; Peter J. Shirron; J. G. Tuttle; John Francis; Marcelino San Sebastian; Donald Wegel; Nicholas M. Galassi; Daniel S. McGuinness; David Puckett; Yury Flom


Cryogenics | 2014

Techniques for on-orbit cryogenic servicing

C.H. DeLee; P. Barfknecht; Susan Breon; Rob Boyle; M. J. DiPirro; John Francis; J. Huynh; Xiaoyi Li; J. McGuire; Shuvo Mustafi; J. G. Tuttle; Donald Wegel


Archive | 2011

Design and Development of the Astro-H 3-Stage ADR

Peter J. Shirron; Mark O. Kimball; Bryan L. James; Donald Wegel; Michael DiPirro; Raul M. Martinez; Dick Faulkner; Marcelino Sansebastian; Evan S. Kunes


Archive | 2011

Low-Thermal Conductivity Suspensions Used in the Isolation of the Salt Pills Aboard the Astro-H Adiabatic Demagnetization Refrigerator

Mark O. Kimball; Peter J. Shirron; Donald Wegel; Bryan L. James; Nicholas M. Galassi; Richard L. Faulkner; Marcelino San Sebastian


ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering#N#Conference - CEC, Vol. 53 | 2008

DEVELOPMENT OF A CRYOGEN-FREE CONTINUOUS ADR SYSTEM FOR MILLI-GRAVITY EXPERIMENTS

K. Takahashi; K. Kamiya; Hideki Nakagome; Takenori Numazawa; Peter J. Shirron; Donald Wegel


低温工学・超電導学会講演概要集 = Meetings of Cryogenics and Superconductivity | 2007

宇宙用磁気冷凍機の開発(4) : 冷凍試験結果報告

健太 高橋; 宏治 神谷; 健則 沼澤; Donald Wegel; Peter J. Shirron

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Peter J. Shirron

Goddard Space Flight Center

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Mark O. Kimball

Goddard Space Flight Center

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Bryan L. James

Goddard Space Flight Center

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Raul M. Martinez

Goddard Space Flight Center

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Franklin Miller

University of Wisconsin-Madison

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J. G. Tuttle

Goddard Space Flight Center

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John Francis

Goddard Space Flight Center

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Michael DiPirro

Goddard Space Flight Center

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