Spitzer space telescope thermal/cryogenic system flight performance

被引：0

作者：

Finley, Paul T. ^{[1
]}

Hopkins, Richard A. ^{[1
]}

Schweickart, Russell B. ^{[1
]}

机构：

[1] Ball Aerosp & Technol Corp, Boulder, CO 80301 USA

来源：

ICEC 20: PROCEEDINGS OF THE TWENTIETH INTERNATIONAL CRYOGENIC ENGINEERING CONFERENCE | 2005年

关键词：

D O I：

暂无

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

The Spitzer Space Telescope (formerly called SIRTF) was launched into an Earth-trailing, solar orbit on August 25, 2003. The Cryogenic Telescope Assembly is Spitzer's instrument payload. The design operational lifetime is 5 years, limited by the loss rate from the superfluid helium cryostat that cools the instruments to 1.3 K and the telescope to 5.5 K by vapor cooling. The thermal/cryogenic system flight performance to date is meeting expectations.

引用

页码：413 / 418

页数：6

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