Flight performance of gravity probe B cryogenic system

被引:0
|
作者
Murray, D. O. [1 ]
Taber, M. A. [1 ]
Burns, K. M. [2 ]
机构
[1] Stanford Univ, Stanford, CA 94305 USA
[2] Lockheed Martin Adv Technol Ctr, Palo Alto, CA 94304 USA
来源
ADVANCES IN CRYOGENIC ENGINEERING, VOLS 51A AND B | 2006年 / 823卷
关键词
cryogenic; superfluid helium; space;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Gravity Probe B (GP-B) is a cryogenic and space-based test of Einstein's General Theory of Relativity by means of precision gyroscopes, The GP-B spacecraft was launched into a polar orbit from Vandenberg AFB on April 20, 2004. The launch and operation of GP-B represented the culmination of forty years of planning, technology development, hardware fabrication, and testing. The superfluid liquid helium became depleted on September 29, 2005, giving a lifetime of 17.3 months compared to the requirement of 16.5 months and a thermal model prediction of 16.6 months. The flight dewar contained 2320 liters of similar to 1.8 K superfluid helium at launch and housed the science instrument consisting of four precision gyroscopes and a telescope. A porous plug phase separator effected the venting of the helium boiloff gas. This venting helium was used to operate 16 thrusters, which are the actuators that effect precision pointing on a fixed star and adjust the orbit to be drag free or close to true zero-g.
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页码:1303 / +
页数:2
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