2015
DOI: 10.1088/0264-9381/32/22/224008
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The design and performance of the Gravity Probe B telescope

Abstract: The Gravity Probe B spacecraft was launched on 20 April 2004 to measure the geodetic and frame-dragging effects predicted by the theory of general relativity. A cryogenic optical telescope was used to establish the inertial reference frame for the measurements by tracking a reference or guide star. The motion of this star was independently checked by reference to background galaxies. With the mission now over, we describe the design, construction and evaluation of the optical and electrical performance of the … Show more

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Cited by 10 publications
(11 citation statements)
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“…The first class of systematic uncertainty is small effects not present in the model, such as unmodeled torques, telescope and gyroscope readout, and guide star proper motion. Papers 6 [23] and 8 [24] review the telescope and SQUID readout; paper 21 [35] reviews the uncertainty in guide star proper motion. 'Other nonrelativistic torques' in table 3 includes the mass unbalance and suspension effects discussed earlier and various parameters determined on the ground and onorbit.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The first class of systematic uncertainty is small effects not present in the model, such as unmodeled torques, telescope and gyroscope readout, and guide star proper motion. Papers 6 [23] and 8 [24] review the telescope and SQUID readout; paper 21 [35] reviews the uncertainty in guide star proper motion. 'Other nonrelativistic torques' in table 3 includes the mass unbalance and suspension effects discussed earlier and various parameters determined on the ground and onorbit.…”
Section: Resultsmentioning
confidence: 99%
“…The telescope (paper 8, [24]) was a folded Schmidt-Cassegrain fabricated from fused quartz, with a convex tertiary mirror centered in the primary, and a sophisticated beam splitter assembly on its front end corrector plate, seen in figure 7. The folded design eased the image divider layout and simplified the quartz block interface.…”
Section: The Telescope and Siamentioning
confidence: 99%
“…Conceptually, the configuration is simple: a rotor, housed within a spacecraft, is placed in a circular polar orbit about the Earth. Gyro drift is measured relative to distant inertial space by means of an on-board telescope [5] tracking a guide star that ideally is in the orbit plane.…”
Section: Introductionmentioning
confidence: 99%
“…(4) Locating the four gyros close to the roll axis to limit the magnitude centrifugal acceleration. (5) Operating one gyro in drag-free mode, described below, to reduce residual rotor acceleration and the associated support force.…”
Section: Introductionmentioning
confidence: 99%
“…V below. Of course, performing the necessary angular measurement would require rotational stabiliza-tion (or real-time monitoring) of the orbiting spacecraft relative to an inertial reference frame (e.g., a distant set of stars and/or quasars; the approach used, e.g., on Gravity Probe B [GP-B] [173][174][175][176]).…”
Section: (H) Showing the Frequency Rangesmentioning
confidence: 99%