C. W. F. Everitt 2026-11-05
C. W. F. Everitt led the Gravity Probe B experiment, which tested general relativity using four cryogenic gyroscopes in Earth orbit. The instrument measured slow changes in spin-axis direction relative to a stellar reference, separating the geodetic effect from frame dragging.
The 2011 final-results paper reported a geodetic drift of milliarcseconds per year and a frame dragging drift of milliarcseconds per year, compatible with the predicted values within the reported uncertainties. The latter effect was much smaller, illustrating why identifying and modelling instrument drifts was central to the test.[ref]
Figure 1.
C. W. F. Everitt receiving an award in 2011
. Everitt is on the left, as identified in the Stanford Gravity Probe B mission account of the 4 May 2011 presentation.
Frame dragging 2026-11-05
Frame dragging is the influence of mass-energy currents, especially rotation, on local inertial directions in general relativity. In a stationary axisymmetric metric tensor, an observer with zero angular momentum has coordinate angular velocity when the other spatial coordinates are held fixed. Around a rotating source this can be nonzero even without an applied azimuthal torque.
Gravity Probe B tested the effect with four cryogenic gyroscopes in Earth orbit, comparing their spin directions with a guide-star reference. Its analysis separated the much larger geodetic precession from the smaller rotation-dependent drift. This tests a change of inertial orientation, rather than ordinary frictional dragging of the spacecraft.[ref]
Gravity Probe B 2026-11-05
Gravity Probe B was a space experiment that measured the slow drift of orbiting gyroscope axes relative to a distant guide star to test general relativity. It targeted geodetic precession from motion through curved spacetime and frame dragging associated with Earth's rotation.
The apparatus used four nearly spherical gyroscopes operating at cryogenic temperature, a telescope tracking the guide star and superconducting magnetic readout of spin orientation. Drag-free spacecraft control reduced unwanted forces. A crucial challenge was separating the tiny relativistic drift from classical torques, including electrostatic surface-patch effects and changing gyroscope orientation.[ref]
The 2011 final analysis reported drift components and milliarcseconds per year, compared with predicted geodetic and frame-dragging values and . The signs depend on the stated sky-coordinate convention. Dividing uncertainty by the measured magnitude shows why the experiment tested the much larger geodetic effect more precisely than the smaller frame-dragging effect.[ref]