The Orbital Acceleration Research Experiment (OARE), which has flown o
n STS-40, STS-50, and STS-58, contains a three-axis accelerometer with
a single, nonpendulous, electrostatically suspended proofmass, which
can resolve accelerations to the 10(-9) g level, The experiment also c
ontains a full calibration station to permit in situ bias and scale-fa
ctor calibration, This on-orbit calibration capability eliminates the
large uncertainty of ground-based calibrations encountered with accele
rometers flown in the past on the Orbiter, and thus provides absolute
acceleration measurement accuracy heretofore unachievable, This is the
first time accelerometer scale-factor measurements have been performe
d on orbit, A detailed analysis of the calibration process is given, a
long with results of the calibration factors from the on-orbit OARE fl
ight measurements on STS-58, In addition, the analysis of OARE flight-
maneuver data used to validate the scale-factor measurements in the se
nsor's most sensitive range are also presented, Estimates on calibrati
on uncertainties are discussed, These uncertainty estimates provides b
ounds on the STS-58 absolute acceleration measurements for future appl
ications.