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Residual accelerations due to thermal effects are estimated through a modelof the New Horizons spacecraft and a Monte Carlo simulation. We also discussand estimate the thermal effects on the attitude of the spacecraft. The work isbased on a method previously used for the Pioneer and Cassini probes, whichsolve the Pioneer anomaly problem. The results indicate that after theencounter with Pluto there is a residual acceleration of the order of$10^{-9}~\mathrm{m/s^2}$, and that rotational effects should be difficult,although not impossible, to detect.

Estimating the thermally induced acceleration of the New Horizons spacecraft