Modelling the reflective thermal contribution to the acceleration of the Pioneer spacecraft

Physics – Space Physics

Scientific paper

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Version accepted for publication in Physics Letters B. 19 pages, 7 figures, 3 tables

Scientific paper

10.1016/j.physletb.2012.04.034

We present an improved method to compute the radiative momentum transfer in the Pioneer 10 & 11 spacecraft that takes into account both diffusive and specular reflection. The method allows for more reliable results regarding the thermal acceleration of the deep-space probes, confirming previous findings. A parametric analysis is performed in order to set an upper and lower-bound for the thermal acceleration and its evolution with time.

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