FIELD: measurement technique.
SUBSTANCE: invention refers to the field of space technology and is intended for determination on board of space object of position coordinates of space object module pressure skin puncture by interstellar-dust or technogenic particle. The result is provided by accommodation of five pressure sensors inside pressure skin of unmanned space object, their coordination in coordinate system of the space object and fixing by pressure sensors time moments of soundwave front passing, and puncture position is determined from relations given in formula.
EFFECT: operative, at the rate of puncture determination of puncture position coordinates and minimisation of puncture position coordinates determination error due to optimal location of pressure sensors inside pressure skin of unmanned space object.
2 cl, 5 dwg
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