The invention provides an experimental device for sampling
combustion soot of a space
station, and belongs to the technical field of microgravity
combustion and
combustion diagnosis systems, and the experimental device specifically comprises a mounting seat which is used for being connected with a
combustor mounting position on a gas experimental plug-in; the multi-jet
combustor is mounted on the mounting seat, the multi-jet
combustor comprises a fuel
pipe and a wake gas channel, the end, away from the mounting seat, of the multi-jet combustor serves as a combustion end, and fuel and wake gas are ignited after being converged at the combustion end; the sampling
assembly is detachably mounted on the combustion end, the sampling
assembly comprises a plurality of probes, and the sampling ends of the probes are in contact with the
flame of fuel combustion so as to sample the combustion
soot of the fuel; the protective cover is detachably connected with the sampling
assembly, the protective cover is used for surrounding the probe, and the protective cover is connected with the sampling assembly after the fuel is combusted and the sampling assembly completes sampling. The device can be applied to a space
station combustion
scientific experiment system, and the functions of
flame ignition,
soot sample collection and the like are achieved.