The invention relates to the technical field of manned spacecrafts, in particular to a re-entry
capsule device. The re-entry
capsule capsule device comprises a capsule body, wherein an installation
blind hole is formed in the bottom face of the capsule body, a containing
blind hole is formed in the side wall of the installation
blind hole, a first sliding groove is formed in the side wall of the installation blind hole, and a second sliding groove is formed in the side wall of the containing blind hole; an anti-
impact column body inserted into the installation blind hole, wherein the lower end of the anti-
impact column body abuts against an anti-heat insulation cover, the side wall of the upper end of the anti-
impact column body is provided with a first protruding block, and the lower end of the first sliding groove is provided with a first limiting block; a blocking column body inserted into the containing blind hole, a spring is pressed between one end of the blocking column body and the end wall of the containing blind hole, a second convex block is arranged on the side wall of the end, and a second limiting block suitable for blocking the second convex block is arranged at the end of the second sliding groove. According to the re-entry capsule device provided by the invention, the anti-impact column body can
resist the impact force borne by the anti-impact column body under the blocking force of the blocking column body, so that the damage caused by direct collision between the capsule body and the ground is avoided, and the safety of astronauts and precise instruments is ensured.