Detent force umbrella for reentry deceleration of reentry capsule
A return capsule and magnetic resistance technology, which is applied to the system of the spacecraft returning to the earth’s atmosphere, the landing device of the spacecraft, etc., to achieve accurate landing, reduce control difficulty and risk, and improve deceleration efficiency
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[0012] The following introduces specific embodiments as the content of the present invention, and the content of the present invention will be further clarified through specific embodiments below. Of course, the description of the following specific embodiments is only to illustrate the content of different aspects of the present invention, and should not be construed as limiting the scope of the present invention.
[0013] In order to make the present invention more comprehensible, preferred embodiments are described below in detail with the accompanying drawings.
[0014] figure 1 Shows the structural schematic diagram of the magnetic resistance umbrella used for the reentry deceleration of the return capsule of the present invention, wherein the magnetic resistance umbrella of the present invention includes a front plasma collecting electrode 3 and a rear plasma collecting electrode 3 respectively arranged in the return capsule 1. The collecting electrode 2 and the multi-turn c...
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