Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5472202 | Acta Astronautica | 2017 | 6 Pages |
Abstract
Among them are the following: firstly, the unused propellant residues in tanks convective gasification based on the hot gas (heat carrier) supply in WS tanks after main liquid propulsion engines cutoff is proposed as the basic technology; secondly, the obtained unused propellant residues in WS tanks gasification products (evaporated propellant residues + pressurizing agent + heat carrier) are used for WS stabilization and orientation while descending trajectory moving. The applying of the proposed technologies allows providing fire and explosion safety requirements of LV with main liquid propulsion engines practically.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
V. Trushlyakov, Ya. Shatrov, B. Sujmenbaev, D. Baranov,