ANALYSIS OF THE PROCESS OF EVACUATION HYDROGEN AT SUPERCRITICAL PARAMETERS FROM THE TANKS SYSTEMS OF ENERGY SUPPLY ORBITAL SHIP
DOI:
https://doi.org/10.18198/j.ind.gases.2012.0648Keywords:
Liquid hydrogen, Cryogenic tank, Storage systems and preparation of reagents the orbital ship systems of energy supply (SSPR SES OS), Evaporator heat exchanger hydrogen, Communications of liquid hydrogen, Capacity to drain hydrogen, Start complexAbstract
In case of delayed or failed start orbital ship on the launch complex, and post-flight servicing of the aircraft must be carried out the hydrogen evacuation from the storage capacity and the preparation of reagents energy supply systems (SSPR SES) orbital ship. Draining a hydrogen in tanks at supercritical parameters, it is necessary to carry out in the ground stationary and transport systems that provide it`s secure appointment. Report the results of research works JSC «Uralkriomash» for development of methods and means of the hydrogen evacuation within the container SSPR SES the orbital ship at supercritical parameters in industrial processes in the start or landing complex orbital ship.
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