Risk Assessment and scaling for the SLS LOx ET

[摘要] In this report we analyze the transpiration cooling by He bubble injection of the long LOx tank feedline heated by the environment heat. We consider possible hazards that can arise in the proposed design of the SLS core stage where the feedline length is much longer than that used in the Space Shuttle.

[发布日期] 2012-12-01

[学科分类] 航空航天科学