Uniaxial tensile test data for HAYNES 282 sa ta material at 21 °C

The FP7 project "In Space Propulsion 1" was set up to improve the fundamental knowledge and the techniques which are necessary to allow Europe to implement new ambitious space programs involving cryogenic propulsion. It concentrates on liquid oxygen, liquid hydrogen, and liquid methane propellants, and the anticipated progress will address - LOX methane combustion - heat and propellant management - materials tribology, compatibility, and hydrogen embrittlement. The data included here were generated in the part of the project relating to hydrogen embrittlement. In a frist step, materials of interest were screened through a literature research and by carrying out tensile tests in gaseous hydrogen (GH2) and Ar. As part of the screening process, tensile tests on INVAR and HAYNES 282 alloys have been carrid out in GH2 (gaseous hydrogen) as well as in Ar.

FP7项目“太空推进1号（In Space Propulsion 1）”旨在夯实基础认知、完善核心技术，助力欧洲开展涉及低温推进系统的雄心勃勃的新型太空计划。该项目聚焦液氧、液氢及液态甲烷推进剂，预期研究成果将覆盖以下方向：液氧-甲烷燃烧、热与推进剂管理、材料摩擦学、材料相容性及氢脆。本数据集收录的数据源自该项目中与氢脆相关的研究分支。研究伊始，团队通过文献调研及在气态氢（gaseous hydrogen, GH2）与氩气（argon, Ar）中开展拉伸试验的方式，对目标材料进行筛选。作为筛选流程的一部分，团队已在气态氢（gaseous hydrogen, GH2）及氩气（argon, Ar）中对因瓦合金（INVAR）与HAYNES 282合金开展了拉伸试验。