The invention discloses a manufacturing method of an Mg-Sc
shape memory alloy matched with service environments of the moon and the Mars and having
large strain and wide temperature range performance, and belongs to the field of research of high-performance shape memory alloys for moon and Mars exploration. The invention aims to solve the problems of low hyperelastic temperature window, low recoverable strain and the like of the Mg-Sc
alloy. Cyclic heat treatment after deformation is adopted to induce abnormal growth of
crystal grains, materials in different
crystal grain states are prepared, and the reason of the abnormal growth of the
crystal grains is from huge
internal stress and subboundary generated in the materials in the cyclic
phase change process. The prepared
single crystal material is subjected to low-temperature aging treatment, so that an
alloy parent phase is converted into an ordered state from a disordered state, and the yield strength of the
alloy is remarkably improved, so that the recoverable strain of the Mg-Sc alloy is improved; in addition, due to the ordered nanometer domain formed in the ordered state, the stress
lag in the superelastic deformation process of the alloy is effectively reduced, the superelastic deformation
critical stress sensitivity is reduced, and then the superelastic temperature window of the alloy is increased. When the alloy exists in the form of a large-size
single crystal, and the result is shown as lt; 110gt, 110gt; and when the crystal is oriented, the hyperelasticity is particularly remarkable.