The invention relates to the field of high-strength single crystal superalloys and particularly provides a high-strength and tissue stable nickel-base single crystal superalloy with the temperature capability reaching to 1,150 DEG C. The high-strength and tissue stable nickel-base single crystal superalloy is mainly suitable for blade materials, used at the temperature of 1,100 DEG C or above, of an aero-engine. The superalloy comprises chemical components (wt%): 3%-5% of Cr, 6%-13% of Co, 6%-8% of W, 0.1%-2% of Mo, 4.5%-6% of Re, 2%-4% of Ru, 5.5%-6.5% of Al, 6%-10% of Ta, 0%-0.2% of Hf and the balance Ni. A preparation method comprises the steps that the temperature gradient range of a single crystal growth furnace is 40K/cm-80K/cm, the pouring temperature is 1,480 DEG C-1,550 DEG C, the mold shell temperature and the pouring temperature keep consistent, and a single crystal blade or a test bar is prepared within the growth rate range of 4mm/min-8mm/min; and then, solid solution homogenization treatment, high-temperature aging treatment and low-temperature aging treatment are carried out so that the superalloy can have high endurance strength. The service life of the superalloy is 100 h or longer under the endurance condition of 1,140 DEG C/137 MPa, and the endurance strength of the superalloy is equivalent to that of an EPM102 alloy; the high-temperature tissue stability is good; and a heat treatment window is wide, and solution treatment is easy to control.