Abstract-This essay firstly analyzed the development trend of space debris, and the establishment of a development model of low-orbit space debris size. On this basis, this essay in-depth analysis of the efficiency of different methods to eliminate debris. The relational model is built for the elimination of space debris each way and cost efficiency, compare and contrast the applicability of the different methods. Finally, we analyzed separately from a risk, cost, and risk appetite three angles. We are considered different situations to build combinatorial optimization model made a different way to eliminate space debris, which could optimize the choice under different restrictions.