This paper proposes the development of small satellite launch vehicles by using the method of solid rocket missiles.
The requirements for military small satellites were assumed to be the number and capability of satellites required responding to TCT(Time Sensitive Target) in case of emergency. And the requirements of launch vehicle are the capability and quantity that can meet the small satellite requirements. As a result, in this paper, a method and a tool for verifying the performance of a launch vehicle are presented, and an alternative analysis procedure and method for determining the number of launch vehicle is presented.