Systems Engineering of Agena Aerospace Ground Equipment

This paper discusses problems of performing systems engineering in order to establish optimum and economical A. G. E. configurations in support of R & D missions in a multi-program, multicomplex environment. The combination of short lead-times, high launch rates and varied dynamic requirements of a large number of different yet simultaneous R & D operations provides a unique support situation. The problem has grown from support of the first successful orbiting vehicle in 1959 to last year´s support of 36 successful launchings. The advantages of utilizing MIL-D-9412D to enhance systematic documentation of the A. G. E. system considerations and configuration will also be emphasized.