Over the past several years there has been a significant effort within
the United States to assess options to replace the Space Shuttle some
time after the turn of the century. In order to provide a range of te
chnology options, a wide variety of vehicle types and propulsion syste
ms have been examined. These vehicle concepts which are representative
of the classes of concepts that could be proposed for any future vehi
cle development is being used in the initial phase of the access to sp
ace activity to identify requirements for the technology maturation ef
fort and to assess approaches to achieve the required low operations c
ost. This paper provides the results of recent systems analyses and de
scribes the ongoing technology maturation and demonstration program su
pporting the Reusable Launch Vehicle Program.