The National Aeronautics and Space Administration (NASA) Ares Projects Office (APO) is continuing to make progress toward the final design of the first stage propulsion system for the Ares I crew launch vehicle and the Ares V cargo launch vehicle. Ares I and Ares V will provide the space launch capabilities necessary to fulfill NASA's exploration strategy of sending human beings to the Moon, Mars, and beyond. As primary propulsion for both the Ares I and Ares V, the Space Shuttle-derived Reusable Solid Rocket Motor (RSRM) is one of the first and most important components to be tested. The first flight of Ares I, called Ares I-X, will occur in April 2009. The Ares I-X flight will use a combination of flight and simulation hardware to obtain data on controlling the long and narrow crew launch vehicle configuration.


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    Progress on Ares First Stage Propulsion

    Priskos, Alex S. / Tiller, Bruce / Jackman, Angie | NTRS | 2008


    Progress on Ares First Stage Propulsion

    Priskos, Alex S. / Tiller, Bruce | NTRS | 2008


    Progress on Ares First Stage Propulsion

    Priskos, Alex / Tiller, Bruce / Garson, Regina | AIAA | 2008


    Progress on Ares First Stage Propulsion

    Priskos, Alex S. / Williams, Thomas J. / Brasfield, Fred et al. | NTRS | 2008


    Ares I First Stage Propulsion System Status

    Priskos, Alex S. | NTRS | 2010