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.
Progress on Ares First Stage Propulsion
2008
3 pages
Report
No indication
English
Space Launch Vehicles & Support Equipment , Ares 1 first stage , Ares 1 launch vehicle , Ares 5 cargo launch vehicle , Spacecraft propulsion , Spacecraft design , Spacecraft launching , Reusable rocket engines , Space shuttle boosters , Nasa programs , Project management , Propulsion system performance , Manned space flight , Space exploration , Launch vehicle configurations , Booster recovery
Progress on Ares First Stage Propulsion
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