Since the October 1988 update on the Commercial Atlas Launch System presented to the IAF, additional enhancements have been incorporated into the launch vehicles offered. Previous papers have dealt with performance and configuration details of the Atlas I, II, IIA launch vehicles. This paper discusses the latest addition to the line of Atlas launch vehicles, namely the Atlas IIAS, and other enhancements that have been made across the board. Discussion of the Atlas IIAS configuration includes details about structural upgrades made to the booster stage, the basic configuration of the solid rocket motors (SRMs) used, upgrades made to the launch facility, effects of the configuration change on spacecraft environments, and overall performance enhancement. By selective incorporation of the enhancement available, the performance of Atlas launch vehicles can be tailored to the specified requirements of particular missions. These capability enhancements include minimum residual shutdown of the Centaur upper stage, transverse spin separation, and small payload accommodations (SPA). When matched with existing capabilities of in-flight retargeting and precision pointing and injection accuracies, these improvements lead to the availability of a launch vehicle that can be tailored to a spacecraft's unique requirements. Finally, a review of performance capabilities for the entire line of Atlas launch vehicles is presented, capping a comprehensive view of the current state of the Atlas launch vehicle.