1. • EELVORDAFSPC002-93-II
2. • EELV through2029;MinotaurI/IV through2019 • Planneddevelopmentfor next-gen med-heavy launcherstarts in FY15, with
3. Configuration choices that can mitigate these technical challenges such as both stages burning in parallel from liftoff to reduce the lateral c.g. shift or mounting the upper stage on the nose of the booster to keep the c.g. in the same line can reduce the aerodynamic interactions between the stages. An integrated reusable booster demonstrator, may not need to be demonstrate these options since successfully demonstrating the side mounted, sequentially burning stagesshouldprovideanupperbound interms of technicalchallengesfor the ascentphaseof anRBS.