• Aztec: A TSTO Hypersonic Vehicle Concept Utilizing TBCC and HEDM Propulsion Technologies 

      Kokan, Timothy Salim; Hutchinson, Virgil L., Jr.; Reeves, John Daniel; Olds, John R. (Georgia Institute of Technology, 2004-07)
      The Aztec reusable launch vehicle (RLV) concept is a two-stage-to-orbit (TSTO) horizontal takeoff, horizontal landing (HTHL) vehicle. The first stage is powered by ten JP- 5 fueled turbine-based combined-cycle (TBCC) ...