3Marty Bradley,Kevin Bowcutt,James Mc Comb.Revolutionnary Turbine Accelerator(RTA)Two-Stage-to-Orbit(TSTO)Vehicle Study[R].AIAA 2002-3902.
4Paul A.Bartolotta,Nancy B.Mc Nelis,High Speed Turbines:Development of a Turbine Accelerator(RTA)for Space Access[R].AIAA 2003-6943.
5Douglas G.Shafer.Development of a Ground Based Mach 4+Revolutionary Turbine Accelerator Technology Demonstrator(RTATD)for Access to Space[R].ISABE 2003-1125.
6High Mach Turbine Engines for Access to Space Launch Systems,AIAA 2003-5036.
7Johnson,R.,Allison Gas Turbine Division,Indianapolis,IN,“Cycle Selection Considerations for High Mach Applications”,AIAA-87-2105,23rd JPC,June 29-July 2,1987,San Diego,CA.
8Snyder,L.And Escher,D.,AADC,Indianapolis,IN“,Access to Space(ATS)Turbine Engine Capabilities”,JANNAF,November,2002,Orlando.
9RECOVER BLEED AIR TURBOJET,U.S.Patents Nos.141,571.