1. An exploraloiy study OS parallel-stage scparation OS rciisahlc launch vcliiclcs J.P.Decker -J. Gcra NASA-TND-4765 Octobcr 1968d
2. Method for determining interference components of atrodynamiccharacteristicsofaircraftsintegrated with a body ofrevolution atMach 3and 6 M.V. Mukovazov ("0Energia ) Applied Problems of Acromechanics and Geo-Cosmic Physics -Moscow, 1990(p.73) 8. Numerical simulation of three dimensional and unsteady aerodynamics about bodies in relative motion applied InaTSTOseparation P. Brenner AIAA-93-5142 figure 3 TSTOlauncher(RADIANCE) Fitstageusingairbreathing propulsion