05 - Propulsion
RESEARCH OF PROPULSION ENGINES FOR ADVANCE REUSABLE TSTO AEROSPACE SYSTEM
A.I. Lanshin¹, O.V. Sokolova¹, Y.M. Shikhman¹, V.E. Shlyakotin¹; ¹CIAM, Russia
An attractiveness of the TSTO for delivery of payload into low earth orbit is showed. The TBCC aeroplane-accelerator propulsion (GTE+RAMJET, Mmax=6-7) with endothermic hydrocarbon fuel is discussed. Some results of the TBCC engines calculation and the model DMRAMJET tests with gasified kerosene and its thermodestruction products is presented.