A Rocket Based Combined Cycle combustor model is tested at a ground direct connected rig to investigate the flame holding characteristics with a small rocket exhaust using liquid kerosene. The total temperature and the Mach number of the vitiated air flow. at exit of the nozzle are 1505 K and 2. 6. https://www.parisnaturalfoodes.shop/product-category/all-purpose-baking-flour/