Endothermic Heat Sinks for High-speed Supersonic Applications

Traditional fuel system designs do not provide the combination of sucient cooling and low system weight at the Mach 5+ range. Thus, if currently available non-cryogenic propellants are to be employed, an additional heat sink source beyond a simple physical heat sink is required to meet the regenerative cooling demand. The endothermic...

Exergy loss reduction by combining exothermic and endothermic reaction routes

Document(en) uit de collectie Chemische Procestechnologie