AAWSAP DIRD, MHD Air Breathing Propulsion and Power for Aerospace Applications, November 2010
DOW-UAP-D149 · page 20 of 32
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-------- UNCLASSIFIED/ /FOR AFEICIA.k W&i 8,.LY ----------> ------> --- .:,, ---- --> Air counterflow -->---- ', ' ' ' ' ' Aerodynamic: heat : ' ' 't' EleC'/oc energy I 000 0 00-00 l [ ~<>'""'o'""'o'""a:-L , -l----->--:;""'ct;,o..,,-o---'-N.::::ozzle: , a ... -------- ... ,--------- I v MHD controlled inlet ~-----------------, ----------------- '/ ' MHD accel9:rator ' Combustion chambe~ _, Modified CheJlllcal Hem Magneto-Plasma-Chem1cal Rege,nernrion S~cern Engine (MPCE) fuel Figure 7. Schematic of Ajax Hypersonic Vehicle Concept. The upper and lower pictures represent the same concept, but were published by the authors (A. Kuranov et al.) at different times. The key idea of the Ajax is that, with propulsion, aerodynamic, and heat protection system for hypersonic vehicles hitting their theoretical and practical limits, the only way beyond these limits is smart management of energy (i.e., taking energy from the surrounding flow and putting that energy where it is needed for propulsion benefits). The following three major concepts/systems are included in Ajax: 24 • Endothermic fuel conversion. A mixture of hydrocarbon fuel (similar to kerosene) and water initially stored on board is used to cool the external surfaces and engine walls, and the heat transferred to the mixture is used in UNCLASSIFIED/FQA QFFHiilif.tl: WOE 8,.L'I 16