Hanson-Haber aircraft engine for the production of stratospheric compounds and for the creation of atmospheric reflectivity and absorption and to increase ground reflectivity of solar radiation in the 555nm range and to increase jet engine thrust and fuel economy through the combustion of ammonia and ammonia by-products

An aircraft engine modification consisting of a ring of structures containing Haber Processes surrounding and lying longitudinally along the high pressure and high temperature area of an aircraft engine consisting of two cooperating pathways:

• Pathway A (particulate dispersion), wherein
• a) an initial Haber Process would lead to
• b) a higher temperature, higher pressure, higher efficiency Haber Process sitting above it with 0
• c) both Haber processes leading to,
• d) an ammonia bypass chamber,
• e) a Urea production chamber (CO2+NH3),
• f) a Urea distillation chamber and flash drum and/or vacuum evaporator and
• g) a miniature Prilling tower where various sections could be combined or repurposed for the different steps in the Urea production process, and where the entire pathway would produce a mixture of Ammonia and Urea which can be ejected into the aircraft engine contrail, and
• Pathway B (thrust) which would be identical to Pathway A except instead of structures dedicated to Urea production there would be
• h) an ammonia combustion chamber,
• i) a nitrous oxide creation chamber which could either be ported directly into
• j) the main combustion area of the engine via nozzles or
• k) into a secondary (Jet A, ammonia/methane mix, or other fuels) combustion chamber which produces thrust.