An independent and conserved source of fuel and / or power comprises a top stage
rocket engine firing up to 5000 F. at very high pressures, delivering jet flows up to
transonic velocities into a near adiabatic tunnel for mixing in general and / or for transforming reactants introduced to suit specific objectives. The related compression is supplied by an independent
prime mover which compresses its exhaust and other recoverable fluids. Low grade flows, thereby upgraded in
temperature and pressure, are adiabatically contained, are further upgraded in the tunnel to become part of the prescribed fuel for export at the tunnel ends; or fuel to be fired in a
prime mover for electric or other power, or
hydrogen for chemical use. Expansion turbines for this purpose are relieved of the load used to compress the excess air in standard
gas turbines thus increasing export power. A portion of the expansion
turbine's exhaust becomes part of recoverable fluids. When
oxygen is used instead of air, the gases through turbines are
nitrogen-free with more
heat capacity reducing
turbine inlet temperatures for the same power. When reactant transformation is specified, the larger
water vapor content in the cycle enhances the
water gas / shift autothermally for
ammonia and / or power and alternatively for
pyrolysis cracking for olefins and diolefins. Further, staging
rocket engine reactors increases efficiency in boilers and steam turbines; and staging can produce
sponge iron and / or iron
carbide as well as expansion
turbine power and
fuel cells for peak and off-peak loads.