Heat Conductor Reservoir (HCR)
Assume that you will be using the heat conductors shown in the sub-title Heat Conductors or sorts whose characteristics are close to those .
For a 3 stage amplification:
HCR-1 would then contain R600
The HCR in ICG1 would contain R30
HCR-3 would contain n-heptane.
The Turbine propellant for the Back End would be a mix or type that reaches 15 bar, when n-heptane is at about 5 to 8 bar.
For a 2 stage amplification:
HCR-1 would then contain R600
HCR-3 would contain R30.
The Turbine propellant for the Back End would be a mix or type that reaches 15 bar, when R30 is at about 5 to 8 bar.
The outlets and inlets for the propellant entering the turbine chamber would then have widths that are multiples of 1cm2 in order to produce the required amount of NM force for the Turbine blades.
HCR-1 does not have any special insulation, because it operates at environmental temperatures. All other HCRs will have insulation, because they operate at temperatures above 50° C.
All other HCRs will also have a jacket through which in coming heat is passed, so that it's heat conductor content will have a temperature that is the same as the amplified input of the in coming heat, caused by vapor compression in the Cmp-P pumps.
That allows follow up stages to start collecting heat at temperatures that would otherwise not be possible.
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Heat conductor reservoir component types used in Solar heat engines
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