For every pound you must invest in the heat shield for the recoverable rocket's orbital* stage you will lose one pound of payload. Does it make sense then to recover simple tankage? Perhaps one should only recover the engines, pumps, and avionics. I.e., something like** ULA's "SMART" but applied to the upper stage***.
* typically second stage
** may or may not use inflatable heat shield
*** or think drop tanks
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