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Expander cycle engines are limited because you need heat to run the turbo pump. And the heat is provided by running propellant around engine to cool it off. The advantages Tim Dodd mentions for larger engines (propellant flow increases faster than surface area of the engine), are exactly the things that make expander cycle engines hit their limit: not enough area to heat up the propellant to run the pumps enough for the amount of propellant you need for the thrust you want.

Aerospikes have more surface area, which means more area to cool... which is more area for the propellant to flow through to get heated up to run the engine, which means more power available to give more fuel.



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