the ordinary steel that you initially mentioned will do just the same job as 4130 (at 10-20% of the cost ?)
these are not aviation-type steady loads, IMO you cannot design to stresses that will take 4130 close to its elastic limit
(only if so designing would the ordinary steel need to be thicker (than the 4130) to avoid going beyond its elastic limit)
those spaceframe race cars even in F1 were made from the cheaper material for this reason
anyway, best wishes for your project !