A system for providing hydrogen enriched fuel, comprising: a. a first gas turbine comprising: i. a first compressor, wherein the first compressor produces a first compressed working fluid; ii. a combustor downstream of the first compressor; iii. a first turbine downstream of the combustor; b. a second gas turbine comprising: i. a second compressor in fluid communication with the first compressor, wherein the second compressor receives a portion of the first compressed working fluid from the first compressor and produces a second compressed working fluid having a higher pressure than the first compressed working fluid; ii. a fuel compressor in fluid communication with a fuel source and including an inlet and an outlet, wherein the fuel compressor receives a fuel through the inlet from the fuel source at a first pressure and a first temperature and provides a compressed fuel at a higher pressure and a higher temperature than the first pressure and the first temperature; iii. a reformer downstream of the second compressor and the fuel compressor, wherein the reformer receives the second compressed working fluid and the compressed fuel and produces a reformed fuel; iv. a second turbine downstream of the reformer, wherein the second turbine receives the reformed fuel and produces a cooled reformed fuel; and c. a fuel skid in fluid communication with the second turbine and the combustor, wherein the fuel skid provides a flow path for the cooled reformed fuel from the second turbine to the combustor. a. a first gas turbine comprising: i. a first compressor, wherein the first compressor produces a first compressed working fluid; ii. a combustor downstream of the first compressor; iii. a first turbine downstream of the combustor; i. a first compressor, wherein the first compressor produces a first compressed working fluid; ii. a combustor downstream of the first compressor; iii. a first turbine downstream of the combustor; b. a second gas turbine comprising: i. a second compressor in fluid communication with the first compressor, wherein the second compressor receives a portion of the first compressed working fluid from the first compressor and produces a second compressed working fluid having a higher pressure than the first compressed working fluid; ii. a fuel compressor in fluid communication with a fuel source and including an inlet and an outlet, wherein the fuel compressor receives a fuel through the inlet from the fuel source at a first pressure and a first temperature and provides a compressed fuel at a higher pressure and a higher temperature than the first pressure and the first temperature; iii. a reformer downstream of the second compressor and the fuel compressor, wherein the reformer receives the second compressed working fluid and the compressed fuel and produces a reformed fuel; iv. a second turbine downstream of the reformer, wherein the second turbine receives the reformed fuel and produces a cooled reformed fuel; and i. a second compressor in fluid communication with the first compressor, wherein the second compressor receives a portion of the first compressed working fluid from the first compressor and produces a second compressed working fluid having a higher pressure than the first compressed working fluid; ii. a fuel compressor in fluid communication with a fuel source and including an inlet and an outlet, wherein the fuel compressor receives a fuel through the inlet from the fuel source at a first pressure and a first temperature and provides a compressed fuel at a higher pressure and a higher temperature than the first pressure and the first temperature; iii. a reformer downstream of the second compressor and the fuel compressor, wherein the reformer receives the second compressed working fluid and the compressed fuel and produces a reformed fuel; iv. a second turbine downstream of the reformer, wherein the second turbine receives the reformed fuel and produces a cooled reformed fuel; and c. a fuel skid in fluid communication with the second turbine and the combustor, wherein the fuel skid provides a flow path for the cooled reformed fuel from the second turbine to the combustor.