Mostly CO2 and CO, see for instance https://en.wikipedia.org/wiki/RP-1
https://en.m.wikipedia.org/wiki/Kerosene The combustion reaction can be approximated as follows, with the molecular formula C12H26 (dodecane):
2 C12H26(l) + 37 O2(g) → 24 CO2(g) + 26 H2O(g); ∆H˚ = -7513 kJ
The atomic makeup of RP-1 is about CH1.97[1], so at stoichiometric ratio[2] that would yield 71.3% CO2 and 28.7% H2O by mass.
[1] http://www.qrg.northwestern.edu/projects/vss/docs/propulsion...
[2] in reality Falcon 9 burns fuel-rich