Propulsion and Thermodynamic Parameters of van der Waals Gases in Rocket Nozzles

Table 2

Maximum densities (1000 K and 35 MPa) and critical densities (Data from [24]).

	He	H2	N2	H2O	CO2
(kg/m^3)	16.9	7.95	104.92	83.25	170.60
(kg/m^3)	69.64	31.26	313.30	322.00	467.60