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

Table 1

van der Waals constants.

	He	H2	N2	H2O	CO2
(K)	5.19	33.18	126.10	647.13	304.19
(MPa)	0.23	1.31	3.39	22.06	7.38
(Pa·m^6·kg^−2)	215.9	6016.8	174.1	1706.3	188.7
(m^3/kg)	0.0059	0.0130	0.0014	0.0017	0.0010