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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 2
/
Research Article
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
H
2
N
2
H
2
O
CO
2
(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