New Contour Design Method for Rocket Nozzle of Large Area Ratio

Table 4

Performance of the nozzle designed by different methods.

Mass flow		Var.
	(N)/ (s)	(N)/ (s)
-20%	590.98/320.55	592.22/321.22
-10%	665.73/320.97	667.14/321.65
Nominal	739.89/321.08	742.07/322.00
+10%	813.99/321.10	815.85/321.83
+20%	888.78/321.38	890.58/322.04