Dynamic Characteristics of LOX/Kerosene Variable Thrust Liquid Rocket Engine Test System Based on General Modular Simulation Method

Table 1

Main parameters of the test system.

Parameters	Flow (kg/s)	Pressure (MPa)	Accuracy
Kerosene	2.5	5	1.5%
LOX	3.5	5	1.5%
Hydrogen	0.05	5	1%
Oxygen	0.1	5	1%
Nitrogen	1.5	5	1%
Coolant	2.5	2	1%