Research Progresses of Flash Evaporation in Aerospace Applications

Table 3

The thrust of the hot-water rocket engine, superheated steam rocket engine, and conventional rocket engine [50].

Initial pressure (MPa)	Hot-water rocket engine (N)	Superheated steam rocket engine (N)	Conventional rocket engine (N)
13.6	1616.2	957.9	1120.8
7.15	670.3	484.4	548.2