This invention relates to the field of
rocket engine testing technology and discloses a method for handling hazardous media, comprising: setting a first and a second field
torch above the
thrust chamber of the
rocket engine, and setting a third field
torch below the
thrust chamber; the first, second, and third field torches are adapted to ignite the
hydrogen-
oxygen mixture discharged before the pre-
combustion chamber ignites; a fourth and a fifth field
torch are respectively arranged to the left and right of the
thrust chamber of the
rocket engine; the fourth and fifth field torches are adapted to ignite the
hydrogen-rich gas discharged after the pre-
combustion chamber ignites; both the
hydrogen-
oxygen mixture and the hydrogen-rich gas are hazardous media. This application, by setting five field torches and using field ignition, can promptly ignite the hazardous media discharged from the thrust chamber outlet of the
rocket engine, safely
handle the hydrogen-
oxygen mixture and hydrogen-rich gas, and meet the
safety testing requirements of rocket engines.