The invention discloses a
water pressure detection device for a
solid rocket engine. The device consists of a
combustion chamber shell, a spray
pipe shell, a top cover, a rear blanking cap, a
cushion block, a sealing ring, a bolt and a locking nut, the top cover is connected with the front connector through a bolt, and a first sealing ring is arranged on the front connector of the
combustion chamber shell. The spray
pipe shell is connected with a
combustion chamber shell rear connector through a bolt, and a second sealing ring is arranged on the
combustion chamber shell rear connector. A step is arranged on the largest outer cylindrical surface of the rear blanking cap and forms an end face sealing groove with the
tail step of the spray
pipe shell, and a third sealing ring is installed; the small end of the rear blanking cap is provided with an external thread, penetrates through the step at the
tail part of the spray pipe shell and the
cushion block, and is tensioned by the locking nut; the middle of the rear blanking cap is provided with a through hole as a water
inlet channel, and the small end is provided with internal threads for connecting a water inlet pipe. The pressure
bearing capacity of the
combustion chamber shell, the spray pipe shell and the top cover is examined through one-time
hydraulic test, the sealing performance of the sealing ring and the strength performance of the connecting structure are examined, and efficiency is improved.