This invention provides a
rocket jet
test structure, including a support rod, a connector, a
projectile body, a balance, a high-
pressure pipe, a
tail section, a
gas chamber, a
nozzle I, a
nozzle II, a
nozzle seat, and a support rod. One end of the support rod is connected to an external gas source pipeline, and the other end is connected to the balance, the support rod, and the high-
pressure pipe, introducing the external gas source into the high-
pressure pipe. The connector is sleeved on the outside of the support rod, with both ends fixedly connected to an external wind tunnel test mechanism and the support rod, respectively. The
projectile body,
tail section, and nozzle seat simulate the shape of a
rocket shell. One end of the
projectile body mates with the
conical surface of the balance, and the other end is connected to the
tail section. The other end of the tail section is sealed by the nozzle seat, on which a nozzle II that does not participate in the jet is installed. The high-pressure
pipe, the
gas chamber, and the support rod are located within the cavity formed by the projectile body, tail section, and nozzle seat. The high-pressure
pipe is connected to the
gas chamber, and the support rod is fixedly connected to the gas chamber. The nozzle I that participates in the jet is fixed at the end of the gas chamber. The support rod, the high-pressure
pipe, the gas chamber, and the nozzle I form a complete gas path. The gas introduced from the support rod flows through the pipeline and is ejected from the nozzle I.