Variable-expansion-ratio spray pipe of single-chamber double-thrust solid rocket engine
A solid rocket, dual-thrust technology, applied in rocket engine devices, machines/engines, mechanical equipment, etc., can solve the problems of complicated nozzle design process, affecting missile range, increasing missile bottom resistance, etc., to achieve rapid reduction in structural strength, The effect of low density and increased thrust
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[0034] The technical solutions in the embodiments of the present application are clearly and completely described below in combination with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of this application.
[0035] like figure 1 As shown, the application provides a single-chamber double-thrust solid rocket motor variable expansion ratio nozzle, including a nozzle body 1, the nozzle body 1 has a nozzle outlet, and the nozzle body 1 is close to the nozzle outlet. The nozzle expansion section is fixedly connected at the position, and the nozzle expansion section includes the front section 2 of the nozzle expansion section and the rear section 3 of the nozzle expansion section. The rear sec...
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