Ramjet engine rocket e.g. flight rocket, for e.g. air force, has ramjet engine comprising elongated diverging nozzle and truncated shaped air inlet device, and body, tail units and tanks separately assembled one after other

摘要

The rocket has a ramjet engine (D) comprising an elongated diverging nozzle (9) and a truncated shaped air inlet device (11). A long cylindrical body (1), tail units (15), liquid fuel tank (2) and a liquid oxidizing tank (3) are separately assembled one after the other and are provided for conduits connected to an aggregate of turbopumps (4). A main portion of the body is occupied by a rocket engine (C) composed of a combustion and mixing chamber (7). Housings are provided on a surface of the air inlet device for fixing profiled rigid elements (14) and the tail units.