The invention relates to a catapulting engine. The catapulting engine comprises a shell body, charging assemblies, a rear top cover, a spray
pipe, an igniting device, a volution, a front bolt, a rearbolt, a from top cover sealing ring, a rear top cover sealing ring, and a spray
pipe sealing ring. The catapulting engine has the advantages of large increased
area ratio, simple structure, mature process, wide
working temperature range, and good trajectory performance. Two rows of charging assemblies are evenly distributed in a
combustion chamber shell body, and after ignition of the engine, fuelgas amount of the catapulting engine is gradually increased with time. A two-path ignition tube is installed at the head part, redundancy design is conducted, reliable ignition energy is provided, and spherical
propellant is ignited. The volution is used to fix the spray
pipe at the
tail part, and the process is mature, simple and convenient. The catapulting engine can be applied to of
missile orcarrier
rocket emission in a wide temperature range, the initial overload is low, and the stability and reliability of
missile or carrier
rocket emission are improved.