MISSILE WITH CASELESS NOZZLELESS ENG-IGNITION ENGINE (VERSIONS) Russian patent published in 2013 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: proposed missile comprises head and solid propellant charge. In compliance with one version, proposed missile comprises sliding finned bush arranged at solid propellant. Said bush is equipped with impellers for threads connected with missile head to be wound thereon. In compliance with another version, missile head accommodates impeller with skewed or crosswise vanes and is connected with spools. The latter are connected by thread with sliding bush and fin. In compliance with one more version, missile head accommodates motor, reduction gear and two or more spools for thread winding. The latter are connected by thread with sliding bush and fin. In compliance with the other version, missile fin is composed of several fins glued to engine charge and jointed in one plane "heat-to-tail" or "ledge-to-slot". In compliance with one more version, missile head accommodates motor, reduction gear and two or more spools for thread winding connected with sliding bush with gas rudders or interceptors.

EFFECT: better controllability.

10 cl, 3 dwg