On existing mathematical model of the influence of power winds on rocket in process of her(its) flight, are received importance’s of the value of the deflection of the rocket of the type "land-land" from plane of the shooting. The simplified form of the rocket is Considered in the manner of collections of the cylinder and cone. Three - dimensional and mass features two considered rockets are chose approximately, flight path of the rockets are simplified for simplifications of the calculation of the values of the deflections of the rocket. The Main problem of the article - a practical results of the values of the deflections of the rocket from plane of the shooting that allows to value, insofar greatly or small power winds can influence upon deflections of the rocket of the type "land-land" in process of the flight.
deflection of the rocket, lateral speedup of the rocket, velocity winds
"Otklonenye raketы ot ploskosty strelbы pod vozdeistvyem sylы vetra" ,
Information Processing Systems,