| 摘要 |
The invention relates to rocket and space technology, in particular to the aircrafts, such as carrier rockets that perform a flight in the atmosphere. The invention provides a high accuracy of hitting the fall area. In a method of rescue of a detachable part of an aircraft, mostly of a stage of a carried rocket, consisting in formation and execution during flight in the atmosphere of the given program, its orientation relative to the oncoming flow, after separation of a stage its spatial angle of attack and the rate of change of this angle with prediction of the stage miss are measured, then it is determined the angle of attack of stage and/or its rate of change or rate of change of angle of attack, and/or the moment of change the current value of this rate up to a value sufficient to compensate for the miss, and angular movement with the parameters is imparted to the stage, and in case of impossibility of performance of the operation - prior entering the atmosphere rotation around the transverse axis with maximum angular speed is imparted to the stage. |
