RU

Keyword: «helicopter»

The article presents the main features of the design of a springless torsion sleeve of a load-bearing unit.
The article discusses a method for improving the reliability of helicopter systems based on the use of high-energy-dense natural materials.
The article provides an analysis of various helicopter landing methods in emergency situations, provided and not provided for in the Flight Operation Manual of domestic helicopters of various modifications. A detailed analysis of the landing of the Mi-24P helicopter in autorotation mode with a minimum total pitch of the main rotor was performed.
The article is devoted to the technical operation of helicopters in the aviation hours of the VUNC Branch of the VVA Air Force in Syzran after the developed and proposed measures for the maintenance of aviation equipment. The main and main goal of all personnel of aviation units is to increase the combat readiness of aviation equipment by reducing its failures.
The article considers the main directions of development of aviation unguided missiles. Further development and perfection is reduced to the fact that aviation guided missiles are being developed on the basis of the latest samples of unguided missiles. It is possible that such missiles are being tested and may have already been put into service.