Mathematical Modeling of the Strength of Parachuteless Airdrop Systems From Helicopters

Abstract

The article is devoted to the simulation of parachuteless airdrop system from helicopters during tests. The issue of testing the equipment strength for parachuteless airdrop is considered in detail. Simulated mathematical modeling of the structural strength characteristics of the parachuteless airdrop system was performed. An assessment of the power strength elements of the removable on-board equipment for parachuteless airdrop design from helicopters is given.