629.762 Mathematical methods for optimal selection of linear increasing over time mass-flow characteristics of energy devices ensuring aircraft gas-dynamic ejection with specified parameters

Plyusnin A. V. (Bauman Moscow State Technical University/JSC MIC NPO Mashinostroyenia)

GAS DYNAMICAL EJECTION, LAUNCHING POD, CRAFT, SOLID PROPELLANT, TUBULAR GRAIN


doi: 10.18698/2309-3684-2019-3-5785


The paper proposes the theory for optimized selection of linear increasing over time mass-flow rates of energy devices designed for craft gas dynamic ejection from a launch container under the specified restrictions on parameters. Theory is also proposed for optimized selection of geometrical parameters of multigrain tubular charge for implementing these mass-flow rates. A visual geometric interpretation of theoretical developments is presented, and their practical feasibility is confirmed by numerical simulations of parameters of gas-dynamic ejection and internal ballistics processes.


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