Evolution of mathematic simulation instruments for space launch vehicle engine devices

Aerospace propulsion engineering


Аuthors

Partola I. S.

Abstract

A typical composition of space launch vehicle (SLV) engine devices (ED) is under consideration. An interconnection between control hard and soft instruments for engine devices and ED effectiveness growth is shown. Stages of evolution of mathematic simulation instruments for SLV ED systems and processes are detailed. A conclusion about necessity of mathematic simulation instruments development as ED effectiveness growth base is formulated. The task to develop common mathematic simulation instruments complex for ED processes and control algorithms is postulated as basis to cut ED experimental verification duration and costs.

Keywords:

space launch vehicle, engine device, liquid rocket engine, mathematic simulation complex.


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