The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies

Some data on the knowledge base to support development of low-thrust liquid-propellant rocket engines using computer technologies are presented. The structure is proposed basis characteristic features engines, including purpose, fuel components, physical principles organizing work process etc. presence electronic versions schematic diagrams, configuration and main achieved characteristics in database will make it possible choose effective design solutions at stage new products. In future these lead required parameters being developed. description engine used allows assessing capabilities engineering solution design, as well tracing trends a particular direction propulsion. peculiarity created that, parallel with information about their components accessories accumulating, which can also be developments. Given growing volume some forms communications presented that quickly find information, but requires certain ordering already initial stages.