Electric rocket engine

Description

The invention relates to the field of electric jet engines. To ensure reliable supply of solid fuel to the source of a plasma-forming substance during long-term operation of an electric rocket engine at low negative temperatures, the surface of a guide device for direct-flow movement of solid fuel in a source of plasma-forming substance from the side-by-side movement of solid fuel is coated with a glass-like film in the form of nanomaterial.

Детали

Usage

Template of the usage

Application area

Template of the application area

Development stage

Template of the development stage

Availability of patents

Template of the availability of patents

Financing from the federal budget

Template of the financing from the federal budget

Participation of foreign partners

Template of the participation of foreign partners

Authors

Template of authors