Aerospace Laser-Propulsion Engine

descriptionPublicationkeyboard_double_arrow_right Part of book or chapter of book , Other literature type 01 Jan 2021 English Publisher:Springer International Publishing

Authors: Yuri A. Rezunkov;

doi: 10.1007/978-3-030-79693-8_4

Aerospace Laser-Propulsion Engine

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Abstract

Development of the airspace laser-propulsion engine operating both in RP and CW modes of thrust production is validated. The engine is considered as a basic unit for creation of HPLP. The aerospace laser device differs sufficiently as compared with other laser-propulsion engines by its design, and it consists of two principal units, namely, laser beam concentrator and jet nozzle. Such type of the device allows optimizing both units of the engine independently on other one, taking into account only laser beam parameters and gas-dynamic effects.

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