ANALYSIS AND COMPARISON OF LIQUID-PROPELLANT ROCKET ENGINES AND SOLID-PROPELLANT ROCKET MOTORS AS PROPULSION SYSTEMS FOR AERIAL ATTACK VEHICLES BASED ON THE EXAMPLE OF SOVIET AIR-TO-SURFACE MISSILES.

Author: Sheiko Zakhar, Oles Honchar Dnipro National University

Section: Engines and power plants of aircraft. Energy supply of spacecraft

Publication date: 19 April, 2025

DOI: HTTP://DOI.ORG/10.62717/2221-4550-2025-1-039

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