Performance Evaluation for Launcher Testing Vehicle

Performance Evaluation for Launcher Testing Vehicle

The paper’s purpose is to present a calculus model for a testing vehicle that can be used to validate guidance, navigation and control systems for reusable launchers in all flight phases. The technical solution is based on a throttleable engine with thrust vectoring control and a reaction control sy...

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Bibliographic Details
Main Authors: Teodor-Viorel Chelaru, Valentin Pană, Costin Ene
Format: Article
Language:English
Published: MDPI AG 2022-09-01
Series:Aerospace
Subjects:
mathematical model
guidance navigation and control system
reaction control system
testing vehicle
reusable launcher
flight envelope
Online Access:https://www.mdpi.com/2226-4310/9/9/504

Internet

https://www.mdpi.com/2226-4310/9/9/504

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