The CSF landing system for short takeoff and landing aircraft; report on proposed system which permits on-board determination of aircraft coordinates with respect to ground station; basic principles of system which must be both easy to control and precise; description of experimental design and of results obtained; possible future developments and summary of practical characteristics (weight, dimensions, reliability, etc).
Le systeme d'atterrissage CSF pour avions a decollage et atterrissage courts
Le systeme d'atterrissage CSF pour avions a decollage et atterrissage courts
Annales de Radioelectricite ; 22 , n 90
1967
11 pages
Article (Journal)
French
© Metadata Copyright Elsevier B. V. All rights reserved.
SYSTEME DE PROPULSION HYBRIDE POUR AERONEF A DECOLLAGE ET ATTERRISSAGE VERTICAUX
European Patent Office | 2020
|SYSTEME DE PROPULSION HYBRIDE POUR AERONEF A DECOLLAGE ET ATTERRISSAGE VERTICAUX
European Patent Office | 2024
|SYSTEME DE PROPULSION HYBRIDE POUR AERONEF A DECOLLAGE ET ATTERRISSAGE VERTICAUX
European Patent Office | 2020
|Système de propulsion hybride pour aéronef à décollage et atterrissage verticaux
European Patent Office | 2021
|