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Telemetry antennas withstanding very high accelerations and centrifugal forces

Published online by Cambridge University Press:  07 June 2021

Loïc Bernard*
Affiliation:
ISL, French-German Research Institute of Saint-Louis, F-68300 Saint-Louis, France
Hrvoje Covic
Affiliation:
ISL, French-German Research Institute of Saint-Louis, F-68300 Saint-Louis, France
Andreas Zeiner
Affiliation:
ISL, French-German Research Institute of Saint-Louis, F-68300 Saint-Louis, France
Armin Schneider
Affiliation:
ISL, French-German Research Institute of Saint-Louis, F-68300 Saint-Louis, France
*
Author for correspondence: Loïc Bernard, E-mail: loic.bernard@isl.eu

Abstract

We present the design steps of a coaxial dipole antenna for telemetry applications under extreme conditions of accelerations and centrifugal forces. Both, electromagnetic and mechanical designs are explained, as well as performance compromises that have to be made between both domains. The experimental results are given in the following part of the article, before some details on the instrumented firings and the receiving station; at last a few examples of projectiles equipped with such antennas are presented.

Type
EuCAP 2020
Copyright
Copyright © The Author(s), 2021. Published by Cambridge University Press in association with the European Microwave Association

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References

Kingey, MK (1959) Preliminary development of telemetry for aeroballistic ranges. Arnold Engineering Development Center, Report TN-59-7, Feb.Google Scholar
Bernard, L, Adam, R, Schmoltzi, D, Thomas, C, Kreitz, J and Schneider, A (2016) Instrumentation of the basic finner reference projectile for attitude measurements at supersonic velocities. IEEE Aerospace and Electronic Systems Magazine 31, 3240.CrossRefGoogle Scholar
Barton, A (2015) 155-mm M795 Aerofuze test at the KOFA range, Yuma proving ground, Arizona, 19 May 2015. Technical Report ARMET-TR-16076.Google Scholar
Decrocq, C, Martinez, B, Albisser, M, Dobre, S, Gnemmi, P, Bailly, Y and Roy, J (2018) Aerodynamic prediction of a projectile fitted with fins. International Journal of Numerical Methods for Heat & Fluid Flow 28, 12181236.CrossRefGoogle Scholar
Bailey, AB (1939) Antenna system. US patent 2,184,729.Google Scholar
Georget, E, Abdeddaim, R and Sabouroux, P (2014) A quasi-universal method to measure the electromagnetic characteristics of usual materials in the microwave range. Comptes Rendus Physique Volume 15, 448457.CrossRefGoogle Scholar
Johnson, RC (1991) Designer Notes for Microwave Antennas. London, UK: Artech House.Google Scholar
Krcmar, J (2012) ‘IntBal 1.0’ includes STANAG 4367 “Thermodynamic Interior Ballistic Model with Global Parameters”.Google Scholar
Decrocq, C, Martinez, B, Juncker, J, Berner, C, Leopold, F, Bailly, Y and Roy, J-C (2016) Aerodynamic study for capability increase of a spin-stabilized projectile fitted with fins. In Proceedings of the 2016 Applied Aerodynamics Conference. Royal Aeronautical Society.Google Scholar
Albisser, M, Dobre, S, Decrocq, C, Saada, F, Martinez, B and Gnemmi, P (2017) Aerodynamic characterization of a newconcept of long range projectiles from freeflight data. In 30th ISB International Symposiumon Ballistics, Long Beach, CA.CrossRefGoogle Scholar