An improvement in high altitude communication with a small, rocket-borne sonde can be achieved by transmitting circularly polarized waves. Signal losses due to cross polarization of linear antennas can be reduced. Measured radiation patterns for instrument mounted linear and several helical antennas are presented. Flight data are discussed.
Rocketsonde Transmission Link Characteristics
IEEE Transactions on Aerospace and Electronic Systems ; AES-6 , 6 ; 843-846
1970-11-01
720125 byte
Article (Journal)
Electronic Resource
English
Design of a Rocketsonde Launched UAS
AIAA | 2016
|Design of a Rocketsonde Launched UAS (AIAA 2016-3711)
British Library Conference Proceedings | 2016
|Stochastic network link transmission model
Elsevier | 2017
|Stochastic network link transmission model
Online Contents | 2017
|