ECHO

Satellite Communications Glossary

Satellite Communications — Echo

 

 

 

 

 

 

Argos Home

 

 
 


Information on Echo

On 12 August 1960, in conjunction with Bell Telephone Laboratories and the Jet Propulsion Laboratory, NASA launched a passive reflector, Echo I: a 30-m plastic balloon (weighing 61.2 kg) with an aluminium coating. The balloon had 82 panels that were folded before launch and inflated in orbit. A second satellite, Echo II, was launched on 25 January 1964 but inflated too rapidly and the balloon exploded.
     Echo was used principally for FM voice, facsimile and data transmission, but was also used on 19 August 1960 to test picture transmission. Although a passive reflector, Echo contained two tracking beacons transmitting with a power of 10 mW at a frequency of 107.9 MHz.
     Although Echo was simple and reliable, it was severely limited by being a passive reflector—despite the sphere having a reflectivity of 98%, Earth stations required extremely high-power transmitters (approximately 10 kW). Even with these high powers, useable receive powers were only possible because the satellite operated at a low height of 1 500 km. At that height, however, the periods of rotation were very small (118.3 minutes) so that the satellite was only accessible to ground stations for a short time.


Other topics in our resources on Satellite Communications related to Echo include: 
 
  • Satellite Receiver
  • SCORE
  • Relay I
  • Satellite system
  • Communications Moon Relay I (CMR)
  • Sputnik
  • Explorer I
  • Arab Satellite Communications Organisation (ARABSAT)
  • Syncom
  • Asia Cellular Satellite (ACeS)
  • Orbcomm
  • Ellipso
  • Telstar
  • Courier
  • Comsat
  • Intelsat
  •  

    Please contact Argos Press if you would like to propose related words or phrases for this glossary. © Argos Press Pty Ltd, Canberra, 2003-2004. All rights reserved. Please contact Argos Press Pty Ltd to seek permission to broadcast, adapt, reproduce and communicate our content (such as this entry on Echo).