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Deep Space Network Capabilities for Receiving Weak Probe SignalsPlanetary probes can encounter mission scenarios where communication is not favorable during critical maneuvers or emergencies. Launch, initial acquisition, landing, trajectory corrections, safing. Communication challenges due to sub-optimum antenna pointing or transmitted power, amplitude/frequency dynamics, etc. Prevent lock-up on signal and extraction of telemetry. Examples: loss of Mars Observer, nutation of Ulysses, Galileo antenna, Mars Pathfinder and Mars Exploration Rovers Entry, Descent, and Landing, and the Cassini Saturn Orbit Insertion. A Deep Space Network capability to handle such cases has been used successfully to receive signals to characterize the scenario. This paper will describe the capability and highlight the cases of the critical communications for the Mars rovers and Saturn Orbit Insertion and preparation radio tracking of the Huygens probe at (non-DSN) radio telescopes.
Document ID
20070014619
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Asmar, Sami
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Johnston, Doug
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Preston, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 2005
Publication Information
Publication: 2nd International Planetary Probe Workshop
Subject Category
Space Sciences (General)
Distribution Limits
Public
Copyright
Public Use Permitted.
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