The data link for the Ames baseline probe as applied to the MJU spacecraft specifically with an entry at Uranus is analyzed. A frequency analysis, a trajectory analysis, and a discussion of the effects on the spacecraft design by the data link are presented. The possibilities of a two-way link are considered.
Data link relay design
1974-08-01
Conference paper
No indication
English
Link design and payload configuration concepts for the Data Relay Satellite
British Library Conference Proceedings | 1989
|Design and architecture of the relay link analysis tool
NTRS | 2002
|