The way a Proposed Deep Space Mission is designed should be linked to additional design parameters/ constraints such as the availability of the Deep Space Network to support communications. This paper explores this exact methodology by examining the launch opportunities of a simulated mission to Jupiter during a decade long timeframe.
Using available DSN tracking converage as a design parameter in mission proposals
12th AAS/AIAA Space Flight Mechanics Meeting
2002-01-27
Conference paper
No indication
English
Mars Together Mission: Proposals
British Library Conference Proceedings | 1995
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British Library Conference Proceedings | 1995
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