INITIAL NAVIGATION ANALYSIS FOR THE EUROPA MULTIPLE FLYBY MISSION CONCEPT

被引：0
|
作者：
Nandi, Sumita [1 ]
Kangas, Julie [1 ]
Valerino, Powtawche [1 ]
Buffington, Brent [2 ]
Ionasescu, Rodica [1 ]
Boone, Dylan [1 ]
机构：
[1] CALTECH, Jet Prop Lab, Mission Design & Nav Sect, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
[2] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
来源：
SPACEFLIGHT MECHANICS 2016, PTS I-IV | 2016年 / 158卷
关键词：
D O I：
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中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Earth and spacecraft-based observations of the Jovian moon Europa have identified it as the most plausible habitat for extraterrestrial life in our solar system. Recently, NASA has formed a Europa Mission Concept to potentially explore this icy world with a sophisticated instrument suite operating from a spacecraft in orbit about Jupiter. Candidate trajectories have been designed that would use the Jovian moons to repeatedly bring the spacecraft near Europa, providing multiple observation opportunities over the mission duration. This paper describes navigation analyses associated with these trajectories that are being assessed for their operational feasibility. The analysis includes determination of the AV requirements for the mission concept and notional spacecraft ephemeris knowledge capability.
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页码：3839 / 3848
页数：10
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