Rapid Advanced Heliocentric Mission Design for L3, L4, L5, NEO Rendezvous, Capture, Sample Return Project

<p>Provide fast, new capability for Loose SmallSat Constellation with solar sail and impulsive propulsion to nonlinear heliocentric orbits, high inclination, low energy transfer (see tubes). These include orbits around L3, 4, 5, NEO rendezvous (e.g. Earth Trojans), capture, sample return &amp; for space weather monitoring.</p>

Data and Resources

Additional Info

Field Value
Maintainer Martin Lo
Last Updated April 1, 2025, 01:51 (UTC)
Created April 1, 2025, 01:51 (UTC)
accessLevel public
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harvest_source_title DNG Legacy Data
identifier TECHPORT_12168
issued 2012-10-01
landingPage http://techport.nasa.gov/view/12168
modified 2020-01-29
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publisher Space Technology Mission Directorate
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