NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
HelioSwarm: Swarm Mission Design in High Altitude Orbit for HeliophysicsResolving the complex three-dimensional turbulent structures that characterize the solar wind requires contemporaneous spatially and temporally distributed measurements. HelioSwarm is a mission concept that will deploy multiple, co-orbiting satellites to use the solar wind as a natural laboratory for understanding the fundamental, universal process of plasma turbulence. The HelioSwarm transfer trajectory and science orbit use a lunar gravity assist to deliver the ESPA-class nodes attached to a large data transfer hub to a P/2 lunar resonant orbit. Once deployed in the science orbit, the free-flying, propulsive nodes use simple Cartesian relative motion patterns to establish baseline separations both along and across the solar wind flow direction.
Document ID
20190029109
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Plice, Laura
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
Dono, Andres
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
West, Stephen
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
Date Acquired
August 16, 2019
Publication Date
August 14, 2019
Subject Category
Solar Physics
Report/Patent Number
ARC-E-DAA-TN72306
Report Number: ARC-E-DAA-TN72306
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Portland, ME
Country: United States
Start Date: August 11, 2019
End Date: August 15, 2019
Sponsors: American Astronautical Society (AAS-HQ)
Funding Number(s)
CONTRACT_GRANT: NNA13AC87C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
lunar resonant orbit
heliophysics
No Preview Available