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Near Earth Asteroid Scout - Mission UpdateAfter its deployment from NASA’s Space Launch System (SLS), the Near-Earth Asteroid (NEA) Scout mission will travel to and image an asteroid during a close flyby using an 86m^2 solar sail as its primary propulsion. Solar sails are large, mirror-like structures made of a lightweight material that reflects sunlight to propel the spacecraft. The continuous solar photon pressure provides thrust with no need for the heavy, expendable propellants used by conventional chemical and electric propulsion systems. Developed by NASA’s Marshall Space Flight Center (MSFC) and Jet Propulsion Laboratory (JPL), the NEA Scout is based on the industry-standard CubeSat form factor. The spacecraft measures 11 cm x 24 cm x 36 cm and weighs less than 14 kilograms. Following deployment from the Space Launch System (SLS), the solar sail will deploy, and the spacecraft will begin its 2.0 – 2.5-year journey. About one month before the asteroid flyby, NEA Scout will search for the target and start its Approach Phase using a combination of radio tracking and optical navigation and perform a relatively slow flyby (10-20 m/s) of the target. A summary of the mission, sailcraft, mission design, and its first several months of deep space operation will be described.
Document ID
20220008142
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Les Johnson
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Erin Betts
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Andrew Heaton
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Clif Jones
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Leslie McNutt
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Matt Pruitt
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Jim Stott
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Darren Wallace
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Rick Wilson
(ESSCA)
Julie Castillo-Rogez ORCID
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Gregory Lantoine
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Calina Seybold
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Ted Sweetser
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
May 24, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 36th Annual Small Satellite Conference
Location: Logan, UT
Country: US
Start Date: August 6, 2022
End Date: August 11, 2022
Sponsors: Utah State University
Funding Number(s)
PROJECT: EXPX22022D
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Near Earth Asteroid
solar sail
small spacecraft
CubeSat
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