NASA-GSFC Nano-Satellite Technology Development

The scientific understanding of key physical processes between the Sun and Earth require simultaneous measurements from many vantage points in space. Nano-satellite technologies will enable a class of constellation missions for the NASA Space Science Sun-Earth Connections theme. These technologies will also be of great benefit to other NASA science enterprises. Each nano-satellite will weigh a maximum of 10 kg including the propellant mass. Provisions for orbital maneuvers as well as attitude control, multiple sensors and instruments, and full autonomy will yield a highly capable miniaturized satellite. All onboard electronics will survive a total radiation dose rate of 100 krads over a two year mission lifetime. Nano-satellites developed for in-situ measurements will be spin-stabilized, and carry a complement of particles and fields instruments. Nano-satellites developed for remote measurements will be three-axis-stabilized, and carry a complement of imaging and radio wave instruments. Autonomy both onboard the nano-satellites and at the ground stations will minimize the mission operational costs for tracking and managing a constellation. Partnerships with private industry and academic institutions will be utilized for the development, manufacturing, and testing of the nano-satellites. Key technologies under development will be described, which include: advanced, miniaturized chemical propulsion; miniaturized sensors; highly integrated, compact electronics; autonomous onboard and ground operations; miniaturized onboard methods of orbit determination; onboard RF communications capable of transmitting data to the ground from far distances; lightweight, efficient solar array panels; lightweight, high output battery cells; a miniaturized heat transport system; lightweight yet strong composite materials for the nano-satellite and deployer-ship structures; and simple, reusable ground systems.

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Publication Details

Journal
Transactions & studies of the College of Physicians of Philadelphia
Published
2025-08-08
DOI
https://doi.org/10.26077/csjq-j379
Citations
25
Primary Topic
Solar and Space Plasma Dynamics
Type
article
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article

NASA-GSFC Nano-Satellite Technology Development

Victor Sank, David J. Mangus, J.C. Kellogg, Peter Panetta et al.
25 citations
Transactions & studies of the College of Physicians of Philadelphia
Solar and Space Plasma Dynamics
article

NASA-GSFC Nano-Satellite Technology Development

Victor Sank, David J. Mangus, J.C. Kellogg, Peter Panetta, J. S. Gagosian, Harry Culver, Theodore Michalek, Steven Tompkins, Michael Johnson
article en
25 citations

Abstract

The scientific understanding of key physical processes between the Sun and Earth require simultaneous measurements from many vantage points in space. Nano-satellite technologies will enable a class of constellation missions for the NASA Space Science Sun-Earth Connections theme. These technologies will also be of great benefit to other NASA science enterprises. Each nano-satellite will weigh a maximum of 10 kg including the propellant mass. Provisions for orbital maneuvers as well as attitude control, multiple sensors and instruments, and full autonomy will yield a highly capable miniaturized satellite. All onboard electronics will survive a total radiation dose rate of 100 krads over a two year mission lifetime. Nano-satellites developed for in-situ measurements will be spin-stabilized, and carry a complement of particles and fields instruments. Nano-satellites developed for remote measurements will be three-axis-stabilized, and carry a complement of imaging and radio wave instruments. Autonomy both onboard the nano-satellites and at the ground stations will minimize the mission operational costs for tracking and managing a constellation. Partnerships with private industry and academic institutions will be utilized for the development, manufacturing, and testing of the nano-satellites. Key technologies under development will be described, which include: advanced, miniaturized chemical propulsion; miniaturized sensors; highly integrated, compact electronics; autonomous onboard and ground operations; miniaturized onboard methods of orbit determination; onboard RF communications capable of transmitting data to the ground from far distances; lightweight, efficient solar array panels; lightweight, high output battery cells; a miniaturized heat transport system; lightweight yet strong composite materials for the nano-satellite and deployer-ship structures; and simple, reusable ground systems.

Transactions & studies of the College of Physicians of PhiladelphiaVol. 37(2)
Goddard Space Flight Center (US)
Industry, innovation and infrastructure
Solar and Space Plasma Dynamics
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