System Design and Capabilities of a Current Technology, Low-Cost, Small Satellite

Ball Aerospace, with its successful background and strong interest in low-cost lightweight satellites, is studying the designs of current technology satellites for a variety of launchers (e.g., STS/GAS, Pershing, Scout, Poseidon, Conestoga, Titan 11, ILV, and Delta II). Ball Aerospace has completed the design of a current technology, multi-mission, low-cost Scout-compatible satellite. This paper summarizes the system design features and capabilities of this Ball Scout Satellite (BSS). The BSS is designed to accommodate a wide range of Earth and celestially oriented missions, both spinning and 3-axis stabilized. The BSS design provides a marked improvement in payload support capabilities (mass, power, data rate, pointing, interfaces, flexibility, reliability, etc.) than was previously available with earlier Scout satellites, and at a lower cost in current-year dollars.

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Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-09-15
DOI
https://doi.org/10.26077/h47r-wk81
Primary Topic
Spacecraft Design and Technology
Type
article
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article

System Design and Capabilities of a Current Technology, Low-Cost, Small Satellite

Donald Taylor, James R. Stuart
Digital Commons - USU (Utah State University)
Spacecraft Design and Technology
article

System Design and Capabilities of a Current Technology, Low-Cost, Small Satellite

Donald Taylor, James R. Stuart
article en

Abstract

Ball Aerospace, with its successful background and strong interest in low-cost lightweight satellites, is studying the designs of current technology satellites for a variety of launchers (e.g., STS/GAS, Pershing, Scout, Poseidon, Conestoga, Titan 11, ILV, and Delta II). Ball Aerospace has completed the design of a current technology, multi-mission, low-cost Scout-compatible satellite. This paper summarizes the system design features and capabilities of this Ball Scout Satellite (BSS). The BSS is designed to accommodate a wide range of Earth and celestially oriented missions, both spinning and 3-axis stabilized. The BSS design provides a marked improvement in payload support capabilities (mass, power, data rate, pointing, interfaces, flexibility, reliability, etc.) than was previously available with earlier Scout satellites, and at a lower cost in current-year dollars.

Digital Commons - USU (Utah State University)
Ball (United States) (US), Ball (France) (FR)
Spacecraft Design and Technology
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