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EPS

retired
Admin Edit
Launched 9/26/1997
Technical Specifications
Verified technical details
Dry Mass
29950 kg
Total Mass
29950 kg
Power
Unknown
Design Life
Unknown
Stakeholders

Operator

NASA Marshall Space Flight Center

Manufacturer

NASA Marshall Space Flight Center
Launch Mission

Shuttle/Mir-7

9/26/1997

Entity Mentions
All verified mentions of this entity in source documents

C3S develops and manufactures 3U, 6U, 12U, and 16U CubeSat platforms and subsystems including OBC, EPS, and communication modules.

Mentioned as: EPSSourceMay 4, 2023

The Aphelion Primary Bus Module (PBM) is an integrated EPS and onboard computer solution designed for mission-critical, volume-constrained CubeSat environments and provides mass and volume savings.

Mentioned as: EPSSourceApr 20, 2023

Northrop Grumman developed the EPS-R program and provided the EPS emblem.

Mentioned as: EPSSourceMay 20, 2024

The U.S. Air Force awarded Northrop Grumman an $82,000,000 contract to develop a next-generation ground system to provide telemetry, cybersecurity, and control for EPS and EPS-R payloads.

Mentioned as: EPSSourceJul 3, 2019