Abstract
INL has evaluated and refurbished General Purpose Heat Source (GPHS) Radioisotope Thermoelectric Generator (RTG) Flight Unit 5 (GPHS-RTG F5R or F5R) that was defueled in 2005. The generator has passed all the INL internal reviews, an end item data package has been delivered to NASA and is ready fueling for a mission. NASA requested a user’s guide for F5R with enough detail for a prospective mission proposal. This report documents the development of the power prediction model used in the user’s guide. The prediction evaluated the thermoelectric “burn-in” and the graceful degradation modes of the missions and developed a thermal inventory dependent equation that predicts the power that matches Galileo, Cassini, and PNH within a three-standard deviation of ±1%. This prediction is only valid for the 30 VDC load voltage of these missions.
| Original language | English |
|---|---|
| State | Published - Apr 1 2026 |
| Event | Nuclear and Emerging Technology for Space 2025 - Dayton, United States Duration: Nov 10 2025 → Apr 30 2026 |
Conference
| Conference | Nuclear and Emerging Technology for Space 2025 |
|---|---|
| Country/Territory | United States |
| City | Dayton |
| Period | 11/10/25 → 04/30/26 |
INL Publication Number
- INL/CON-25-88991
- 208604
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