Advanced Radioisotope Thermoelectric Space Power System

650792

02/01/1965

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
A radioisotope thermoelectric generator (RTG) using curium-242 as fuel, developed as an alternate power supply, has been shown to be compatible with the Atlas-Centaur and Surveyor requirements. This power supply provides a relatively low weight and highly reliable system capable of producing 25 watts output under lunar conditions for a mission life of 120 days. The system is unique in that it utilizes a thermal control system that maintains a relatively constant thermal input to the energy conversion components.
Major program effort was focused on nuclear safety, thermoelectric generator development, converter development, and system qualification tests.
Meta TagsDetails
DOI
https://doi.org/10.4271/650792
Pages
4
Citation
Elias, D., and Gray, I., "Advanced Radioisotope Thermoelectric Space Power System," SAE Technical Paper 650792, 1965, https://doi.org/10.4271/650792.
Additional Details
Publisher
Published
Feb 1, 1965
Product Code
650792
Content Type
Technical Paper
Language
English