POLONIUM RADIOISOTOPE THERMOELECTRIC GENERATOR. PHASE I TECHNICAL CONCLUSIONS. PART II. [electronic resource]

Nesdps Office Of Nuclear Energy Space And Defense Power Systems; Systems For Nuclear Auxiliary Power (snap)/components For 400 W(e) Polonium-210-fueled, For Use In Space, Engineering Drawings For; Thermoelectric Generators/design Of 400 W(e) Polonium-210-fueled, For Use In Space, Engineering Drawing...

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Bibliographic Details

Online Access:	Online Access
Corporate Authors:	Martin Marietta Corporation (Researcher), U.S. Atomic Energy Commission. Division of Technical Information (Researcher)
Format:	Government Document Electronic eBook
Language:	English
Published:	Washington, D.C : Oak Ridge, Tenn. : United States. Dept. of Energy ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 1965.
Subjects:	Thermoelectric Generators. Space Flight. Design. Thermal Insulation. Capsules. Snap Batteries. Control Equipment. Space Vehicles. Polonium 210.