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Title: General-Purpose Heat Source Development: safety test program. Postimpact evaluation, Design Iteration Test 5

Technical Report ·
DOI:https://doi.org/10.2172/6244144· OSTI ID:6244144

The General-Purpose Heat Source (GPHS) provides power for space missions by transmitting the heat of /sup 238/Pu decay to thermoelectric elements. Because of the inevitable return of certain aborted missions, the heat source must be designed and constructed to survive both re-entry and Earth impact. The Design Iteration Test (DIT) series is part of an ongoing impact test program. The fifth test (DIT-5) was designed to compare the impact response of a GPHS fueled clad that had been welded with a four-pole arc oscillator with the impact response of a clad welded with a two-pole oscillator. In DIT-5 a partial GPHS module containing two fueled clads (one welded with a four-pole oscillator and one welded with a two-pole oscillator) was impacted at 60.5 m/s and 930/sup 0/C. The fuel capsules were severely deformed by the impact; both clads breached. The capsule welded with a four-pole oscillator failed extensively. Neither failure was related to the welding technique. Postimpact analyses of the test components are described, with emphasis on microstructure and impact response.

Research Organization:
Los Alamos National Lab. (LANL), Los Alamos, NM (United States)
DOE Contract Number:
W-7405-ENG-36
OSTI ID:
6244144
Report Number(s):
LA-10232-SR; ON: DE85007392
Country of Publication:
United States
Language:
English