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U.S. Department of Energy
Office of Scientific and Technical Information

ASTR rod-drive replacement. Technical report, 1 October 1963-31 December 1964

Technical Report ·
OSTI ID:5146716
The 10-MW ASTR rod-drive mechanisms, originally designed for an airborne environment, were becoming difficult to repair because of high radiation levels and inability to procure direct-replacement spare parts. Failure of the original mechanism is attributed to (1) misalignment, (2) component failure, (3) water damage, and (4) radiation damage. With the reactor environment considerably different from that existing during the flight program, the mechanisms were no longer exposed to the g forces, extreme vibrations, and low temperatures for which they were designed. However, the mechanisms were required to function under varying depths of water of from 0 to 30 ft, under a core pressure of 75 psi, and at water temperatures of up to 185 F. Therefore, a program was initiated to develop a replacement-drive mechanism. This program involved prototype design and fabrication, testing, and installation and checkout on the ASTR. The new rod-drive mechanism basically is a 115-V, 60-cycle-powered rack and pinion type. The reactor operational checkout program resulted in several design changes being made in the mechanical interlock, shaft seals, electrical harness, and magnet-not-in-contact switch. These changes were incorporated in the nine mechanisms that were fabricated. The rod-drive mechanisms in their final configuration performed well throughout reactor operation.
Research Organization:
General Dynamics Corp., Fort Worth, TX (USA). Nuclear Aerospace Research Facility
OSTI ID:
5146716
Report Number(s):
AD-469554/0/XAB; FZK-226
Country of Publication:
United States
Language:
English