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Daye, C. J.

Publications and source records attributed to Daye, C. J..

Tank fragmentation test

A photographic study of a simulated tank fragmentation test was made. Sixteen disks and four spheres were ejected from a test article mounted in a vertical orientation 110 ft above a target installed on the test chamber floor. The test was performed at a chamber pressure of 25 microns. Velocities at impingement on the target ranged from 88 to 120 ft/sec; corresponding ejection velocities at the exit plane of the ejector assembly ranged from 29 to 87 ft/sec. Tumble axes of the disks were expected to be all in the north-south direction; the majority of those measured were, while some were skewed from this direction, the maximum observed being 90 deg. A typical measured tumble rate was 2.4 turns/sec. The dispersion pattern measured on the target was reasonably regular, and measured approximately 16 ft east-to-west by 11 ft north-to-south.

Daye, C. J.

Skylab payload shroud jettison tests

The separation concept of the skylab payload shroud is presented, and its behavior in three full-scale jettison tests in vacuum is described. The shroud petal arresting mechanism is explained, as well as the primary and secondary data acquisition systems. The first two tests demonstrated the need for some structural design modifications although the separation process was satisfactory in each test. The third test, incorporating these design modifications, was satisfactory in all aspects of shroud performance.

Daye, C. J.