Engineering topics
Publications and source records attributed to Mason, C. C..
The dust coma of comet Hale-Bopp was observed in the themal infrared over a wide range in solar heating (R=4.9-0.9 AU) and over the full wavelength range from 3 mu to 160 mu.
To ensure good aerial photography, the effects that factors such as submergence depth, sun angle, film and filter type, exposure, aircraft altitude, and polarization have on the photographic resolution of an underwater object must be determined. Various subjects were photographed, such as the deck of a small submersible, colored and gray scale panels, and natural bottom features. No underwater resolution target was used.
Analysis of lunar particle size distribution data indicates that the surface material is composed of two populations. One population is caused by comminution from the impact of the larger-sized meteorites, while the other population is caused by the melting of fine material by the impact of smaller-sized meteorites. The results are referred to Mars, and it is shown that the Martian atmosphere would vaporize the smaller incoming meteorites and retard the incoming meteorites of intermediate and large size, causing comminution and stirring of the particulate layer. The combination of comminution and stirring would result in fine material being sorted out by the prevailing circulation of the Martian atmosphere and the material being transported to regions where it could be deposited. As a result, the Martian surface in regions of prevailing upward circulation is probably covered by either a rubble layer or by desert pavement; regions of prevailing downward circulation are probably covered by sand dunes.
Lunar surface erosion due to Apollo 11 descent engine
Module landing effects on lunar surface, deriving erosion law from Surveyor 5 engine firing test and vacuum test data
Gaussian particle size distribution with porosity and surface irregularity corrections used to determine mean particle size of lunar surface material at Surveyor sites
Interface tests for evaluating ability of pressure for subjects to perform lunar scientific tasks
Possible excursions for typical 35-hour lunar surface exploration, experimental and recording instruments, sample collection, and photography