Miniature X-ray Source for Planetary Exploration Instruments, Phase II

The objective of the proposed work is to develop a rugged, low power, passively cooled X-Ray source that is compatible with miniaturized XRD systems. The XRD instruments would be used for in situ measurements on planetary surfaces. This X-ray source will integrate an X-ray emitting vacuum tube and both low and high-voltage power supplies into a compact and lightweight unit. This X-ray source will enable further miniaturized X-ray instruments to be deployed for surface and subsurface exploration of the solar system. The objectives will be achieved with an X-ray source that combines the advantage of easy thermal management and simple control electronics. The concept relies on the use of state-of-the-art ceramic materials that combines very good electrical insulation properties with good thermal conductivity. This source will allow using the grounded-cathode geometry for simple and compact electronics, and rely on the heat-sinking properties of the electrical insulator for heat dissipation to ground. The most promising material for this application is Aluminum Nitride (AlN). Objective specifications for the source to be developed are as follows: Accelerating Voltage (25 kV), Electron Beam Current (200 uAmps), X-ray Spot Size (50 microns), X-ray Tube Dimensions (65 mm x 25 mm,lxd)

This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

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