Our proposed Phase II program exploits the use of cryogenic variable conductance heat pipe (CVCHP) technology to provide temperature control for two demonstration systems, a 220 K active aperture radar antenna and a 35 K IR sensor, whose feasibility was established in Phase I. To capture the performance benefits of radar operating at these low temperatures, either in space or on the ground, the CVCHP offers improvements in temperature uniformity, lower power consumption and simplicity of operation not found with conventional single phase pumped loops. CVCHPs for 35 K IR sensors also offer attractive benefits of temperature stability, lower power consumption, installation flexibility and lower costs compared to the control provided by mechanical cryocoolers. The working and control fluids for the IR sensor application will be neon and helium, respectively. We have selected a modified monogroove heat pipe as our baseline CVCHP for both applications. This heat pipe provides maximum capacity, minimum fluid charge and the ability to provide flexible/bendable sections, as needed. Our objectives in Phase II are to design, fabricate and test demonstrate these two applications. We expect the results will confirm our Phase I findings and allow CVCHPs to be commercialized for these and other applications.