A 2.5-THz receiver front end for spaceborne applications

The OH radical is an important player in known ozone depletion cycles; howe ver, due to its location in the atmosphere, it must be studied from either a balloon or spaceborne platform. For long-term mapping over large portions of the earth, a spaceborne platform is the most desirable. NASA's Earth Ob serving System Microwave Limb Sounder instrument is slated to house a 2.5-T Hz Schottky-diode receiver for such measurements. In this paper, we describ e the design, fabrication, and testing of the receiver front end. Measured double-sideband (DSB) receiver noise temperatures of better than 9000 K are reproducibly achieved with all devices of our best design. Estimated mixer noise is 3500-K DSB for optimal bias conditions and at room temperature. S elected components will be used in the first terahertz heterodyne receiver to be flown in space.