Digital Beamforming has gained significant importance in radar applications in the past years. It helps improve radar performance while reducing mass and power. Improving these figures becomes even more important for space applications. The Space Exploration Synthetic Aperture Radar (SESAR) is a novel P-band (70 cm wavelength) radar instrument developed for planetary applications that will enable surface and near-subsurface measurements of Solar System planetary bodies. The radar will measure full polarimetry at meter-scale resolution, and perform beam steering through programmable digital beamforming architecture. The data obtained with SESAR will provide key information on buried ice and water signatures that can facilitate the design of future human and robotic exploration missions. In this paper we describe SESAR’s large antenna array, the sub-systems integration process, and the different environmental testing activities performed to the overall system in order to raise the Technology Readiness Level (TRL) for its future inclusion in a space-proven system.
Superconducting Transition Edge Sensor (TES) bolometer arrays with thousands of pixels are essential for achieving the science objectives of future cold far-infrared astronomical telescopes. The readout of such large format TES arrays represents a significant challenge for these missions in terms of power consumption and thermal loading on the coldest cryogenic stages of the instruments. The Time Domain Multiplexing (TDM) technology is mature and has been implemented on many ground-based and air-borne instruments using TES arrays. Several concept studies such as Origins Space Telescope (OST [4]) or Mid-InfraRed Exo-planet CLimate Explorer (MIRECLE [5]) consider this technology and Time Domain Multiplexing as one of the possible baseline technologies for their instruments. In order to address the aforementioned challenges we propose a novel modular solution called Modular Adaptive Transition Edge Sensor Superconducting quantum interference device Electronics (MATESSE) that will serve as the necessary step towards an adaptation of the solution to a space-proven system.
The HIgh-Resolution Mid-infrarEd Spectrometer (HIRMES) is the 3rd Generation Instrument for the Stratospheric Observatory For Infrared Astronomy (SOFIA). The HIRMES cryostat is comprised of several cooling stages (300K, 65K, 4K, 800mK, 400mK, and 70mK), which are essential to achieve the required sensitivity on the mid-infrared waveband in which HIRMES observes (25 um-122um). The science application of the HIRMES instrument is the study of proto-planetary systems that contain water-vapor, water-ice, deuterated hydrogen, and neutral oxygen. In this paper, we discuss the use of a He3 stage coupled to an Adiabatic Demagnetization Refrigerator (ADR) stage in order to achieve the required temperature of 70mK on the Focal Plane Assembly (FPA). HIRMES' FPA contains two Transitioning Edge Sensor (TES) bolometric detector arrays that can provide a combination of four primary observing modes; High Resolution (R ~ 100,000), Mid-Resolution (R ~ 10,000), Low-Resolution (R ~ 600) spectroscopy, and Spectral Imaging (R ~ 2000).1 Moreover, we discuss the operations of the detector readout, in combination of a grating-dispersive spectroscopy mechanism, and a host of Fabry-Perot tunable narrow-band filters to achieve HIRMES' unmatched sensitivity in all four modes.
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