Silicon-Germanium Front-End Electronics for Space-Based Radar Applications

Metadata Updated: July 17, 2020

Over the past two decades, Silicon-Germanium (SiGe) heterojunction bipolar transistor (HBT) technology has emerged as a strong platform for high-frequency applications. The high performance of SiGe and its compatibility with mature silicon fabrication processes allow for highly integrated mixed-signal systems for a relatively low cost. A lesser-known benefit of SiGe is its great potential for extreme environment electronics. Extreme environments are environments outside the realm of typical design specifications. The performance of electronics can drastically change in such environments. Space-borne synthetic aperture radars in orbit endure temperatures up to 120∞ C while facing the sun and down to -110∞ C during the night, the whole time being bombarded by intense radiation. Commercial radar systems on Earth are not exposed to these extreme environment conditions. Electronics in space are typically contained in temperature-controlled "warm boxes," which are bulky, expensive, and consume large amounts of power. Radar systems perform best when the front-end electronics are as close as possible to the antenna, and electronics that need to be contained in a warm box limit the capabilities of the radar. It would be beneficial from both a performance and a cost standpoint to have radar electronics that can function in space without the need for a warm box.

During my graduate studies, I plan to research SiGe front-end radar electronics for low-temperature and radiation-intensive environments like space. I will particularly focus on the design and operation of SiGe power amplifiers (PAs) in these environments. PAs are the critical elements in the transmit path of transmit/receive (T/R) modules, and their performance in extreme environments has only begun to be explored. In Year 1 I will characterize the performance of SiGe devices and power cells over temperature and calibrate compact models to fit the measured data. Some cryogenic measurement challenges will need to be overcome before these devices can be characterized. I will begin exploring the effects of prolonged radiation exposure on PA performance as well. Based on studies of other front-end circuit blocks, it is presumed that radiation will have little impact on PA performance. In Year 2 I will investigate the effects of DC biasing on the performance of PAs over temperature. Studies have shown that PA performance at a single bias point changes drastically with temperature. Adjusting the biasing with temperature may be the key to achieving temperature-invariant performance. I will continue studying the effects of radiation on PA performance, with a focus on single event upsets caused by individual heavy ion strikes. Also, I will characterize devices at mmWave frequencies and develop models so I can begin designing a mmWave PA. In Year 3 I will aim to design a PA with invariant performance from room temperature down to cryogenic temperatures. If radiation exposure significantly degrades PA performance, I will explore radiation hardening techniques for PAs. The mmWave PA will be designed in Year 3 as well. In Year 4 I will aim to design a temperature-invariant, radiation-hardened mmWave PA. I will investigate the design of a mmWave SiGe T/R module for these conditions as well. I will explore the integration of these electronics on the organic packaging material liquid crystal polymer (LCP) as well.

The front-end electronics developed from my research will increase the capabilities of space radar. This radar will enable high-resolution imaging of moons and other celestial bodies without the need for a warm box. An internship experience with NASA would give me a better top-to-bottom understanding of radar systems and would make me a better designer at both the circuit and the system levels.

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Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

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Metadata Created Date August 1, 2018
Metadata Updated Date July 17, 2020

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date July 17, 2020
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_4217
Maintainer Email
Public Access Level public
Bureau Code 026:00
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Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2015-08-01
Homepage URL
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash 30e0feac4375174d5de07db3ff8e8cfd5d7e055c
Source Schema Version 1.1

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