CubeRRT: CubeSat Radiometer Radio Frequency Interference Technology Validation

Metadata Updated: July 17, 2020

We propose the CubeSat Radiometer Radio Frequency Interference (RFI) Technology Validation (CubeRRT) mission to demonstrate wideband RFI mitigating backend technologies vital for future space-borne microwave radiometers. Recent passive microwave measurements below 40 GHz have shown an increase in the amount of man-made interference, corrupting geophysical retrievals in a variety of crucial science products, including soil moisture, atmospheric water vapor, sea surface temperature, sea surface winds, and many others. Spectrum for commercial use is becoming increasingly crowded, accelerating demand to open the bands reserved for passive microwave Earth observation and radio astronomy applications to general use. Due to current shared spectrum allocations, microwave radiometers must co-exist with terrestrial RFI sources. For example, the GPM Microwave Imager currently in orbit is impacted by RFI from commercial systems over both land and sea. As these sources expand over larger areas and occupy additional spectrum, it will be increasingly difficult to perform radiometry without an RFI mitigation capability. Co-existence in some cases should be possible provided that a subsystem for mitigation of RFI is included in future systems. Successful RFI mitigation will not only open the possibility of microwave radiometry in any RFI intensive environment, but will also allow future systems to operate over a larger bandwidth resulting in lower measurement noise. This crucial technology is required for the US to maintain a national capability for spaceborne microwave radiometry.

Initial progress in RFI mitigation technologies for microwave radiometry has been achieved in the SMAP mission, which is currently operating in space a digital subsystem for this purpose in a 24 MHz bandwidth centered in the protected 1413 MHz band. RFI subsystems for higher frequency microwave radiometry over the range 6-40 GHz however require a larger bandwidth, so that the capabilities of RFI mitigation backends in terms of bandwidth and processing power must also increase. To date, no such wideband subsystem has been demonstrated in space for radiometers operating above 1413 MHz.

The enabling technology is a digital Field-Programmable Gate Array-based spectrometer with a bandwidth of 1 GHz or more and capable of implementing advanced RFI mitigation algorithms such as the kurtosis and cross-frequency methods. This technology has a strong ESTO heritage, with the algorithms developed and demonstrated via the Instrument Incubator Program (IIP) and wideband backends developed under other ESTO support. The digital backend is currently at TRL 5, having been successfully tested in an RFI environment, and can be ported easily to a flight-ready firmware. Though the technology can be demonstrated for any frequency band from 1 to 40GHz, we will integrate the backend with a wideband radiometer operating over a 1 GHz bandwidth tunable from 6-40 GHz to demonstrate RFI detection and mitigation in important microwave radiometry bands. Along with a wideband dual-helical antenna, the payload will be integrated with a 6U CubeSat to demonstrate operation of the backend at TRL 7. The payload is expected to operate at a minimum duty-cycle of 25% to be compatible with spacecraft power capacity. Although the spatial resolution to be achieved will be coarse (due to the limited antenna size possible), the goal of demonstrating observation, detection, and mitigation of RFI is achievable in this configuration.

The proposed demonstration will act as an immediate risk reduction of new technologies that are necessary for future Earth science missions. The technology will allow newly enabled measurements by operating in previously untenable spectral regions over larger bandwidths. The benefits from the above technology are directly relevant to all future microwave Earth science missions, such as SCLP, GMI follow on, SMAP follow on, and others.

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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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Dates

Metadata Created Date February 28, 2019
Metadata Updated Date July 17, 2020

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date February 28, 2019
Metadata Updated Date July 17, 2020
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_40865
Maintainer
TECHPORT SUPPORT
Maintainer Email
Public Access Level public
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
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Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2018-12-01
Homepage URL https://techport.nasa.gov/view/40865
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash a115fc2cbf87a16f9ca26d6d6eea279e068099d6
Source Schema Version 1.1

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