Frequency agile heterodyne detector for submillimeter spectroscopy of planets and comets

Metadata Updated: February 28, 2019

The primary objective of this proposal is the development of a planetary THz heterodyne sensor for molecular line spectroscopy in space, based on transitions between quantum states in semiconductor quantum wells, and that can operate at physical temperatures of 50 K to 70 K. This would be a major advance for deep-space planetary and cometary missions. To date, all other THz heterodyne mixers (usually developed, for astrophysics applications) have utilized superconducting materials, and thus required cryogens or a mechanical cooler for operation near 4 K. Such systems cannot be flown for an extended period of time or require substantial cooling power and are unsuitable for planetary missions. State-of-the-art (SOA) heterodyne receiver technology intended for planetary instruments is based on Schottky-diodes operating at ambient temperature, typically below 1 THz. The only submillimeter heterodyne instrument that has flown to another planetary body is the Microwave Instrument for the Rosetta Orbiter (MIRO). MIRO has performed spectacularly on the cometary mission having determined the abundances of major gases, the surface outgassing rate and the nucleus subsurface temperature. However, it is based on decades-old mixer technology and its operating range was limited to two bands: 190 GHz (189-192) and 562 GHz (548-581), with high noise temperature ~ 8,000 K single-side band (SSB) in the 562 GHz band. The proposed Tunable Antenna-Coupled Intersubband Terahertz (TACIT) mixer will be a big leap forward for planetary science in the wide THz range, which is rich with many spectral lines. Besides the much greater number of gaseous species becoming accessible, a TACIT-based receiver will enable the study of winds with sufficient velocity resolution and permit high-sensitivity thermal imaging of surfaces. TACIT mixer absorbs THz radiation power resonantly, via a transition of electrons from the lower energy subband to the higher energy subband in a quantum well (QW) engineered AlGaAs/GaAs based material. Electric gates control the energy separation between subbands and thus provide the possibility to tune the mixer[HTML_REMOVED]s frequency. After the radiation is absorbed the detector operates as a hot-electron bolometer (HEB). That is, the radiation power heats the electron gas and a large bolometric response is observed since the resistance has strong temperature dependence. This mixer will have several revolutionary technological advantages including: [HTML_REMOVED] low noise temperature (~ 2,000 K [SSB]); [HTML_REMOVED] low required local oscillator power (~ 20 microwatts); [HTML_REMOVED] operating temperature obtainable with passive radiative cooling in space (50-70 K); [HTML_REMOVED] very broad frequency range (1-5 THz) tunable electrically. Beside the spectral coverage, the [HTML_REMOVED]breakthrough[HTML_REMOVED] TACIT mixer will: [HTML_REMOVED] enable sensitive array receivers thus tremendously increasing the volume of data returned over the life time of a mission; [HTML_REMOVED] be frequency re-programmable in flight so it can address questions or conditions not anticipated pre-launch. A TACIT-based THz spectroscopic receiver can be used on a number of the missions mentioned in the [HTML_REMOVED]Vision and Voyages for Planetary Science in the Decade 2013-2022.[HTML_REMOVED] It is relevant to the numerous mission concepts, e.g., NASA[HTML_REMOVED]s Europa mission, Journey to Enceladus and Titan, Enceladus Explorer, VESPER (Venus), Martian Water Dynamics, Comet Explorer, Jupiter Icy Moons Explorer, Titan-Saturn System, Jupiter-Europa Orbiter, etc. In the proposed 3-year task we will optimize the material processing and the embedded THz antenna circuit, and will demonstrate a fully operational laboratory receiver. At entry, the TRL = 2, at the exit TRL = 4. The TACIT development effort is collaboration between the Jet Propulsion Laboratory and University of California Santa Barbara with contributions from Princeton University and LongWave Photonics LLC. This work builds on a recent 1-year PIDDP funded effort in 2013.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Metadata Created Date February 28, 2019
Metadata Updated Date February 28, 2019

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Harvested from NASA Data.json

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Resource Type Dataset
Metadata Created Date February 28, 2019
Metadata Updated Date February 28, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_24879
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
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Harvest Object Id 90141c7c-7ebb-4011-b408-143bfec8ec2b
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2018-04-01
Homepage URL https://techport.nasa.gov/view/24879
License http://www.usa.gov/publicdomain/label/1.0/
Data Last Modified 2018-09-07
Program Code 026:027
Source Datajson Identifier True
Source Hash 1fb1657467184ae8004e5b9dc10fc748971f9ae0
Source Schema Version 1.1

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