An Enhanced Modular Terminal Descent Sensor for Landing on Planetary Bodies, Phase I

Metadata Updated: February 28, 2019

Remote Sensing Solutions (RSS) proposes to fill a critical niche in Entry, Descent, and Landing with the design and subsequent development of a terrain relative radar altimeter/velocimeter in support of missions to planetary bodies. This sensor, similar to that of the successful Mars Science Laboratory's Terminal Descent Sensor (MSL-TDS) will 1) expand the range of operation over that of the MSL-TDS and 2) mitigate identified risks due to dust and anomalously low backscatter areas. We will achieve this in part by establishing a Ku-band TDS design. In Phase 1 we will explore compact multi-beam shared aperture antenna designs and system trades to minimize antenna aperture size. In addition, the design approach for the system back-end electronics will be modular, compact, reproducible, and highly versatile. Utilizing RSS' novel, modular reconfigurable digital subsystem will enable us to produce reconfigurable architectures and pulse-timing/geometry. Such a solution is independent of the eventual transmit frequency of operation. As such, Ka-band or even W-band sensors could be produced based on this design for landing scenarios where velocity accuracy or size is a premium, and dust or airborne particulates are not a concern. The Phase 1 will establish a design that not only meets the stated MSL-TDS requirements but exceeds them in terms of sensitivity and range of altitudes of operation. We will simulate the sensor capability over the full range of altitude, velocity, and backscatter ranges. A path for demonstration and space-qualification of critical subsystems and components will be evaluated. At the termination of the Phase 1 we will have a design with of the Ku-band TDS, recommendations for a prototype in the Phase 2, a system weight and power estimate and a path-to-space.

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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 August 1, 2018
Metadata Updated Date February 28, 2019

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Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date February 28, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_93370
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 9e3cd0fa-548a-41bc-a051-3f3a077dce04
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2017-12-01
Homepage URL https://techport.nasa.gov/view/93370
License http://www.usa.gov/publicdomain/label/1.0/
Data Last Modified 2018-07-19
Program Code 026:027
Source Datajson Identifier True
Source Hash e6b5ebdf52776d1e6382ee1cb25930ff7801c69b
Source Schema Version 1.1

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