High Efficiency S-Band 20 Watt Amplifier

Metadata Updated: July 17, 2020

This project includes the design and build of a prototype 20 W, high efficiency, S-Band amplifier.[HTML_REMOVED][HTML_REMOVED] The design will incorporate the latest semiconductor technology, Gallium Nitride (GaN), which has superior thermal and efficiency performance over the traditional technology, Gallium Arsenide (GaAs).[HTML_REMOVED] Power consumption and tuning will be optimized for the NASA Space Network (SN) return link service.[HTML_REMOVED] This effort will significantly improve data rates on scientific balloons using the[HTML_REMOVED]SN, and enable the Wallops Flight Facility range to improve over the horizon service for range customers.The objective of this project is to develop a highly efficient, prototype S-band (2200 to 2290 MHz) amplifier capable of at least 20 watts of RF output power. [HTML_REMOVED]The final delivery for the project will be a flight ready prototype unit.[HTML_REMOVED] The primay target appliciation is[HTML_REMOVED]NASA scientific balloon missions.[HTML_REMOVED][HTML_REMOVED]20 W of[HTML_REMOVED]output power[HTML_REMOVED]is a four times increase[HTML_REMOVED]over the present communications system,[HTML_REMOVED]and results in[HTML_REMOVED]a four times increase in data throughput as well.[HTML_REMOVED] However, balloon craft[HTML_REMOVED]use solar power and have limited power budgets.[HTML_REMOVED] This requires a very efficient amplifier on the order of 40% in order to avoid flying additional solar panels.[HTML_REMOVED][HTML_REMOVED][HTML_REMOVED]This technology can also be incorporated into existing SN transmitters used for various Wallops range customers that may require over the horizon downlink capability.[HTML_REMOVED] The new design will alleviate existing parts obsolescence issues and improve power efficiency and thermal requirements.The goal is to design a single board amplifier module with a DC power conversion and associated enclosure.[HTML_REMOVED] The amplifier will be a 2 or 3 stage module centered around a high power GaN transistor used for the output stage.[HTML_REMOVED] [HTML_REMOVED]The[HTML_REMOVED]project includes part selection, part characterization, impedance matching for input, output, and inter-stage, and enclosure configuration.[HTML_REMOVED] [HTML_REMOVED]Output stage transistor selection will be driven by balancing output power and compression points.[HTML_REMOVED][HTML_REMOVED] Transistor efficiency improves significantly when output stage operation moves into the non-linear region.[HTML_REMOVED]GaN parts will be selected for the high power transistor and driver stage.[HTML_REMOVED][HTML_REMOVED] In the last 10 years, GaN has emerged as the technology of choice for all new RF/microwave designs, including satellite and communications electronics.[HTML_REMOVED] GaN high power density opens up a whole new arena to higher power applications.[HTML_REMOVED] For instance, GaAs has a power density of 1.5 W/mm while GaN is 5 to 12 W/mm.[HTML_REMOVED] GaN parts are also capable of delivering higher efficiencies.[HTML_REMOVED]Board layout will follow manufacture recommendations for best thermal performance.[HTML_REMOVED] This includes chip to board interface as well as board to enclosure mounting. To optimize overall module efficiency, a power conversion circuit will be designed to efficiently convert a typical unregulated flight system voltage to the regulated 28 volts and higher required for GaN transistor drain voltage.[HTML_REMOVED][HTML_REMOVED]

Access & Use Information

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.

Downloads & Resources


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_90777
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 31deffd4-71fd-474c-9707-d6b8b5a57712
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2017-09-01
Homepage URL https://techport.nasa.gov/view/90777
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash f39a275bd7222675e3566c98452c3307b2a747ca
Source Schema Version 1.1

Didn't find what you're looking for? Suggest a dataset here.