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NASA Technical Memorandum 83745
20 and 30 GHz MMIC Technology for FutureSpace Communication Antenna Systems
G. Anzic and D. J. ConnollyLewis Research CenterCleveland, Ohio
Prepared for theGallium Arsenide (GaAs) Integrated Circuits Symposiumsponsored by the Institute of Electrical and Electronics EngineersBoston, Massachusetts, October 23-25, 1985
NASA
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ERRATA
NASA Technical Memorandum 83745
20 and 30 GH? MMIC TECHNOLOGY FOR FUTURESPACE COMMUNICATION ANTENNA SYSTEMS
G. Anzlc and D. J. Connolly
Cover: The dates of the symposium should be October 23-25, 1984.
20 AND 30 GHz MMIC TECHNOLOGY FOR FUTURE SPACE COMMUNICATION ANTENNA SYSTEMS
G. Anzic and D. J. Connolly
National Aeronautics and Space AdministrationLewis Research CenterCleveland, Ohio 44135
ABSTRACT
The development of fully monolithic galliumarsenide (GaAs) receive and transmit modules isdescribed. These modules are slated for phasedarray antenna applications in future 30/20 GHzcommunications satellite systems. Performancegoals and various approaches to achieve them arebriefly described. The latest design and perform-ance results of components, submodules and modulesare presented.
INTRODUCTION
With the expanding utilization of existingfrequency and orbital slot resources, the futuregeneration of communications satellites is underincreasing pressure to maximize its operating ef-ficiency while minimizing cost. A major factor inachieving these goals has been identified as theimplementation of multiple scanning beam antennasystems on future communications spacecraft. TheAdvanced Communications Technology Satellite(ACTS) scheduled for launch in late 1980's, willbe the first satellite to employ scanning beamantenna technology in the 30/20 GHz bands. Futuresatellite communications systems are expected touse monolithic receive and transmit module tech-nology to better implement this function.
Gallium arsenide (GaAs) Monolithic MicrowaveIntegrated Circuits (MMIC) offer substantial per-formance advantages in the proposed frequencies ofinterest. Since entire microwave circuits can befabricated on a single chip, the resulting circuitis free of parasitics, losses and component valueuncertainties normally associated with wire bondsand other external interconnects.
NASA Lewis Research Center has a substantialongoing program to develop 20 GHz transmit and30 GHz receive modules for this application.
20 GHz TRANSMIT MODULE
The original transmit module concept is shownin Fig. 1. Although the stated module size andthe power output have been modified, the designapproach shown still applies. The module performstwo distinctly different functions necessary forphased array antenna application. These are phaseand amplitude control of the radiated rf energy.Proper phase control of radiating elements results
in beam steering while amplitude control of selec-ted radiators defines the beam shape. A basicconcept employing MMIC transmit modules in a mul-tiple scanned beam spaceborne antenna applicationis shown in Fig. 2. Similarly, the receive mod-ules (described later in this report), operatingat different frequencies, can be incorporatedinto the same feed array by use of prthomodetransducers. Since a typical feed array willcontain hundreds of radiators, both phase andamplitude will be controlled by a computer withcapability to adapt to changing beam size andscan requirements.
The phase shifting and the variable powerfunctions of the transmit module are being devel-oped as two separate chips by two separate manu-facturers. The phase shifter chip is beingdeveloped by Rockwell International while TexasInstruments is developing the variable poweramplifier.
VARIABLE POWER AMPLIFIER MODULE
The performance goals of the variable poweramplifier are as follows:
rf bandrf power outGainEfficiencyAmplitude controlMechanical design
17.7 to 20.2 GHz0 to 0.5 W (variable)20 dB max. (variable)15 percent/6 percentOperate on digital inputFully Monolithic
While exhibiting high efficiency, the ampli-tude control provides for five output power statesat levels of 500, 125, 50, and 12.4 mW and off.The amplitude control is digital and TTL compat-ible. The 4 bit D/A converter has been designed,fabricated, and tested.
The variable power amplifier module develop-ment approach uses four stages of amplification,with dual gate FET's. A preliminary four stagesingle-gate amplifier module achieved an outputpower of 630 mW with 25-dB gain and 21-percentpower added efficiency at 18 GHz. The four stagedual-gate FET amplifier (fig. 3) is still in de-velopment. So far it has demonstrated a 250-mWoutput power with 15-dB gain at 19 GHz.
PHASE SHIFTER MODULE
The phase shifter module performance goalsare as follows:
rf bandrf power outGainEfficiencyPhase controlMechanical design
17.7 to 20.2 GHz>200 mW716 dB>15 percentOperate on digitalFully Monolithic
input
Figure 4 shows the fabricated version of the phaseshifter module. The module consists of five cas-caded single bit phase shifters each employing aswitched line approach using FET devices forswitches. The digital control circuitry acceptsa TTL input signal and provides the signals toswitch in or out each of the five phase shifters.A two stage buffer amplifier follows the phaseshifters to compensate for their insertion losses.Finally, a three stage power amplifier providesthe required output power.
A saturated output power of approximately+21 dBm was measured across the band of interest.The phase shifters operated well although theinsertion loss per bit was approximately 3.5 dB,which is about 1 dB above the goal.
Initial investigation of the phased arrayantenna design disclosed that more efficientantenna operation can be realized by dividing thephase shifter module in two submodules where phaseshifting and amplitude control are accomplishedat two different physical locations.
20 GHz HIGH POWER AMPLIFIER MODULE
In a related effort, Texas Instruments isdeveloping a monolithic amplifier which exhibitshigher power. The objectives of this effort areas follows:
Efficiencyrf bandrf power outGain
20 percent (Sat)19-21 GHz2.5 W (Sat), 1.5 W (Lin)>15 dB
With the effort under way for approximatelyone year, the following results have beenachieved:
(1) An output power of 2 W with 12 dB gainand 20 percent power added efficiency has beenachieved for the 3 stage amplifier. The lineargain was 14 dB at 1 W output at 17 GHz.
(2) A four-way monolithically combinedtravelling-wave amplifier has achieved an outputpower of 2 W at 7 to 8 percent efficiency (notoptimized).
(3) A travelling wave amplifier has achievedstate of the art results of 0.5 W output powerover 2 to 21 GHz frequency range with average gainof 4 dB and 14 percent power added efficiency.
30 GHz RECEIVE MODULE
The 30 GHz monolithic receive module is beingdeveloped by two contractors as a parallel effort.The two contractors are Hughes-Torrance ResearchCenter and Honeywell-Corporate Technology Center.The module's performance goals are as follows:
rf bandif center frequencyNoise figure at
room temperaturerf/if gain
Gain control
Phase control
Module powerconsumption
Phase and gaincontrol
Mechanical design
27.5 to 30 GHzBetween 4 to 8 GHz£5 dB
^30 dB at highest level ofgain control
At least six levels; 30, 27,24, 20, 17 dB andoOff
5 bits; each bit ±3° bandcenter
250 mW in all states exceptOFF. In OFF state, 25 mW
Operate on digital input.
Fully monolithic
The receive module consists of the followingfour basic submodules: Low noise amplifier, phaseshifter, gain control and mixer/IF. The approximatemodule layout is represented by Fig. 5. The dimen-sions shown are preliminary. The final module dimen-sions are expected to be smaller. Basically, thedesign approaches of both contractors are similar withsome minor differences. Both contractors have com-pleted approximately 2 years of the scheduled 4 yeareffort.
Figure 6 shows the Hughes low noise amplifiersubmodule. It's gain and noise figure are expectedto be approximately 11.5 dB and 4.5 dB respectively.Significantly better results are expected in the FETgain and noise performance area in the future.
Honeywell's initial submodule, a 3 bit phaseshifter, is shown in Fig. 7. Its measured performanceshowing the various possible phase states across theband of interest is shown in Fig. 8. A slight phasedisturbance just above 28 GHz is due to instrumen-tation and not the phase shifter itself. The finalphase shifter performance goal requires that it oper-ate at five different phase states. The phase shifterdesign approach is based on switched transmissionlines where large gate periphery FET's are used as rfswitches.
The remaining submodules are in various stages'ofdevelopment.
CONCLUDING REMARKS
A brief overview of the development of the mono-lithic microwave integrated circuit receive andtransmit modules has been presented. NASA Lewis ispursuing those MMIC developments that promise maximumsystem impact in areas of efficiency, weight and cost.Initial results indicate that the major goals of the20 and 30 GHz MMIC module contracts are likely to bemet.
5 BIT PHASE SHIFTER 1 WATT VARIABLE POWER AMPLIFIER
PHASE CONTROL LOGIC
BIT NO. 5180°
RFINPUT
INPUTBUFFERSTAGE
BIT NO.111.25°
BUFFERSTAGE
BIT N0.345°
BIT NO. 222.5°
POWER CONTROL LOGIC
DRIVERSTAGE
0.1 WATTDG FET
J_L
y« WATTDQFET
V. WATTDUAL QATE (DG|
FET
0.1 WATTDC FET
V4 WATTDG FET
0.1 WATTDG FET
'/< WATTDGFET
POWERSPLITTER
0.1 WATTDG FET
'/4 WATTDG FET
POWERCOMBINER
Figure 1. - 20 GHz GaAs monolithic transmit module.
20 GHz MONOLITHICTRANSMIT MODULE
SCANNING SPOTBEAM
ANTENNA
SCANNING SPOTBEAM MMIC FEED
SYSTEM A
Figure 2. - Multiple scanning spot beam antenna.
4.8 mm X 6.4 mm X 0.127 mm C'84'1139
Figure 4. - 20 GHz monolithic phase shifter module.
RFIN
DCINB "REF. IN
Figure 5. - 30 GHz monolithic receive module.
94mm
Figure 6. - 27.5 -30 GHz monolithic low noise amplifier.
Figure 7. - Three bit 30 GHz phase shifter.
<Q-
0
45
90
135
180
215270
315
27.5 21.1 21.7FREQUENCY, GHz
29.3 30.0
Figure 8. - Insertion phase for 3-bit phase shifter.
1. Report No.
NASA TM-83745
2. Government Accession No. 3. Recipient's Catalog No.
4. Title and Subtitle 5. Report Date
20 and 30 GHz MMIC Technology for Future SpaceCommunication Antenna Systems 6. Performing Organization Code
506-58-227. Author(s)
G. Anzic and D. J. Connolly
8. Performing Organization Report No.
E-222710. Work Unit No.
9. Performing Organization Name and Address
National Aeronautics and Space AdministrationLewis Research CenterCleveland, Ohio 44135
11. Contract or Grant No.
12. Sponsoring Agency Name and Address
National Aeronautics and Space AdministrationWashington, D. C. 20546
13. Type of Report and Period Covered
Technical Memorandum
14. Sponsoring Agency Code
15. Supplementary Notes
Prepared for the Gallium Arsenide (GaAs) Integrated Circuits Symposium sponsoredby the Institute of Electrical and Electronics Engineers, Boston, Massachusetts,October 23-25, 1984.
16. Abstract
The development of fully monolithic gallium arsenide (GaAs) receive and transmitmodules is described. These modules are slated for phased array antenna applica-tions in future 30/20 gigahertz communications satellite systems. Performance goalsand various approaches to achieve them are briefly described. The latest designand performance results of components, submodules and modules are presented.
17. Key Words (Suggested by Authors))
Monoli thi c ci rcui ts; Receive/transmi tmodules; GaAs FET amplifiers; Low noiseamplifiers; 30/20 GHz communicationstechnology; Phased arrays
18. Distribution Statement
Unclassified - unlimitedSTAR Category 32
19. Security Classif. (of this report)
Unclassified20. Security Classif. (of this page)
Unclassified21. No. of pages 22. Price'
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