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Microwave & Space Electronics Components
A useful starting reference is Baljit Chandhoke’s Microwave Journal article RF Signal Chain and Components for Space-Based Satcom Applications, which organizes the RF transmitter and receiver around the same building blocks described here.
1. Core component map
| Component | Main job | Parameters you should recognize |
|---|---|---|
| LNA | amplify weak received signal with minimal added noise | NF, gain, $P_{1dB}$, IIP3, stability |
| PA / SSPA | create RF transmit power | $P_{sat}$, $P_{1dB}$, gain, PAE, linearity, thermal resistance |
| TWTA | very high RF/microwave power in space | output power, efficiency, gain, lifetime, EPC/high-voltage requirements |
| Driver amplifier | drive final PA/TWTA | gain, linearity, output level |
| Mixer | translate RF ↔ IF/baseband | conversion loss/gain, IIP3, isolation, LO drive, image response |
| Filter | select wanted spectrum / reject unwanted signals | insertion loss, rejection, bandwidth, Q, group delay |
| Diplexer / duplexer / multiplexer | separate/combine frequency bands | isolation, insertion loss, power handling, group delay |
| Switch | route RF paths | insertion loss, isolation, switching time, power handling |
| Circulator / isolator | route or absorb reverse power | insertion loss, isolation, VSWR, power |
| Limiter | protect receiver from large signals | limiting threshold, leakage, recovery, power handling |
| Attenuator / DSA | control signal level | attenuation range, step size, phase variation, linearity |
| Phase shifter | control RF phase | phase range, resolution, insertion loss, RMS error |
| Beamformer IC | amplitude/phase control for arrays | channels, gain/phase resolution, NF, linearity, power |
| Power divider / combiner | split/combine RF power | loss, isolation, amplitude/phase balance |
| Directional coupler | sample forward/reverse power | coupling, directivity, insertion loss |
| Hybrid coupler | equal split with defined phase | amplitude balance, phase balance, isolation |
| VCO / oscillator | create RF reference | tuning range, phase noise, pushing/pulling |
| PLL / synthesizer | lock/tune RF frequency | phase noise, spurs, lock time, step size |
| OCXO / TCXO / CSAC | stable frequency/time reference | stability, aging, radiation tolerance, phase noise |
| Frequency multiplier/divider | generate related frequencies | conversion loss/gain, phase noise multiplication |
| Detector / log detector | measure RF power/amplitude | dynamic range, response time, accuracy |
| ADC / DAC | RF/IF ↔ digital conversion | sample rate, ENOB, SFDR, jitter, power |
| FPGA / ASIC / RFSoC | digital modem, beamforming, control | throughput, interfaces, radiation strategy |
| Waveguide / coax / connector | carry microwave energy | loss, power, mode, VSWR, multipaction margin |
| Antenna feed / OMT / polarizer | couple RF into desired polarization/mode | isolation, axial ratio, return loss, bandwidth |
| DC-DC / LDO / POL regulator | power the RF electronics | efficiency, ripple, PSRR, radiation, EMI |
| Transponder | integrated receive/command/track/transmit function | coherent/noncoherent operation, turnaround ratio, bands, ranging |
| Modem | modulation, coding, framing | data rate, coding gain, EVM, latency |
2. Low-noise amplifier (LNA)
The LNA is usually the first active device in a receiver.
Its job is to provide gain before noisier downstream components.
For a cascade,
\[F_{total} = F_1+ \frac{F_2-1}{G_1} + \frac{F_3-1}{G_1G_2} +\cdots.\]Thus first-stage LNA noise figure and gain strongly determine receiver sensitivity.
Important specifications
- noise figure (NF);
- gain;
- gain flatness;
- input/output return loss;
- $P_{1dB}$;
- IIP3/OIP3;
- stability factor;
- DC power;
- radiation and temperature behavior for space.
Microwave Journal emphasizes LNA noise figure as one of the defining receiver parameters in its space satcom signal-chain article.
3. Power amplifier (PA) and SSPA
The PA creates the final RF output power.
Typical semiconductor technologies include
- GaAs;
- GaN;
- silicon LDMOS at lower microwave bands;
- integrated MMIC architectures.
Key quantities include
\[PAE = \frac{P_{RF,out}-P_{RF,in}}{P_{DC}}.\]and
\[P_{1dB},\qquad P_{sat},\qquad OIP3.\]Why GaN matters
GaN offers high breakdown voltage and high RF power density. Microwave Journal has repeatedly highlighted GaN-on-SiC for satellite PAs because it can reduce amplifier size and power consumption while maintaining high RF output.
See:
- GaN SSPA Technology for Space-Based Applications
- Linear Ka-Band GaN-on-SiC MMIC for Satcom Terminals
4. Traveling-wave-tube amplifier (TWTA)
TWTAs remain important in spacecraft where very high microwave output power and efficiency are needed.
NASA describes the TWTA as a microwave vacuum-tube amplifier in which an RF wave interacts with an electron beam traveling along the tube.
A spacecraft chain may be
\[\text{exciter} \rightarrow \text{TWTA} \rightarrow \text{waveguide switch} \rightarrow \text{HGA}.\]The NASA Roman Space Telescope, for example, uses a TWTA to create the high RF output power required for its Ka-band science downlink.
Know these concepts
- helix TWT;
- electron gun;
- slow-wave structure;
- collector;
- electronic power conditioner (EPC);
- gain and saturation;
- efficiency;
- lifetime;
- high-voltage design.
NASA continues to develop higher-efficiency Ka-band TWTAs for long-range space telecommunications.
5. Mixer and frequency converter
A mixer multiplies two signals and creates sum/difference frequencies:
\[f_{IF}=|f_{RF}-f_{LO}|.\]The same component can perform
- downconversion;
- upconversion;
- image-reject conversion;
- I/Q conversion.
Specifications
- conversion loss/gain;
- LO drive;
- RF/LO/IF isolation;
- IIP3;
- $P_{1dB}$;
- noise figure;
- spurious products.
Microwave Journal discusses practical I/Q and image-reject mixer architectures in Implementing I/Q, Single Sideband and Image Reject Mixers.
6. Filters
Filters control where RF energy is allowed to propagate.
Types include
- low-pass;
- high-pass;
- band-pass;
- band-stop/notch;
- cavity;
- waveguide;
- microstrip;
- SAW/BAW;
- tunable RFIC filters.
Important specifications are
\[IL,\quad RL,\quad BW,\quad Q,\quad \tau_g.\]where $\tau_g$ is group delay.
In a receiver, filter loss before the LNA directly degrades noise figure.
In a transmitter, filtering suppresses
- harmonics;
- mixer products;
- broadband PA noise;
- adjacent-channel emissions.
The Microwave Journal article SOI RFIC Tunable Filters Improve Phased Array System Performance is a useful example of the trade between filter loss, LNA gain, receiver NF and front-end power.
7. Diplexers, duplexers, IMUX and OMUX
These are especially important in satellite payloads.
Diplexer
Combines/separates two frequency bands onto a common path.
Duplexer
Allows transmit and receive functions to share an antenna while providing isolation.
IMUX
Input multiplexer separates incoming satellite channels.
OMUX
Output multiplexer combines high-power amplified channels before the antenna.
Know
- channel isolation;
- insertion loss;
- group delay;
- power handling;
- multipaction;
- thermal stability.
A useful Microwave Journal reference is Transceiver Duplexer Design Considerations.
8. RF switches
Common implementations include
- PIN-diode switches;
- GaAs pHEMT;
- SOI/SOS RFIC;
- MEMS switches;
- electromechanical/coaxial switches;
- ferrite waveguide switches.
Important specifications:
- insertion loss;
- isolation;
- switching time;
- linearity;
- hot-switching capability;
- power handling;
- control voltage/current.
In spacecraft, waveguide transfer switches can provide redundant routing between transmitters and multiple antennas.
9. Circulators and isolators
A circulator is a nonreciprocal device:
\[1\rightarrow2,\qquad 2\rightarrow3,\qquad 3\rightarrow1.\]If one port is terminated, it becomes an isolator.
Uses include
- protecting a PA from reflected power;
- Tx/Rx routing;
- stabilizing amplifier load impedance;
- protecting sensitive receivers.
Key parameters:
- isolation;
- insertion loss;
- VSWR;
- bandwidth;
- power handling.
Microwave Journal discusses their role in Duplexer Considerations for X-Band T/R Modules.
10. RF limiter / receiver protector
A limiter protects the receiver front end from large RF power.
Typical technologies include
- PIN diodes;
- Schottky diodes;
- GaAs/GaN limiter structures.
Know
- limiting threshold;
- flat leakage;
- spike leakage;
- recovery time;
- insertion loss;
- survival power.
A limiter often appears directly ahead of the LNA in radar, EW and shared-antenna systems.
11. Attenuators and DSAs
An attenuator provides a known RF loss.
A digital step attenuator (DSA) allows programmable gain control.
Important metrics:
- attenuation range;
- LSB/step size;
- RMS attenuation error;
- insertion loss;
- phase variation;
- IP3;
- power handling.
Space-qualified RFIC attenuators are attractive because they can replace larger discrete networks and support digital calibration.
12. Phase shifters
Phase shifters control
\[\phi\]without ideally changing signal amplitude.
They are central to
- phased arrays;
- vector modulators;
- cancellation loops;
- calibration.
Important specifications:
- phase range;
- phase resolution;
- RMS phase error;
- insertion loss;
- amplitude variation;
- bandwidth.
13. Beamformer IC and T/R module
A modern phased-array channel may contain
\[\boxed{ \text{switch} + \text{LNA} + \text{PA} + \text{phase shifter} + \text{attenuator} }\]around each antenna element or small subarray.
Microwave Journal describes planar array front ends built around PAs, LNAs and beamformers in Overcoming Planar Phased Array Circuit Design Challenges.
A beamformer IC may integrate
- phase control;
- gain control;
- T/R switching;
- channel calibration;
- telemetry.
14. Power dividers and combiners
Common types include
- Wilkinson;
- resistive;
- reactive;
- corporate feed;
- high-power combiners.
For an ideal equal two-way split,
\[P_{out,each}=\frac{P_{in}}{2}\]before dissipative losses.
Know
- insertion loss;
- isolation;
- amplitude balance;
- phase balance;
- power handling.
15. Directional couplers
A directional coupler samples a known fraction of forward or reverse traveling power.
Applications:
- power monitoring;
- VSWR/reflection measurement;
- feedback loops;
- test ports.
Important metrics:
- coupling factor;
- directivity;
- insertion loss;
- return loss;
- frequency flatness.
16. Hybrid couplers
A 90° or 180° hybrid splits signals with a known phase relationship.
They appear in
- balanced amplifiers;
- image-reject mixers;
- IQ modulators;
- monopulse receivers;
- power combiners.
The key specifications are amplitude and phase balance.
17. VCO, DRO and YIG oscillator
VCO
Voltage tunes oscillator frequency.
DRO
Uses a dielectric resonator for low-noise microwave oscillation.
YIG oscillator
Uses a magnetically tuned ferrimagnetic resonator for wide tuning and good spectral purity.
Important quantities include
- frequency range;
- phase noise;
- tuning sensitivity;
- pushing;
- pulling;
- harmonic content.
18. PLL and frequency synthesizer
A typical PLL contains
\[\boxed{ \text{reference} \rightarrow \text{phase-frequency detector} \rightarrow \text{loop filter} \rightarrow \text{VCO} \rightarrow \text{divider}. }\]A synthesizer generates many coherent frequencies from one reference.
Know
- phase noise;
- reference spurs;
- fractional-N spurs;
- loop bandwidth;
- lock time;
- frequency resolution.
Phase noise matters because it directly affects
- EVM;
- reciprocal mixing;
- radar coherence;
- Doppler/ranging accuracy.
19. Stable frequency references
Space systems may use
- TCXO;
- OCXO;
- ultra-stable quartz oscillator (USO);
- chip-scale atomic clock (CSAC);
- rubidium or other atomic references in demanding systems.
Important quantities:
- Allan deviation;
- aging;
- temperature coefficient;
- phase noise;
- radiation sensitivity;
- holdover.
Microwave Journal has reported space-qualified crystal oscillators designed for high total-dose tolerance and precision frequency control.
20. Frequency multipliers and dividers
A multiplier generates
\[f_{out}=Nf_{in}.\]Ideally, phase noise increases approximately by
\[20\log_{10}N\]in dB when frequency is multiplied by $N$.
Dividers can improve phase noise referred to the lower output frequency.
These blocks are common in microwave LO chains.
21. Detectors and log amplifiers
RF detectors convert RF amplitude/power into a low-frequency voltage or digital measurement.
Types include
- diode detectors;
- RMS detectors;
- logarithmic detectors;
- detector/controller loops.
Applications include
- PA power monitoring;
- AGC;
- telemetry;
- fault detection;
- calibration.
22. Modulators and demodulators
Common forms include
- I/Q modulator;
- vector modulator;
- BPSK/QPSK modulator;
- direct-conversion transceiver.
They connect complex baseband
\[I(t)+jQ(t)\]to an RF carrier.
Important impairments include
- I/Q gain mismatch;
- quadrature phase error;
- LO leakage;
- DC offset;
- EVM.
23. ADC and DAC
For the dedicated high-speed converter reference—including direct-RF sampling/synthesis, jitter limits, ENOB/SFDR, JESD204, ADC/DAC architectures and measurement—see ADC & DAC — Data Converters.
Modern microwave systems increasingly digitize closer to the antenna.
Important ADC metrics:
- sample rate;
- analog input bandwidth;
- ENOB;
- SNR;
- SFDR;
- aperture jitter.
For a sine-wave input, clock jitter limits SNR approximately as
\[SNR_{jitter} \approx -20\log_{10}(2\pi f_{in}\sigma_t).\]Important DAC metrics include
- sample rate;
- SFDR;
- output bandwidth;
- interpolation;
- noise spectral density.
Microwave Journal discusses the increasing use of direct ADC/DAC and integrated transceivers in Integrated Transceivers Simplify Design, Improve Phased Array Radar Performance.
24. FPGA, ASIC, RFSoC and DSP
The digital side handles
- modulation/demodulation;
- FEC;
- filtering;
- digital down/upconversion;
- beamforming;
- packet handling;
- encryption;
- telemetry;
- calibration.
For space, the choice also depends on
- radiation tolerance;
- configuration upset behavior;
- redundancy;
- scrubbing;
- power.
25. Transponder
A spacecraft transponder integrates much of the communication chain.
NASA describes spacecraft transponders as combined receive/transmit electronics that can
- acquire an uplink;
- track it with a PLL;
- demodulate command data;
- derive a coherent frequency reference;
- generate a downlink.
Deep-space transponders may support coherent turnaround for precise Doppler/ranging measurements.
See NASA’s Onboard Systems — Telecommunications Subsystems.
26. Exciter
An exciter generates the low-power modulated RF signal that is later amplified.
It may contain
- reference oscillator;
- synthesizer;
- modulator;
- DAC;
- IF/RF conversion;
- filtering.
The exciter’s spectral purity contributes directly to transmitter EVM and phase noise.
27. Waveguide
At microwave and millimeter-wave frequencies, waveguide is often preferred for high-power, low-loss routing.
Know
- TE/TM modes;
- cutoff frequency;
- flange types;
- insertion loss;
- bends/twists;
- pressurization;
- power handling;
- multipaction in space.
For rectangular waveguide,
\[f_{c,10} = \frac{c}{2a\sqrt{\epsilon_r}}.\]28. Coaxial cable and connectors
Common microwave interfaces include
- SMA;
- 3.5 mm;
- 2.92 mm (K);
- 2.4 mm;
- 1.85 mm (V);
- SMP/SMPM;
- TNC/N in lower-frequency rugged systems.
Know
- upper usable frequency;
- mode-free operation;
- repeatability;
- return loss;
- torque;
- power handling.
Connector transitions can dominate high-frequency measurement uncertainty.
29. Antenna feed, horn, OMT and polarizer
Space antennas often include more RF hardware than the reflector itself.
Feed horn
Illuminates a reflector.
OMT
Orthomode transducer separates two orthogonal polarizations.
Polarizer
Converts linear ↔ circular polarization.
Feed network
Routes multiple frequencies/polarizations.
Important specifications include
- return loss;
- isolation;
- axial ratio;
- cross-polarization;
- insertion loss.
30. Switch matrices and RF distribution units
Spacecraft with redundant radios and several antennas need routing networks.
An RF distribution unit may include
- transfer switches;
- diplexers;
- couplers;
- loads;
- waveguide;
- coax.
NASA/JPL spacecraft frequently use commandable waveguide switches to select the active antenna and amplifier path.
31. DC-DC converters
Space electronics rarely operate directly from the spacecraft bus voltage.
DC-DC converters create local rails.
Important quantities:
- efficiency;
- ripple;
- switching frequency;
- conducted/radiated EMI;
- transient response;
- radiation tolerance;
- fault behavior.
A 2026 Microwave Journal article, Radiation-Hardened Space-Based Power Systems, emphasizes that switching-supply noise can directly degrade sensitive RF systems.
32. LDO regulators
LDOs are useful for low-noise local rails.
Important specifications include
- PSRR;
- output noise;
- dropout;
- load transient;
- radiation;
- temperature.
A common architecture is
\[\text{DC-DC} \rightarrow \text{LDO} \rightarrow \text{PLL/LNA/ADC}.\]This combines conversion efficiency with local noise cleanup.
33. Semiconductor technologies to recognize
GaAs
Strong for
- LNAs;
- mixers;
- switches;
- phase shifters;
- medium-power PAs.
GaN
Strong for
- high-power PA;
- SSPA;
- radar;
- high-power satcom.
SiGe BiCMOS
Useful when high-frequency analog and dense digital/control integration must coexist.
RF SOI / SOS
Strong for
- switches;
- attenuators;
- tuners;
- integrated RF control.
CMOS
Excellent for high integration and digital-heavy RF transceivers.
InP
Used for very high frequency and very low-noise mmWave/THz applications.
The right technology is chosen by frequency, noise, output power, linearity, integration, radiation, cost and thermal requirements.
34. MMIC
A monolithic microwave integrated circuit implements several microwave functions on one semiconductor die.
Examples:
- PA;
- LNA;
- mixer;
- phase shifter;
- switch;
- attenuator;
- multifunction core chip.
MMICs reduce
- size;
- interconnect parasitics;
- assembly complexity.
But they introduce new concerns around
- thermal density;
- package transitions;
- yield;
- radiation qualification.
35. Packaging
Microwave packaging is part of the circuit.
Packages may include
- plastic QFN;
- ceramic QFN;
- hermetic ceramic;
- metal housing;
- bare die / chip-and-wire;
- LTCC;
- multichip modules.
Important effects include
- bond-wire inductance;
- package resonance;
- grounding;
- thermal path;
- cavity modes;
- outgassing;
- hermeticity.
Space applications often favor ceramic, metal and hermetic approaches when reliability or power dissipation justifies them.
36. Thermal design
A PA can be electrically excellent and still fail as a product because of junction temperature.
A basic thermal estimate is
\[T_j = T_{case} + P_{diss}\theta_{JC}.\]In vacuum there is no convective cooling.
Heat must be moved by
- conduction;
- heat pipes/straps;
- spacecraft structure;
- radiation to space.
This makes RF efficiency directly related to spacecraft thermal mass.
37. Radiation effects
Space components must be evaluated for several radiation mechanisms.
Total ionizing dose (TID)
Long-term accumulated ionizing exposure changes transistor/device parameters.
Single-event upset (SEU)
A particle changes logic state.
Single-event latchup (SEL)
A parasitic structure enters a high-current state.
Single-event burnout (SEB)
A destructive high-energy event, especially important in power devices.
Displacement damage
Particles physically damage the semiconductor lattice.
Radiation tolerance must be specified for the actual orbit and mission duration.
38. Space reliability and screening
Useful concepts include
- MIL-STD-883;
- MIL-PRF-38535;
- MIL-PRF-38534;
- NASA EEE-INST-002;
- lot qualification;
- burn-in;
- temperature cycling;
- hermeticity;
- derating.
The 2024 Microwave Journal space signal-chain article emphasizes reliability, packaging and radiation as first-order component-selection criteria.
39. Redundancy
Space communication chains commonly use redundant equipment.
Examples:
- two transponders;
- two PAs/TWTAs;
- cross-strapped receivers;
- multiple antennas;
- redundant oscillators;
- redundant power converters.
A failed component must not necessarily cause a failed mission.
RF switches and distribution networks are therefore part of reliability architecture, not merely signal routing.
40. Example deep-space spacecraft chain
A representative architecture is
\[\boxed{ \text{HGA} \rightarrow \text{diplexer/filter} \rightarrow \text{LNA} \rightarrow \text{downconverter} \rightarrow \text{transponder/modem} }\]for receive, and
\[\boxed{ \text{transponder/exciter} \rightarrow \text{upconverter} \rightarrow \text{driver} \rightarrow \text{TWTA/SSPA} \rightarrow \text{waveguide switch} \rightarrow \text{HGA} }\]for transmit.
NASA’s spacecraft documentation gives real examples using
- deep-space transponders;
- TWTAs;
- waveguide transfer switches;
- diplexers;
- filters;
- coax/waveguide;
- multiple high/medium/low-gain antennas.
41. Example phased-array front end
A representative active-array channel is
\[\boxed{ \text{antenna element} \leftrightarrow \text{T/R switch} \leftrightarrow \text{PA / LNA} \leftrightarrow \text{phase + gain control} \leftrightarrow \text{converter / beamformer}. }\]The Microwave Journal articles
- Overcoming Planar Phased Array Circuit Design Challenges
- Digital Beamforming Accelerates the Evolution to Next-Generation Radar
are useful references for the component-level evolution from analog T/R modules toward highly integrated and digital beamforming architectures.
42. Specifications that repeatedly appear
For microwave components, be comfortable reading
\[S_{11},\ S_{21},\ S_{12},\ S_{22},\]plus
- insertion loss;
- return loss;
- VSWR;
- gain;
- noise figure;
- $P_{1dB}$;
- $P_{sat}$;
- IIP3/OIP3;
- PAE;
- isolation;
- phase noise;
- spurs;
- group delay;
- EVM;
- ACLR;
- dynamic range;
- SFDR;
- bandwidth;
- switching speed;
- power handling.
For space parts, add
- TID;
- SEE/SEU/SEL/SEB;
- operating temperature;
- thermal resistance;
- screening level;
- mission life;
- hermeticity;
- vibration/shock;
- outgassing;
- derating.
43. Component checklist by subsystem
Receiver front end
- antenna/feed;
- preselector/filter;
- limiter;
- T/R switch/circulator;
- LNA;
- DSA/VGA;
- mixer/downconverter;
- LO/PLL/VCO;
- IF filter/amplifier;
- ADC.
Transmitter
- DAC/modulator;
- LO/PLL;
- upconverter;
- driver amplifier;
- DSA/VGA;
- PA/SSPA or TWTA;
- harmonic/output filter;
- isolator/circulator;
- coupler/detector;
- switch/diplexer;
- antenna.
Phased array
- core/beamformer IC;
- phase shifter;
- attenuator;
- switch;
- LNA;
- PA;
- power detector;
- calibration coupler;
- control IC;
- ADC/DAC for digital arrays.
Spacecraft telecom
- transponder;
- exciter;
- USO/OCXO/atomic reference;
- receiver;
- SSPA/TWTA;
- RF distribution unit;
- diplexer;
- waveguide transfer switch;
- coax/waveguide;
- HGA/MGA/LGA;
- modem/FEC;
- FPGA/ASIC;
- rad-hard DC-DC/LDO.
44. Trade and institutional references
Microwave Journal
- RF Signal Chain and Components for Space-Based Satcom Applications — excellent overall component map.
- Overcoming Planar Phased Array Circuit Design Challenges — PA/LNA/beamformer/T-R module integration.
- SOI RFIC Tunable Filters Improve Phased Array System Performance — filter placement and front-end tradeoffs.
- Digital Beamforming Accelerates the Evolution to Next-Generation Radar — phase shifters, attenuators, ADC/DAC and digital beamforming.
- Integrated Transceivers Simplify Design, Improve Phased Array Radar Performance — integrated ADC/DAC/mixer/PLL/transceiver architectures.
- Transceiver Duplexer Design Considerations — switch/limiter/circulator duplexers.
- GaN SSPA Technology for Space-Based Applications — space PAs and GaN.
- Radiation-Hardened Space-Based Power Systems — space power and RF noise.
- UltraCMOS RFICs Ease the Complexity of Satellite Designs — RFIC integration and radiation tolerance.
- An Enabling Future: The Evolution of GaN for Higher Performance Microwave and mmWave Systems — semiconductor technology context.
NASA / JPL
- NASA Small Spacecraft Communications State of the Art — radios, mixers, filters, amplifiers, antennas and modem functions.
- NASA Basics of Space Flight — Onboard Systems — spacecraft receivers, transponders, TWTAs, waveguide switches and antennas.
- NASA Roman RF Communications Electronics — real S/Ka-band spacecraft architecture with Ka transmitter and TWTA.
- NASA Deep Space Network — LNAs, IF conversion, exciters and high-power uplink amplifiers.
45. Arduino / MCU control of RF components
Many laboratory RF components are digitally controlled even though the signal path is analog or microwave. Arduino-class MCUs are often sufficient to configure PLLs, DSAs, RF switches, synthesizers, detectors, relays, and temperature/power-monitoring ICs over SPI, I²C, UART, or GPIO.
A common control path is
$ \text{PC} \rightarrow \text{Arduino / MCU} \xrightarrow{SPI} \text{PLL / attenuator / switch}. $
See Arduino Boards — What You Need to Know for voltage levels, buses, timers, interrupts, drivers, and debugging.
Radio-astronomy receiver components
Radio astronomy pushes many of these components to their sensitivity limits: cryogenic InP HEMT LNAs, superconducting SIS mixers, waveguide hybrids/OMTs, ultra-low-phase-noise LO chains, IF amplifiers, ADCs and correlator electronics. See Radio Astronomy — RF Circuits & Receiver Systems.
46. Relation to the rest of this reference
This page connects component-level RF hardware to the larger system:
\[\boxed{ \text{component} \rightarrow \text{RF chain} \rightarrow \text{antenna / array} \rightarrow \text{link budget} \rightarrow \text{mission}. }\]Related: RF & Microwave · AESA & Phased Arrays · Signal Integrity & Power Integrity · Spacecraft Electromagnetics · Artemis Lunar Communications · Measurements & Instruments