Figure 1. The individual slices, or decks, that comprise the PULSAR telemetry unit. The modular design enables inclusion of multiple-band frequency transmitters and receivers.

Researchers at NASA’s Marshall Space Flight Center have developed software-defined radio (SDR) telemetry transceiver technology to collect and transmit data to and from small satellites and microsatellites. The SDR concept uses a minimal number of traditional analog radio-frequency components to convert RF signals to a digital format. Digital signal processing replaces bulky radio-frequency components, and enables reduced cost as well as size, weight, and power requirements (SWaP). The NASA technology enables software and firmware updates that increase the lifespan and efficacy of satellites, supporting a wide variety of changing radio protocols as they are developed. A modular design enables inclusion of multiple band frequency transmitters and receivers (S-band, X-band, Ka-band, etc.). The NASA SDR can find use in satellite applications in which cost savings, upgradability, and reliability are essential. A first-generation SDR has been flight tested on NASA’s FASTSAT mission.

NASA’s SDR uses field-programmable gate array (FPGA) technology to enable flexible performance on orbit. A first-generation FM-modulated transceiver is capable of operating at up to 1 Mbps downlink and 50 kbps uplink, full duplex. An FPGA performs Reed-Solomon (255,223) encoding, decoding, and bit synchronization, providing Consultative Committee for Space Data Systems (CCSDS) and Near Earth Network (NEN) telemetry protocol compatibility. The transceiver accepts data from the onboard flight computer via a source synchronous RS422 interface.

Figure 2. Assembled PULSAR radio, with each deck stacked on top of the other. Decks are designed to be standalone (with the exception of the power deck) for any configuration.

NASA’s second-generation full-duplex SDR, known as PULSAR (Programmable Ultra-Lightweight System-Adaptable Radio) incorporates command receiver and telemetry transmitters, as well as updated processing and power capabilities (see figures). An S-band command receiver offers a maximum uplink data rate of 300 Kbps and built-in QPSK demodulation. X- and S-band telemetry transmitters offer a max downlink data rate of 150 Mbps, flexible forward-error correction (FEC) using Reed-Solomon encoding (LDPC rate 7/8 and 1/2 convolution in development), and QPSK modulation. The use of FEC adds an order-of-magnitude increase in telemetry throughput due to an improved coding gain. An onboard FPGA uses high-speed logic for uplink/downlink and encoding/decoding processes. Balloon flight testing has been conducted and is ongoing for PULSAR.

This technology enables support for changing radio protocols, implementation of new transponder types, and bug fixes while in service. In addition, it enables low production costs by leveraging high-quality componentry without the expense of qualification testing. Possible applications include atmospheric studies (climate and terrestrial weather monitoring and forecasting), Earth observation (transmission of imagery for urban planning, disaster monitoring, agriculture, etc.), and ionospheric studies (observation of space weather phenomena).

NASA is actively seeking licensees to commercialize this technology. Please contact Sammy A. Nabors at This email address is being protected from spambots. You need JavaScript enabled to view it. to initiate licensing discussions. Follow this link for more information: .