Engineering topics
Publications and source records attributed to Michael Campola.
Following a recommendation of the NASA Engineering and Safety Center (NESC), in 2022 NEPP has initiated the development of a NASA Agency-level Technical Standard for RHA. Progress status is presented on behalf of the SME core team.
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Free space optical (FSO) communication links increase data rate, reduce size and power, and increase security. These criteria are particularly important in space communication. Increasing mission complexity and crowding of lower frequency bands is driving the need for optical communications. This makes FSO communication technology extremely attractive, and there is significant ongoing work towards the development of FSO transceivers, ground stations, and relays. Notable projects include the Laser Communications Relay Demonstrator (LCRD), Integrated LCRD Low-Earth Orbit User Modem and Amplifier Terminal (ILLUMA-T), and CubeSat Laser Infrared Crosslink (CLICK) CubeSats. These technologies will eventually operate in unison with existing Radio Frequency (RF) systems, but there is little experimental investigation of such hybrid networks. This paper presents some experimental underpinnings of switching strategies for hybrid RF/FSO systems in various attenuation conditions. A 170 m optical path was constructed in an enclosed test chamber where atmospheric conditions can be tightly controlled. The performance of a 1550 nm infrared FSO link was evaluated in this chamber under varying conditions of turbulence and jitter. The system will eventually be used to investigate switching criteria between the FSO and RF channels. Optimizing the use of RF/FSO communication links will allow data rate, size, power, and security improvements. Therefore, this research will help to mature the network architecture and improve the performance of communication networks to be used for LEO, GEO, Lagrange, Lunar missions and beyond.
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Explore the source record for details and available documents.
Following a recommendation of the NASA Engineering and Safety Center (NESC), in 2022 NEPP has initiated the development of a NASA Agency-level Technical Standard for RHA. An initial progress status is presented on behalf of the SME core team.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
This study was undertaken to determine the total ionizing dose (TID) sensitivity of the PA10 Power Op Amp Manufactured by APEX (figure 1), which is a candidate for use on the LDCM TIRS instrument. The test was conducted with interest in both parametric degradation and functional failure in the configuration like that of the TIRS application. (See figure 2). The DUT was irradiated in a stepwise fashion, with parametric and functional degradation measured between steps. The parts were irradiated with gamma rays at a low dose rate (~0.01 rads(Si)/sec.).
This study was to determine the destructive single-event effect (SEE) susceptibility of the DS25BR100 series Low-Voltage Differential Signaling (LVDS) Buffers with Pre-emphasis and Equalization (DS25BR100, 110, and 120). The device was monitored primarily for destructive events while exposing it to a heavy ion beam at the Texas A&M University’s (TAMU) K500 Cyclotron.
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This study is to determine the destructive single event effect susceptibility of the Analog Devices ADG201 quad SPST switch. The device under tested (DUT) was monitored for destructive events by exposing it to a heavy ion beam at the Texas A&M University’s (TAMU) K500 Cyclotron.
This study was undertaken to determine the destructive single event effect and degradation susceptibility of the 80SCL060SCS Schottky diode. The device was monitored for destructive events and degradation in the reverse bias current during exposure to a heavy ion beam at Texas A&M University's K500 Cyclotron.
An overview of the 2020 single event effects FPGA effort performed by the NASA Electronic Parts and Packaging Group is presented. Information includes Heavy-ion data for the following FPGA devices: Xilinx Kintex-UltraScale and Microsemi PolarFire. Future work is presented.
An overview of the 2020 single event effects FPGA effort performed by the NASA Electronic Parts and Packaging Group is presented. Information includes Heavy-ion data for the following FPGA devices: Xilinx Kintex-UltraScale and Microsemi PolarFire. Future work is presented.
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