A Compact Extremely High Frequency MPM Power Amplifier

The development of a compact radio frequency (RF) vacuum power amplifier for high-resolution airborne radar is described. The amplifier, a microwave power module (MPM), operates in the upper millimeter-wave frequency band of 231.5-235 GHz providing a peak output power of 32 W. Common with previous e...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:IEEE transactions on electron devices 2018-06, Vol.65 (6), p.2183-2188
Hauptverfasser: Armstrong, Carter M., Kowalczyk, Richard, Zubyk, Andrew, Berg, Kevin, Meadows, Clark, Chan, Danny, Schoemehl, Thomas, Duggal, Ramon, Hinch, Nora, True, Richard B., Tobin, Robert, Sweeney, Michael, Weatherford, Brandon
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The development of a compact radio frequency (RF) vacuum power amplifier for high-resolution airborne radar is described. The amplifier, a microwave power module (MPM), operates in the upper millimeter-wave frequency band of 231.5-235 GHz providing a peak output power of 32 W. Common with previous extremely high frequency MPM development at Electron Devices, the {G} -band MPM consists of a periodic permanent magnet focused serpentine waveguide traveling wave tube (TWT) and a miniaturized 20-kV electronic power conditioner. Input drive to the MPM for saturation is around 10 mW. Low-loss chemical vapor deposition diamond WR-4.3 windows serve as the input and output ports of the TWT. Due to the high duty of the radar application, a four-stage TWT collector is employed for beam energy recovery. The MPM operates from a 270- \text{V}_{\sf {dc}} power source. Two MPM configurations have been constructed: a single integrated unit for laboratory testing and a split-package configuration for integration in a standard electro-optical/infrared gimbal. The split-package flight test unit has a maximum prime power requirement of 176 W, corresponding to an overall amplifier efficiency of 9%. The radar sensor has been flown on a modified DC-3 test bed with high-resolution real-time video imagery obtained under cloud-obscured operating conditions.
ISSN:0018-9383
1557-9646
DOI:10.1109/TED.2018.2808327