SpecificationsPeak forward anode voltage (see note 1) . . . . . . . ....................................... . 16 kVPeak inverse anode voltage (see note 2) ............. 16 kVPeak anode current . . . . . ................................. . 350 AAverage anode current . . . . . .....................
7665A: SpecificationsPeak forward anode voltage (see note 1) . . . . . . . ....................................... . 16 kVPeak inverse anode voltage (see note 2) ............. 16 kVPeak anode current . ...
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Peak forward anode voltage
(see note 1) . . . . . . . ....................................... . 16 kV
Peak inverse anode voltage (see note 2) ............. 16 kV
Peak anode current . . . . . ................................. . 350 A
Average anode current . . . . . .............................. 500 mA
Rate of rise of anode current
(see note 3) . . . . . . . . .................................... 2000 A/ms
Anode heating factor . . . . . ............................ . 5x109 VApps
The 7665A is a rugged hydrogen thyratron designed for use in compact military and civil radars. It has a ceramic envelope with a mounting flange and flying lead connections.
It features low jitter and low anode delay time and is suitable for use at high pulse repetition rates; it can switch peak powers up to 3 MW. The tube will operate over an ambient temperature range of 755 to +130 8C. A hydrogen reservoir is incorporated.
This tube of the 7665A was designed to comply with, and is electrically tested to, MIL-E-1/1485D.