ISSN: 2375-2998
International Journal of Electrical and Electronic Science  
Manuscript Information
 
 
Minimization of Micro Discharge in Space TWT for Long Life Satellite Communication
International Journal of Electrical and Electronic Science
Vol.3 , No. 1, Publication Date: Mar. 1, 2016, Page: 1-7
4495 Views Since March 1, 2016, 3044 Downloads Since Mar. 1, 2016
 
 
Authors
 
[1]    

Vishnu Srivastava, Microwave Tubes Division, CSIR-Central Electronics Engineering Research Institute (CSIR-CEERI), Pilani-333031, Rajasthan, India.

 
Abstract
 

Critical technologies for minimizing micro discharge inside a space TWT are presented for long life and high reliability tube operation for satellite communication. UHV grade materials of low vapor pressure and low gas diffusion rate are used for tube fabrication. High purity alumina insulators are used in gun and collector assemblies with high voltage breakdown margin twice the operating voltage and leakage current less than 0.01µA. Ceramic to metal joints are fabricated to minimize triple-junction effects and to avoid charging of insulators due to any stray electron. High purity low loss alumina insulators (99.5%) are used for RF windows. RF coupler is fabricated to avoid multipactor discharge with a margin of 4 times the operating power output. All assemblies are brazed using Cu-Au alloys, and are checked for leak rate less than 10-12 torr litre/sec. The tube is UHV processed at 550°C for more than 100 hrs for ultimate vacuum inside tube less than 10-10 torr to minimize discharging over the tube life.


Keywords
 

Amplifier, Ceramic Insulators, Discharge, Microwave Tube, Space TWT, Satellite Transponder, UHV Device, UHV Materials


Reference
 
[01]    

V Srivastava, TK Ghosh, J Akhtar, SN Joshi, Design of high efficiency space TWT, IETE Technical Review, March-April 1999, pp. 249-254.

[02]    

V Srivastava, TK Ghosh, RK Sharma, SN Joshi, Indigenous design and development of high efficiency space TWTs, Microwaves & Optoelectronics, ISBN-81-88342-44-0, 2004, Anamaya Publishers, pp 1-8.

[03]    

L-3 Electron Technology Inc. for space TWTs, www. L-3. com.

[04]    

Thales Group for Space TWTs, www. thalesgroup. com.

[05]    

G Kornfeld, Reliability considerations for satellite TWTs, Microwave Journal, vol. 27, Aug. 1984, pp. 113-116.

[06]    

JP Calame, DK Abe, Application of advanced material technologies to vacuum electronic devices, Proceedings IEEE, May 1999, pp. 840-864.

[07]    

F Hai, KW Paschen, DC partial discharge/environmental test screening of space TWTs, Proceedings of 18th Intersociety Energy Conversion Engineering Conference, American Institute of Chemical Engineers, 1983, p. 2216-22.

[08]    

W Dürr, J Wegener, E Bosch, RF output multipaction margin of travelling wave tubes, IEEE-IVEC-2011, pp. 19-20.

[09]    

KW Paschen, F Hai, Automated partial-discharge testing of traveling-wave tubes, 1981 STIN. 8224430P, May, 1981.

[10]    

CH De Tourreil, KD Srivastava, Mechansm of surface charging of high voltage insulators in vacuum, IEEE Trans. on Electrical Insulation, vol. 8, March 1973 pp. 17-25.

[11]    

M Alaria, V Srivastava, Multipactor analysis of coaxial RF window for Space TWT, International Journal of Microwave and Optical Technology (USA), vol.6, Sept. 2011, pp. 255-258.

[12]    

K F Bartos, EB Fite, KA Shalkhauser, GR Sharp, A Three-Dimensional Finite-Element Thermal/Mechanical Analytical Technique for High Performance Traveling Wave Tubes, NASA Technical Paper 3081, 1991.

[13]    

RK Sharma, A Bera, V Srivastava, Thermal and Structural Analysis of Electron Gun Assembly for a C-band 60W Space TWT, International Journal of Microwave and Optical Technology, vol. 4, Sept. 2009, pp. 309-314.

[14]    

NV Bijeev, Design and Realization Challenges of Power Supplies for Space TWTs, IEEE-IVEC-2011, Bangalore, pp. 431-432.

[15]    

SAES Getters, www. saesgetters. com.





 
  Join Us
 
  Join as Reviewer
 
  Join Editorial Board
 
share:
 
 
Submission
 
 
Membership