DocumentCode
2700751
Title
Pick-up horn for high power TVAC test of spacecraft payloads for communication satellites
Author
Rao, Sudhakar ; Lee-Yow, Clency ; Venezia, Philip
Author_Institution
Lockheed Martin Commercial Space Syst., Newtown, PA
fYear
2006
fDate
9-14 July 2006
Firstpage
3133
Lastpage
3136
Abstract
This paper presents a novel method for high power thermal vacuum tests of spacecraft payloads using pick-up horns (PUH). The PUH method has benefits of being cost-effective, compact, easy to implement, does not require breaking the vacuum several times and avoids physical contact with flight hardware. It is designed with four oversized slots to receive the high RF power from the flight horns, absorb almost all the power and efficiently transfer the heat outside the TVAC chamber with minimal reflections back to the horn and minimal RF leakage outside the PUH. The PUH has been successfully used for high power TVAC testing and validation of a Ku-band payload for satellite communications
Keywords
antenna testing; microwave antennas; satellite antennas; Ku-band payload; RF leakage; flight hardware; flight horns; high RF power; high power TVAC test; high power thermal vacuum tests; pick-up horn; satellite communication; spacecraft payloads; Artificial satellites; Coolants; Hardware; Heat transfer; Payloads; Performance evaluation; Radio frequency; Reflection; Space vehicles; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Antennas and Propagation Society International Symposium 2006, IEEE
Conference_Location
Albuquerque, NM
Print_ISBN
1-4244-0123-2
Type
conf
DOI
10.1109/APS.2006.1711274
Filename
1711274
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