IEEE International Vacuum Electronics Conference 2014
DOI: 10.1109/ivec.2014.6857483
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Broadband traveling wave tubes in Ka- and Ku-band

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Cited by 3 publications
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“…Taking the Cassini experiment as a reference, in which a Kα-band travelling wave tube amplifier (TWTA) on board the spacecraft had an output power of 10 W for a distance of 5 AU [25], therefore for the distance of 1.5 AU as in DOCS, an amplifier roughly needs an output power of 10 × (1.5/5) 2 W ≈ 1 W. This amplifier can be easily satisfied, e.g. today the most advanced amplifier in space for Kα-band communication can reach an output of 250 W with a bandwidth of 2.9 GHz [48,49]. However, in Cassini project a 4 meter diameter antenna on board the spacecraft, and especially a 34 meter diameter antenna receiver on ground were used to keep a decent low thermal noise level [25].…”
Section: Technical Issues To Be Solvedmentioning
confidence: 99%
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“…Taking the Cassini experiment as a reference, in which a Kα-band travelling wave tube amplifier (TWTA) on board the spacecraft had an output power of 10 W for a distance of 5 AU [25], therefore for the distance of 1.5 AU as in DOCS, an amplifier roughly needs an output power of 10 × (1.5/5) 2 W ≈ 1 W. This amplifier can be easily satisfied, e.g. today the most advanced amplifier in space for Kα-band communication can reach an output of 250 W with a bandwidth of 2.9 GHz [48,49]. However, in Cassini project a 4 meter diameter antenna on board the spacecraft, and especially a 34 meter diameter antenna receiver on ground were used to keep a decent low thermal noise level [25].…”
Section: Technical Issues To Be Solvedmentioning
confidence: 99%
“…This amplifier can be easily satisfied, e.g. today the most advanced amplifier in space for Kα-band communication can reach an output of 250 W with a bandwidth of 2.9 GHz[48,49]. However, in Cassini project a 4 meter diameter antenna on board the spacecraft, and especially a 34 meter diameter antenna receiver on ground were used to keep a decent low thermal noise level[25].It is not yet clear for DOCS if we could achieve a similar or even lower noise level by using similar antennas on board of the two spacecrafts (i.e.…”
mentioning
confidence: 99%
“…FLIGHT Current developments of very high power TWTs are on going in Europe with broadband designs covering the complete Ku-Band (10.7 to 12.7 GHz) with output powers of up to 300 W. These broadband developments can be in addition optimized for narrowband applications [14]. In the Ka-band the new designs will cover almost 3 GHz of bandwidth (from 17.25 GHz to 20.25 GHz) with power levels in the range of 250 W [14].…”
Section: IVmentioning
confidence: 99%
“…In the Ka-band the new designs will cover almost 3 GHz of bandwidth (from 17.25 GHz to 20.25 GHz) with power levels in the range of 250 W [14].…”
Section: IVmentioning
confidence: 99%