2015 IEEE 16th Annual Wireless and Microwave Technology Conference (WAMICON) 2015
DOI: 10.1109/wamicon.2015.7120429
|View full text |Cite
|
Sign up to set email alerts
|

Microwave high power amplifier technologies for space-borne applications

Abstract: This work discusses the main challenges when designing Solid-State Power Amplifiers and Travelling-Wave Tube Amplifiers for space-borne applications. Some examples of flight-proven High Power Amplifiers are given together with on going developments and future trends towards high throughput satellites services (e.g. 3D-TV), that demand the use of higher frequency bands and increased levels of RF output power at the same time.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
3
0

Year Published

2016
2016
2023
2023

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 10 publications
(3 citation statements)
references
References 10 publications
0
3
0
Order By: Relevance
“…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%
See 1 more Smart Citation
“…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%
“…Additionally, since the available energy in a spacecraft is limited, due to the restricted number of solar panels and batteries, also the efficiency of every subsystem becomes a key feature. Therefore, the design of space-borne components is usually the result of a compromise among many aspects [1].…”
Section: Introductionmentioning
confidence: 99%