2011 Aerospace Conference 2011
DOI: 10.1109/aero.2011.5747319
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Deployment verification of large CFRP helical high-gain antenna for AIS signals

Abstract: In this paper the development of the structural design of a deployable helical antenna made from fiber composite material as well as its deployment verification in Zero-G environment will presented 1,2. In the introduction the advantages of helical antennas will be pointed out and a potential field of application, the receiving of AIS (Automatic Identification System) signals from maritime vessels, will be presented. The next chapter deals with the antenna design where especially manufacturing aspects will be … Show more

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Cited by 11 publications
(7 citation statements)
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“…One solution to this issue could be to reduce the beam width of the antenna, and thereby to decrease the coverage area. This case has already been analyzed and tested by DLR Bremen and demonstrated on the DLR satellite AISat [9]. The high gain helical antenna, used on AISat, cannot achieve a smaller coverage than 200 nautical miles.…”
Section: Maritime Mobile Servicesmentioning
confidence: 96%
“…One solution to this issue could be to reduce the beam width of the antenna, and thereby to decrease the coverage area. This case has already been analyzed and tested by DLR Bremen and demonstrated on the DLR satellite AISat [9]. The high gain helical antenna, used on AISat, cannot achieve a smaller coverage than 200 nautical miles.…”
Section: Maritime Mobile Servicesmentioning
confidence: 96%
“…There are many stowage and deployment methods being investigated such as scrunch-up, roll-up, origami-folded, and actively controlled deployment mechanisms. AISat featured a 57 cm diameter, 4 m long helical antenna that deployed like a spring and was designed to receive AIS signals at 162 MHz [3,4]. Inherently small helical antennas (i.e.…”
Section: A Helical Antenna Designmentioning
confidence: 99%
“…The significant engineering challenge in achieving a small-satellite deployable solution is apparent from these calculations (1)- (3). The deployed helix has a diameter of approximately 60 cm and a height of 3.2 m whereas a '1U' CubeSat volume is only 10 cm x 10 cm x 10 cm.…”
Section: A Helical Antenna Designmentioning
confidence: 99%
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