Development of the Orlan space-station antenna

Citation
Vk. Tripp et al., Development of the Orlan space-station antenna, IEEE ANT PR, 42(5), 2000, pp. 9-27
Categorie Soggetti
Eletrical & Eletronics Engineeing
Journal title
IEEE ANTENNAS AND PROPAGATION MAGAZINE
ISSN journal
10459243 → ACNP
Volume
42
Issue
5
Year of publication
2000
Pages
9 - 27
Database
ISI
SICI code
1045-9243(200010)42:5<9:DOTOSA>2.0.ZU;2-M
Abstract
The design of the Crew-Lock antenna for the Russian communication and data system [for the international Space Station] was challenging, because it is enclosed in a conducting shell. In addition, the electromagnetic-field dis tribution within the Crew Lock is highly constrained by the lowest one or t wo normal modes of the structure. Two kinds of antennas were investigated t o address the requirements (presented in Section 2). a half loop and a load ed patch. Computer modeling of these approaches was done by the Finite-Elem ent and Moment Methods, respectively (Section 3). The loop antenna underwen t extensive scale-model testing, and some full-scale tests at Johnson Space Center in Houston (Section 4). The patch antenna was eliminated during the hull-scale tests. The final design is the "towel-bar" loop, which performs the additional function of a handrail for astronauts during the ingress an d egress for extra-vehicular activity (EVA).