APA 6th Edition Huang, J. (2002). The Development of Inflatable Array Antennas. Automatika, 43 (3-4), 145-150. Retrieved from https://hrcak.srce.hr/6736
MLA 8th Edition Huang, John. "The Development of Inflatable Array Antennas." Automatika, vol. 43, no. 3-4, 2002, pp. 145-150. https://hrcak.srce.hr/6736. Accessed 3 Dec. 2021.
Chicago 17th Edition Huang, John. "The Development of Inflatable Array Antennas." Automatika 43, no. 3-4 (2002): 145-150. https://hrcak.srce.hr/6736
Harvard Huang, J. (2002). 'The Development of Inflatable Array Antennas', Automatika, 43(3-4), pp. 145-150. Available at: https://hrcak.srce.hr/6736 (Accessed 03 December 2021)
Vancouver Huang J. The Development of Inflatable Array Antennas. Automatika [Internet]. 2002 [cited 2021 December 03];43(3-4):145-150. Available from: https://hrcak.srce.hr/6736
IEEE J. Huang, "The Development of Inflatable Array Antennas", Automatika, vol.43, no. 3-4, pp. 145-150, 2002. [Online]. Available: https://hrcak.srce.hr/6736. [Accessed: 03 December 2021]
Abstracts Inflatable array antennas are being developed to significantly reduce the mass, the launch vehicle's stowage volume, and the cost of future spacecraft systems. Three inflatable array antennas, recently developed for spacecraft applications, are a 3.3 m × 1.0 m L-band synthetic aperture radar (SAR) array, a 1.0 m-diameter X-band telecom reflectarray, and a 3 m-diameter Ka-band telecom reflectarray. All three antennas are similar in construction, and each consists of an inflatable tubular frame that supports and tensions a multi-layer thin-membrane radiating surface with printed microstrip patches. These antennas demonstrated that inflatable arrays are feasible across the microwave and millimeter-wave spectrums. Further developments of these antennas are deemed necessary, in particular, in the area of qualifying the inflatable structures for space-environment usage.