碩士 / 國立中央大學 / 光機電工程研究所 / 101 / Sounding Rocket NO.8 (SRV8) was launched on June 5, 2013, the rocket carried the reentry capsule to carry out ColdGas thrust experiment in flight. After the experiment, the reentry capsule dropped into the ocean for recovery. The wireless communication and recovery beacon system for the reentry capsule was developed. The primary communication frequency for command and data exchange is UHF 433MHz, while S-Band 2.4GHz is for radar tracking and burst mode data downlink. Moreover, there is a 1.575GHz GPS receiver inside for positioning. The functionality of the system is certified worthy for flight through the test of in-rocket wireless communication through the full flight scenarios, the test of communication distance of side window antenna and open cap airbag antenna after parachute deployment, and the test of GPS positioning.
| Identifer | oai:union.ndltd.org:TW/101NCU05651104 |
| Date | January 2013 |
| Creators | Chih-an Lai, 賴致安 |
| Contributors | Tse-Liang Yeh, Shyh-Biau Jiang, 葉則亮, 江士標 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | zh-TW |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 58 |
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