In February 2013, the first Austrian nanosatellite BRITE-Austria/TUGSAT‑1 was launched into orbit to observe the brightness variations of massive luminous stars. Although the mission was originally planned to last only two years, BRITE-Austria has been providing scientific data at a high quality standard for more than eight years. The natural degradation of the systems on board over time as well as the impact of radiation, especially on the light-sensitive detectors, led to a decrease in efficiency and data quality. To ensure the continuous operation and a high level of data quality, several countermeasures were successfully introduced over the years, some of which are highlighted in this paper.The BRITE mission has shown impressively that, with the help of small and inexpensive satellites, even highly demanding scientific objectives can be achieved. The BRITE satellites have delivered new insights into the physical nature of stars, their pulsations, and “heartbeats”, as described in numerous publications, and even observed the complete development of a nova in the Carina field.
<p>The PRETTY mission is a 3U CubeSat mission, hosting two different payloads, a radiation dosimeter and an interferometric GNSS reflectometer. The intended launch is planned in 2022.</p><p>The reflectometer payload has been built, using flight representative hardware and mounted inside a portable setup. Two campaigns have been carried out, a first one to verify the setup in real world condition and the second one to record reflectometry data over the Danube river. The reflections over the river are analyzed and compared to a reference data set obtained from basemap.at (which is released under Open Government Data &#214;sterreich Lizenz CC-BY 4.0).</p><p>The hardware is capable of generating complex and power waveforms at the same time, and the reflection events are visible in both. Since PRETTY is aiming for phase altimetry, only coherent measurements are conducted with an integration time of 20ms&#160;.</p><p>The re-tracking algorithm for the specular point and height estimation are based on [1]. Due to the low elevation angle and receiver height, the effects from the ionosphere is not considered&#160;, however effects from the atmosphere have to be included in the data re-tracking process. The reflection peaks, and the signal to noise ratio of the peaks, are large enough detect the peak and to calculate the height of the reflection point. The height retrieval is shown in the paper.</p><p>The results are promising w.r.t. the performance of the overall structure of the PRETTY GNSS-R payload&#160; in order to deliver altimetry results on a low-cost CubeSat platform.</p><p>[1] W. Li, E. Cardellach, F. Fabra, S. Rib&#243; and A. Rius, "Assessment of Spaceborne GNSS-R Ocean Altimetry Performance Using CYGNSS Mission Raw Data," in IEEE Transactions on Geoscience and Remote Sensing, vol. 58, no. 1, pp. 238-250, Jan. 2020. doi: 10.1109/TGRS.2019.2936108</p>
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