The LiNSAT is based on the design and the bus similar to the Austrian first astronomical nano-satellite TUGSat-1/ BRITE-Austria (Koudelka, Egger et al. 2009) which is scheduled to launch in April 2011. The LiNSAT will carry a broadband radio-frequency receiver pay...
Perthe competition guidelinestheUK CanSat projectchallenges students aged 14 to 19 years of age to build a satellite which can relay telemetry data about atmospheric conditions such as could help with space exploration. The students’ primary mission is to collect temperature and pressure readings, an...
Receiver Transmitter User Datagram Protocol Universal Serial Bus Voltage Controlled Temperature Compensated Crystal Oscillator YP Yocto Project © 2024 GomSpace A/S All printed copies, and all electronic copies and versions except the one accessible on the GomSpace A/S server, are considered ...
4 Critical satellite subsystems The NanoBob mission will miniaturize the Bob receiver payload for it to fit inside a 12U CubeSat frame. This size limit is chosen as the smallest CubeSat standard that allows for a reasonably large main telescope of 150-mm diameter (potentially up to 180-mm di...
To provide an additional, and more accurate way to align both the OGS telescope and satellite receiver we will implement a two-way beacon (guide star) system, allowing for relatively fast closed-loop control of the satellite attitude, as well as satellite tracking by the OGS telescope. The ...
The AISatnano satellite project at the University of Applied Sciences Bremen is funded by the DLR Institute of SpaceSystems in Bremen and the mission goal is to test the new space based maritime automatic identicationsystem (AIS) payload. The Venta-1 spacecraft is build under the contract ...
In this paper, the development of Ground Sensor Terminal (GST) for the demonstration of Store & Forward (S&F) mission of our first nano-satellite, UiTMSAT-1, is presented. The UiTMSAT-1 is a BIRDS-2 nano-satellite project involving Japan, Malaysia, Philippines, and Bhutan. There are six...
Then, a complete engineering model of LaserCube in its intersatellite link configuration has been developed and tested. It features (1) a dual stage pointing and tracking system based on a coarse pointing mechanism patented by Stellar Project, (2) an optical head with a full–duplex telecom ...
1.A NanoPC device comprising:a small form factor low power computing, Internet accessing, communications and entertainment device, the size of PDA having a Miniature Projector to project focus free images generated by one or more of the plurality of the device application programs, on a flat sur...
In comparison to the existing on-market Pico/Nano-satellite buses, ITUpSAT Ⅱ bus provides not only higher computational power and data link capabilities but also precise orbit determination through its GPS receiver. To cope up with precise pointing requirements across a wide range of scientific ...