GÖKTÜRK-2
The GÖKTÜRK-2 Program has been funded by The Scientific and Technological Research Council of Turkey (TÜBİTAK) and conducted by the Turkish Aerospace & TUBITAK Space team under the coordination of Ministry of National Defense between 2007-2012.
The GÖKTÜRK-2 System and mission have been indigenously designed by Turkish engineers. In the framework of the Project, Turkish Aerospace has performed the following activities regarding the GÖKTÜRK-2 Satellite;
– Structural System design, analysis, manufacturing and test
– Thermal Control System design, analysis, integration and test
– System accommodation design
– Harness design, manufacturing and test
– Attitude and Orbit Control interface unit design, manufacturing, qualification, integration and test
– Assembly of all Satellite Models (* 1SQM, 2QM, 3FM)
– Mass properties measurement of all Satellite Models (SQM, QM, FM) at TAI AIT Facilities
– Structural tests (static, vibration, acoustic) of all Satellite Models (SQM, QM, FM)
– Commissioning of the Thermal Vacuum Chamber (TVC) established at TAI AIT Facilities
– Thermal tests of the Satellite Qualification Model and Flight Model (at TAI TVC)
– Alignment measurements of the Satellite Models (QM, FM)
– Deployment tests of Solar Panels for the Satellite Models (QM, FM)
– Management of Satellite and Launch Vehicle compatibility
– Separation test of the Satellite (QM)
– Integrated Logistics Support
– Satellite FM integration and functional tests
– Indigenous development of thermal analysis software
