Turkey’s full grade state-of-the-art Space Systems Assembly Integration and Test (AIT) Center, which exist in a few developed countries leader in the space sector in the world is fully operational at Turkish Aerospace premises in Ankara.

 


AIT Center is designed to serve for assembly & integration activities, functional performance test and environmental test to be conducted all space systems for earth observation, communication and similar featured satellites until they are ready for launch activities. In addition, the facility has an infrastructure for manufacturing multi-layer insulation blanket, harness manufacturing and measurement processes and ground testing of space systems compatible with ECSS Standards.

 


This state-of-the-art AIT Center serves for more than one satellite up to 5 tons simultaneously by means of 3,800 m2 ISO-8 grade cleanroom and specific ground support equipment within the 10,000 m2 under roof approximately. Besides, ISO-6 grade mobile cleanroom offers high precision activities such as optical equipment/sensors, circuit board operation etc.

 


The time is crucial for system integrators and customers so, the direct connection of the AIT Center to the airport taxiway provides unique advantages in terms of safety, cost and risk management as well as opportunities to complete customs formalities within the premises.
Within the scope of satellite “Assembly” activities, it is aimed to form the main architecture of the satellite such as gathering primary and secondary structures including open end harness installation. By means of “Integration” activities, equipment and sub-system connections are performed to make satellite as functional. Assembly and Integration activities are followed by “Functional Performance Test” activities to generate all possible satellite mission scenarios. The purpose of the functional tests is to ensure that both satellite hardware and software is well functioning with respect to requirements/specifications based on the developed test scenarios related to the mission of satellite in space and performance verification of satellite components.

 


During "Environmental Testing", activities are performed to verify the qualification of satellite and its components against severe environmental conditions during launch and mission phases. The objective of these tests is to simulate environmental conditions from launch to space as close as real conditions and to ensure that satellite with its components exposed to these conditions are working properly. With these challenging activities, the requirements coming from the customers are also verified.
After all successful environmental and functional tests, the satellite will be ready for launch. Please click here for the Space Systems Integration and Test (AIT) Center test systems specifications.

 


Turkish Aerospace AIT Center aims to develop national space systems capability and provide benefits with space systems services to the international customers in the world. Our experiences and the versatility of state-of-the-art AIT facility privileged us in space systems activities against our competitors.

 


Turkish Aerospace continues for innovation in space systems by adopting emerging technologies and implementing new processes, products and solutions.

 


In addition to national projects, Turkish Aerospace Space Systems AIT Center offers transparent and comprehensive services to international distinguished customers.

 


This privilege enables Turkish Aerospace to submit competitive offers to its potential customers for their upcoming projects. Fully equipped Space Systems AIT Center that exists in a few developed countries in the world, makes Turkish Aerospace a challenging international player by providing assembly, integrations and test services for space systems.

 


Moreover, besides professional in-house engineering, analysis, manufacturing and test services, Turkish Aerospace ready to host its customers as an internal resident by means of guesthouse, shopping center, leisure centers, clinic, schools, kindergarden, etc. all inside the premises.

FEATURES
Thermal Vacuum Tests

The satellite begins to be exposed to challenging space conditions even before it is separated from the launcher when it reaches a certain altitude. Space conditions including low pressure, the sun causing heat and heat flux from the Earth and deep space environments causing cooling are simulated in the Thermal Room.

Mass Properties Measurements

Mass parameters used in the launch of the satellite into orbit and the orientation of the satellite required to be measured precisely (mass center, inertia momentum etc.) are measured by the Mass Specifications Measurement System.

Vibration Tests

The effect of mechanical loads occurring with the activation of the launcher on the satellite is observed by vibration tests. Vibration tests are performed separately on the main 3-axes through the electro-dynamic shocker.

Electromagnetic Interaction/Compliance Tests

These test are performed in a fully non-reflective area (free from any RF effect coming from the external environment) to detect the electromagnetic interference occurring when the satellite is at the launch site and after it is placed into the launcher, and verify that each equipment is working electromagnetically in harmony with each other.

Compact Antenna Tests

Antenna tests are conducted to assess the satellite antenna performance. With the reflectors and resources in the Compact Antenna Test Room, the distance of the satellite in orbit to the Earth is simulated to test the functionality and performance of the antennas (antenna gain, receiver and transmitter signal power levels etc.). These tests ensure that the satellite broadcast will only reach the desired target on Earth.

Acoustic Tests

Acoustic Tests: The mechanical loads caused by the reflection of strong sound waves generated by the activation of the launcher on the launcher and hence the satellite are simulated in acoustic tests. The satellite placed in the Acoustic Test Room is exposed to sound waves generated by specialized horns fed by pressurized gaseous nitrogen.

 
 
SPACE SYSTEMS ASSEMBLY INTEGRATION AND TEST CENTER
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