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The stands are intended for testing the items of both rocket-space and aviation engineering for strength and reliability. The application of supporting units of original design allows testing for linear overloads, vibration and vibroimpact loads, changing climatic and environmental conditions, additional movements in several planes. The loads can be tested at their simultaneous effect and in any of the combinations.
It is possible to simulate intensive flight loads in ground-based conditions for large-size and heavy items.
Technical properties
Description | Value | |||||
Definition | СЭ-2,5 | СЭ-4 | СЭ-5А | СЭ-5В | СЭ-5-10 (small rotor) | СЭ-5-10 (big rotor) |
Diameter of the base, m | 2,5 | 4 | 5 | 5 | 5 | 10 |
Mass of the under test item, kg | 100 | 200 | 300 -1000 | 1000 | 1000 | 3000 |
Overload , units/ g | 500 | 320 | 250 -300 | 200 | 250 | 100 |
Specific power, kW/kg | 0,29 | 0,2 | 0,49 | 0,4 | 0,5 | 0,3 |
Heating temperature of the test item up to the temperature, оC | - | - | 1200 | 1200 | 1200 | 1200 |
Vibration frequency range which is being created, Hz | - | - | 10 -2500 | 10 -2500 | 10 - 2500 | 10 - 2500 |
19.05.2012