The final tests of the design elements of the Angara launch vehicle have been completed
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According to the report of the Khrunichev State Research and Production Space Center on October 23, 2012, the Federal State Unitary Enterprise “Research Center of Rocket and Space Technologies” (Remmash) successfully completed the test tests for cryostatic strength of the structural elements of the promising missiles- the Angara launch vehicle (product A5A2S - assembly No. A13) manufactured by the Khrunichev State Research Center of Space Technologies.
Tests of elements of the Angara launch vehicle at the stand (c) of the FKP SIC RCP
The purpose of the test assembly № А13 was to confirm the strength of the accelerator compartments of the III stage of the PH, as well as individual components of the Angara 3A and 5A PH under the influence of loads at all stages - from transporting the launch vehicle to the maximum aerodynamic pressures and separation of steps in flight.
Transportation of the third stage of the Angara launch vehicle (c) FKP SIC RCP
A total of 19 design cases were tested, including at cryogenic temperatures. The maximum loads when determining the axial rigidity were up to 270 tf, when determining the bending rigidity - up to 220 tcm, when loading the tank "O" with the design pressure - up to 7.2 atm. Control over deformations and stresses in the structure of assembly No. A13 was carried out by the method of multichannel strain gaging. Tests are performed in full in accordance with the technical specifications. External examination confirmed that the assembly number A13 passed the test successfully. The final results will be determined after processing the measurement results obtained during the tests.
The third stage of the Angara launch vehicle on the stand (c) of the FKP "SIC RCP"
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