Unit impulse input tests of a system of the «Frigate» upper-stage rocket

Abstract


The paper is devoted to impact tests of a system of the «Frigate» upper-stage rocket, various methods of influence on the test object being used. A procedure is proposed for testing the system of separating the upper stage from the «I» block that makes it possible to reduce the number of loadings of the object.


About the authors

N. A. Mikhalenkov

Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region

Author for correspondence.
Email: n.mikhalenkov@gmail.com

Russian Federation

Test Engineer

V. Y. Yermakov

Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region

Email: v_ermakov2003@mail.ru

Russian Federation

Candidate of Technical Science

Deputy Head of the Department of Dynamics and Spacecraft Vibration Isolation

Y. I. Utkina

Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region

Email: uliaytkina@gmail.com

Russian Federation

Test Engineer

References

  1. Приборы и системы для измерения вибрации, шума и удара [Текст]: справочник. В 2 кн. Кн. 2 / под ред. В.В. Клюева. – М.: Машиностроение, 1978. – 439 с.
  2. Испытательная техника [Текст]: справочник. В 2 кн. Кн. 1 / [Г. С. Батуев и др.]. – М.: Машиностроение, 1982. – 528 с.

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