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Unit impulse input tests of a system of the «Frigate» upper-stage rocket
- Authors: Mikhalenkov N.A.1, Yermakov V.Y.1, Utkina Y.I.1
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Affiliations:
- Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region
- Issue: Vol 12, No 1 (2013)
- Pages: 73-79
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/124
- DOI: https://doi.org/10.18287/1998-6629-2013-0-1(39)-73-79
- ID: 124
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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
Test Engineer
Russian FederationV. Y. Yermakov
Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region
Email: v_ermakov2003@mail.ru
Candidate of Technical Science
Deputy Head of the Department of Dynamics and Spacecraft Vibration Isolation
Russian FederationY. I. Utkina
Federal State Unitary Enterprise «Lavochkin Research and Production Association», Khimki, Moscow region
Email: uliaytkina@gmail.com
Test Engineer
Russian FederationReferences
- 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.
- Испытательная техника [Текст]: справочник. В 2 кн. Кн. 1 / [Г. С. Батуев и др.]. – М.: Машиностроение, 1982. – 528 с.
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