Advances in aircraft and spacecraft science

  • 제5권2호
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  • Pages.165-175
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  • 2018
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  • 2287-528X(pISSN)
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  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
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Spacecraft vibration testing: Benefits and potential issues

  • Kolaini, Ali R. (Jet Propulsion Laboratory, California Institute of Technology) ;
  • Tsuha, Walter (Jet Propulsion Laboratory, California Institute of Technology) ;
  • Fernandez, Juan P. (Jet Propulsion Laboratory, California Institute of Technology)
  • 투고 : 2017.01.29
  • 심사 : 2017.11.06
  • 발행 : 2018.03.25
⟨ 이전 논문 다음 논문 ⟩

초록

Jet Propulsion Laboratory has traditionally performed system level vibration testing of flight spacecraft. There have been many discussions in the aerospace community for more than a decade about spacecraft vibration testing benefits or lack thereof. The benefits and potential issues of fully assembled flight spacecraft vibration testing are discussed herein. The following specific topics are discussed: spacecraft screening test to uncover workmanship problems for launch dynamics environments, force- and moment-limited vibration testing, potential issues with structural frequency identification using base shake test data, and failures related to vibration shaker testing and ways to prevent them.

키워드

참고문헌

  1. Dynamic Environmental Criteria (2001), NASA-HDBK-7005.
  2. Gordon, S. and Kern, D.L. (2015), "Benefits of spacecraft vibration testing", Proceedings of the Spacecraft and Launch Vehicle Dynamic Environments Workshop, The Aerospace Corp., El Segundo, CA.
  3. Kolaini, A.R. (2015), "Spacecraft vibration test/no-test", Proceedings of the Spacecraft and Launch Vehicle Dynamic Environments Workshop, The Aerospace Corp., El Segundo, CA.
  4. Michael, B.V.D. and Landry, P. (2014), "Real-time overturning moment limiting of a spacecraft random vibration test using analog hardware network", Proceedings of the Spacecraft Launch Vehicle Workshop, EL Segundo, CA.
  5. Payload Vibroacoustic Test Criteria (2011), NASA-STD-7001A, 01 February.
  6. Remedia, M. (2016), "A virtual testing approach for spacecraft structures post-correlation purposes", ECSSMET 2016, Toulouse, France.
  7. Scharton, T. (1977), Force Limited Vibration Testing Monograph", NASA Reference Publication, RP-1403.
  8. Scharton, T. (2002), Vibration and Acoustic Testing of Spacecraft, Sound and Vibration, June.
  9. Spacecraft Dynamics Environments Testing (2014), NASA-HDBK-7008, 06 December.
  10. Steffen, W. (2016), "Numerical modelling and simulation of a closed-loop electrodynamic shaker and test structure model for spacecraft vibration testing", Proceedings of the ECSSMET 2016, Toulouse, France.
  11. Tsuha, W., Darlene. S.L. and Long, M. (2015), "Potential issue with structural frequency identification using base driven vibration test data", Proceedings of the Spacecraft Launch Vehicle Workshop, EL Segundo, CA.

피인용 문헌

  1. An investigation on the vibrations of laminated shells under aeroacoustic loads using a WFE approach vol.6, pp.6, 2018, https://doi.org/10.12989/aas.2019.6.6.463