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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (11): 644-646.

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STUDY ON VIBRATION AND SHOCK TEST PARAMETER FOR AVIATION ROCKET LAUNCHERS

Wang Jianmin   

  1. Qingan Aerospace Equipment Research Institute
  • Received:1989-10-25 Revised:1990-04-15 Online:1990-11-25 Published:1990-11-25

Abstract: The theoretical basis of specifying parameters of vibration and shock test for aviation recket launchers are discussed. The usage features of them are investigated. Finally, some concrete opinions regarding the parameter specification are given.

Key words: launcher, vibration and shock, parameter