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Browsing by Author "Wadleigh, K. H."

Browsing by Author "Wadleigh, K. H."

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  • Wadleigh, K. H.; Wiger, H. (Bendix Aerospace Systems Division, 1970)
    This ATM presents the results of the structural dynamics analysis performed for the A2/SP-3 structural arrangement. Section I describes the dynamics portion, and Section II presents the stress analysis.
  • Wadleigh, K. H.; Owens, J. H., Jr.; Dewhirst, D. L. (Bendix Aerospace Systems Division, 1970)
    The purpose of this analysis is to determine the structural effect on ALSEP of an inadvertent rocket motor firing before the ASE is deployed.
  • Min, G. B.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the dynamic analyses performed on two different versions of ALSEP Array E - Subpack I. One version contained the Lunar Surface Gravimeter ( LSG) experiment, among others, while the other ...
  • Wadleigh, K. H. (Bendix Aerospace Systems Division, 1970)
    This ATM presents the results of a dynamic analysis of the heat flow experiment subpallet assembly for Array D. Both the engineering test model and the flight model were investigated.
  • Kaliniec, L.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the dynamic analysis and testing performed on the DVT model of the LEAM Experiment Package. The interface of this package is with the Array E (Apollo 17) - Subpack No. 2 pallet.
  • Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM gives the results of the dynamic analysis on the LEAM Flight Model Experiment Package. The DVT model dynamic analysis and testing results were presented in ATM 1022, Reference 1. A comparison of the flight model ...
  • Goran, M.; Min, G. B.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the structural dynamics analysis performed on the Lunar Ranging Retro Reflector 300 Corner Array.
  • Owens, J. H., Jr.; Wadleigh, K. H.; Chang, D. C. (Bendix Aerospace Systems Division, 1970)
    The attached structural analysis is divided into three sections. Section I presents the component level stress analysis. This analysis is based on an assumed limit loading of 20g's in any direction. Section II is the ...

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