Design and Test Criteria for Components Subjected to Explosive Shock Environments

690616

02/01/1969

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
Full scale ground tests of explosive separation of missile stages defined the shock environment for sensitive components, and indicated the requirement for specification of test criteria according to component weight or location. Design and qualification test criteria for the components were derived by enveloping the peaks of ensembles of shock test response spectra. This approach was justified by analytical considerations. The resulting test criteria specified response spectra tolerance limits of + 100% and − 50%, and a damping ratio of 0.05 (Q = 10) for the shock response spectra analyses. A shock synthesizer electrodynamic shaker system was used successfully to conduct shock qualification tests using the criteria developed for the separation shock environment.
Meta TagsDetails
DOI
https://doi.org/10.4271/690616
Pages
14
Citation
Lane, S., "Design and Test Criteria for Components Subjected to Explosive Shock Environments," SAE Technical Paper 690616, 1969, https://doi.org/10.4271/690616.
Additional Details
Publisher
Published
Feb 1, 1969
Product Code
690616
Content Type
Technical Paper
Language
English