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Title: Cable Effects Study. Tangents, Rabbit Holes, Dead Ends, and Valuable Results

Abstract

Lessons learned during a study on the effects that electrical power and signal wiring harness cables introduce on the dynamic response of precision spacecraft is presented, along with the most significant results. Our study was a three year effort to discover a set of practical approaches for updating well-defined dynamic models of harness-free structures where knowledge of the cable type, position, and tie-down method are known. Although cables are found on every satellite, the focus was on precision, low damping, and very flexible structures. Obstacles encountered, classified as tangents, rabbit holes, and dead ends, offer practical lessons for structural dynamics research. The paper traces the historical, experiential progression of the project, describing how the obstacles affected the project. Methods were developed to estimate cable properties. Problems were encountered because of the flexible, highly damped nature of cables. A beam was used as a test article to validate experimentally derived cable properties and to refine the assumptions regarding boundary conditions. Furthermore, a spacecraft bus-like panel with cables attached was designed, and finite element models were developed and validated through experiment. Various paths were investigated at each stage before a consistent test and analysis methodology was developed

Authors:
 [1];  [2];  [3];  [3];  [4];  [4]
  1. Schafer Corporation, Albuquerque, NM (United States)
  2. Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
  3. Moog CSA Engineering, Albuquerque, NM (United States)
  4. U.S. Air Force Research Lab., Kirtland Air Force Base, NM (United States)
Publication Date:
Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Org.:
USDOE National Nuclear Security Administration (NNSA)
OSTI Identifier:
1106898
Report Number(s):
SAND-2013-6590J
Journal ID: ISSN 0022-4650; 465010
Grant/Contract Number:
AC04-94AL85000
Resource Type:
Journal Article: Accepted Manuscript
Journal Name:
Journal of Spacecraft and Rockets
Additional Journal Information:
Journal Volume: 52; Journal Issue: 2; Journal ID: ISSN 0022-4650
Publisher:
AIAA
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Citation Formats

Ardelean, Emil V., Babuška, Vít, Goodding, James C., Coombs, Douglas M., Robertson, Lawrence M., and Lane, Steven A. Cable Effects Study. Tangents, Rabbit Holes, Dead Ends, and Valuable Results. United States: N. p., 2014. Web. doi:10.2514/1.A32792.
Ardelean, Emil V., Babuška, Vít, Goodding, James C., Coombs, Douglas M., Robertson, Lawrence M., & Lane, Steven A. Cable Effects Study. Tangents, Rabbit Holes, Dead Ends, and Valuable Results. United States. doi:10.2514/1.A32792.
Ardelean, Emil V., Babuška, Vít, Goodding, James C., Coombs, Douglas M., Robertson, Lawrence M., and Lane, Steven A. Mon . "Cable Effects Study. Tangents, Rabbit Holes, Dead Ends, and Valuable Results". United States. doi:10.2514/1.A32792. https://www.osti.gov/servlets/purl/1106898.
@article{osti_1106898,
title = {Cable Effects Study. Tangents, Rabbit Holes, Dead Ends, and Valuable Results},
author = {Ardelean, Emil V. and Babuška, Vít and Goodding, James C. and Coombs, Douglas M. and Robertson, Lawrence M. and Lane, Steven A.},
abstractNote = {Lessons learned during a study on the effects that electrical power and signal wiring harness cables introduce on the dynamic response of precision spacecraft is presented, along with the most significant results. Our study was a three year effort to discover a set of practical approaches for updating well-defined dynamic models of harness-free structures where knowledge of the cable type, position, and tie-down method are known. Although cables are found on every satellite, the focus was on precision, low damping, and very flexible structures. Obstacles encountered, classified as tangents, rabbit holes, and dead ends, offer practical lessons for structural dynamics research. The paper traces the historical, experiential progression of the project, describing how the obstacles affected the project. Methods were developed to estimate cable properties. Problems were encountered because of the flexible, highly damped nature of cables. A beam was used as a test article to validate experimentally derived cable properties and to refine the assumptions regarding boundary conditions. Furthermore, a spacecraft bus-like panel with cables attached was designed, and finite element models were developed and validated through experiment. Various paths were investigated at each stage before a consistent test and analysis methodology was developed},
doi = {10.2514/1.A32792},
journal = {Journal of Spacecraft and Rockets},
number = 2,
volume = 52,
place = {United States},
year = {Mon Aug 04 00:00:00 EDT 2014},
month = {Mon Aug 04 00:00:00 EDT 2014}
}

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