Abstract
The evolution of human spaceflight vehicles including launch vehicles continues to propose a perplexing conundrum in the structural dynamics field. Because of the size and weight of these vehicles, it becomes impossible to perform a ground based modal test that replicates all of the loading events of interest (i.e. liftoff, ascent, staging, etc.). As a result, human spaceflight programs have long relied on “building block approaches” to dynamic model updating and validation. Given the wide interpretation and definition of a “building block” approach to dynamic model validation, this paper reviews the state of art techniques used during the Saturn/Apollo and Space Shuttle dynamic test campaigns and contrasts them with the plans for the Space Launch System (SLS). Some of the lessons learned in each program are presented, in terms of how the building block approach was applied in developing models for stakeholders, using and updating analytical models, and use of other test result outside the dynamic tests.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReferences
Spaulding, D.B.: The art of partial modeling, Colloqium on modeling principles
Performance Test Code 60 Committee, Guide for verification and validation in computational solid mechanics, ASME V&V 10-2006 (2006)
Grimes, P.J., McTigue, L.D., Riley, G.F., Tilden, D.L.: Advancements in structural dynamic technology resulting from Saturn V programs, NASA-CR-1539, vol. I, June 1970
Grimes, P.J., McTigue, L.D., Riley, G.F., Tilden, D.L.: Advancements in structural dynamic technology resulting from Saturn V programs, NASA-CR-1539, vol. II, June 1970
Ryan, R., Jewell, R., Bugg, F., Ivey, W., McComas, R., Kiefling, L., Jones, J.: Dynamic testing of large space systems, NASA-TM-78307, September 1980
Mason, P.W., Harris, H.G., Zalesak, J., Bernstein, M.: Analytical and experimental investigation of a 1/8-scale dynamic model of the shuttle orbiter, vol. I – summary report, Grumman Aerospace Corporation, May 1974
Coppolino, R.: A numerically efficient finite element hydroelsatic analysis: volume I, theory and results, NASA-CR-2662, April 1976
Ivey, E.W.: Mated vertical ground vibration test, NASA-TM-78298, July 1980
Coppolino, R.: Methodologies for verification and validation of space launch system (SLS) structural dynamic models, NASA/CR-2018-219800/Volume I and II, January 2018
Napolitano, K., Yoder, N.: Fixed base FRF using boundary measurements as references – analytical derivation, Proceedings of the 30th International Modal Analysis Conference (2012)
Napolitano, K.L., Winkel, J.P., Akers, J.C., Suarez, V.J., Staab, L.D.: Modal survey of the MPCV orion European service module structural test article using a multi-axis shake table, Proceedings of the 36th International Modal Analysis Conference (2018)
Allen, M.S., Mayes, R.L.: Recent advances to estimation of fixed-interface modal models using dynamic substructuring, Proceedings of the 36th International Modal Analysis Conference (2018)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Society for Experimental Mechanics, Inc.
About this paper
Cite this paper
Sills, J.W., Allen, M.S. (2020). Historical Review of “Building Block Approach” in Validation for Human Space Flight. In: Walber, C., Walter, P., Seidlitz, S. (eds) Sensors and Instrumentation, Aircraft/Aerospace, Energy Harvesting & Dynamic Environments Testing, Volume 7. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-030-12676-6_1
Download citation
DOI: https://doi.org/10.1007/978-3-030-12676-6_1
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-12675-9
Online ISBN: 978-3-030-12676-6
eBook Packages: EngineeringEngineering (R0)