A simplified method for launch vehicle coupled loads analysis with spacecraft by combined apparent mass matrices and inertia relief technique

Author:

NIWA Tomoya1,ANDO Shigemasa1,SHI Qinzhong1

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

Japan Society of Mechanical Engineers

Reference19 articles.

1. Arya Majed, Kevin Partin, Ed Henkel and Thomas P. Sarafin, Variational coupled loads analyses: reducing risk in development of space-flight hardware, Journal of Spacecraft and Rockets, Vol. 42, No. 1(2005).

2. Craig, Jr., R. R. and Bampton, M. C. C., Coupling of sub-structures for dynamic analysis, AIAA Journal, Vol. 6, No.7(1968), pp.1313-1319.

3. Cuppens, K., Sas, P., and Hermans, L., Evaluation of the FRF based substructuring and modal synthesis technique applied to vehicle FE data, Proceedings of the 25th International Seminar on Modal Analysis, Leuven Belgium,(2000).

4. Guyan, R.J., Reduction of stiffness and mass matrices, AIAA Journal, Vol. 3, No. 2 (1965), p.380.

5. Japan Aerospace Exploration Agency (JAXA), Structure design standard, JERG-2-320, revision A(2011), pp.26 (in Japanese).

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