Reduction of Dynamic Stresses and Overloads Using Dampers in the Rocket Fairing Separation System

Author:

Zaitsev BorysORCID,Protasova TetianaORCID,Smetankina NataliaORCID,Klymenko DmytroORCID,Akimov DmytroORCID

Publisher

Springer International Publishing

Reference15 articles.

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2. Kolesnikov, K.S., Kokushkin, V.V., Borzykh, S.V., Pankova, N.V.: Calculation and design of missile stage separation systems: a tutorial. N. E. Bauman Moscow State Technical University Publications, Moscow (2006)

3. Potapov, A.M., Kovalenko, V.A., Kondratiev, A.V.: Payload fairings comparison of existing and prospective launch vehicles and their foreign counterparts. Aerosp. Tech. Technol. 1(118), 35–43 (2015)

4. Rusin, M., Romashin, A.G., Kamnev, P.I.: Experience in the development of aircraft head fairings. Aerosp. Tech. Technol. 5(13), 63–69 (2004)

5. Tang, X.-H., Li, B., Li, G., Hao, P., Chen, C., Ren, M.-F.: Self-impact analysis of the fairing hinge system based on dynamic constitutive models. Chin. J. Comput. Mech. 34(4), 403–410 (2017). https://doi.org/10.7511/jslx201704001

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