Effect of Material Mismatch on Static behavior of Flex Seal

Author:

Prakash D.,Balakrishna Murthy V.,Chandra Mohan R.,Karteek N.

Publisher

Elsevier BV

Subject

General Medicine

Reference13 articles.

1. John Herbert, Redlands, Frank J. Kovitch, Jr., River side, and Max McCorkle ‘Flexible Joint Means’, United States Patent no. 3,390,899, July 2, 1968.

2. E.Y. Wong, “Design, Fabrication, and Test of Omni directional Flexible Seals for Thrust Vector Control of Large Solid Rocket Motors”, NASA CR 72889, final report of Advanced Technical Operations, Sacramento, California. 10 June 1971.

3. Donate James R, “Solid rocket motor nozzle design sensitivity', AIAA.

4. Louis E. Miltenberger, “Thrust Vectoring Control System for Rocket Nozzles”, United States Patent no. 3,726,480, Apr. 10, 1973.

5. Stanley P. Desjardins, Jonathan W, Wilson, Alan R.Canifield. “Movable Thrust Nozzle for rockets”, United States Patent no. 3,696,999, Oct. 10, 1972.

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1. Design and Analysis of Solid Rocket Composite Motor Case Connector Using Finite Element Method;Polymers;2022-06-27

2. Harmonic Analysis of Flex Seal of Rocket Nozzle;IOP Conference Series: Materials Science and Engineering;2021-09-01

3. An experimental and numerical investigation of the effect of geometric parameters on the flexible joint nonlinear behavior for thrust vector control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-06-29

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