Experimentally Validated Thermal Model for Heat Transfer Through Structural Mounting of a Launch Vehicle

Author:

Joseph Reji,Choubey Sharmistha,Praveen Akula Akhil,Peter Jophy

Publisher

Begellhouse

Reference16 articles.

1. B. E. Franklin, Analysis and Design of Flight Vehicle Structures, Tri-state offset company, 1965.

2. W. Ley, K. Wittmann and W. Hallmann, 'Handbook of Space Technology,' W. Ley, K. Wittmann and W. Hallmann, Eds., John Willey & Sons Ltd., 2009.

3. C. M. Yohannan and D. Varkey, 'Design and Analysis of Corrugated Intertank,' International Journal of Engineering Research & Technology (IJERT), vol. 8, no. 4, April 2019

4. R. R. Kumar, R. Palaninathan, E. Kishor, G. S. Kumar and B. Deependran, 'Role of Thermal Contact Conductance on Sandwich-Type Metallic Thermal Protection System Profile,' AIAA Journal, vol. 50, no. 10, October 2012.

5. T. F. Johnson, R. Natividad, H. K. R. H and R. W. S. R, 'Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks,' AIAA Paper 2004-1931, Vols. NASA/TM-2005-213913, 2005.

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