Contact sensitivity analysis of a coupling pin for the nose cap of a launch re-entry vehicle

JBIS - Journal of the British Interplanetary Society

Volumn 61, Issue 1, 2008, Pages 14-19

  Ferraiuolo, Michele ^a   Riccio, Aniello ^a   Tescione, Domenico ^a   Gardi, Roberto ^a   Marino, Giuliano ^a  

^a ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

Author keywords

Finite element method; Sharp hot structures; Thermal protection system; Ultra high temperature ceramic

Indexed keywords

COEFFICIENTS OF THERMAL EXPANSIONS; FINITE ELEMENT MODELLING; MANUFACTURING COST; RE-ENTRY VEHICLES; SHARP HOT STRUCTURES; THERMAL PROTECTION SYSTEM; ULTRA-HIGH-TEMPERATURE CERAMICS; WING LEADING EDGES;

CERAMIC MATERIALS; SILICON CARBIDE; STRUCTURAL DESIGN; THERMAL EXPANSION;

FINITE ELEMENT METHOD;

EID: 37749040860     PISSN: 0007084X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (7)

1. G. Russo, "The PRORA-USV Programme", 4th European Symp. on Aerothermodynamics for Space Vehicles, CIRA, Capua (Italy) 8-11 October 2001, ESA-SP-487, pp. 37-48, March 2002
2. J.T. Dorsey, C.C. Poteet and K.E. Wurster, "Metallic Thermal Protection System Requirements, Environments and Integrated Concepts", Journal of Spacecrafts and Rockets, 41, pp.162-172, 2004.
3. M.L. Blosser, "Fundamental Modeling and Thermal Performances Issues for Metallic Thermal Protection System Concept", Journal of Spacecrafts and Rockets, 41, pp. 195-206, 2004.
4. Kelly H. Neale, D.R. Rummler and R. Jackson, "Research in Structures and Materials for Future Space Transportation Systems -An Overview", Journal of Spacecrafts and Rockets, 20, pp.89-96, 1983.
5. G. Russo and G. Marino, "The USV Program & UHTC Development", 4th European Workshop on Hot Structures and Thermal Protection Systems for Space Vehicles, Palermo (Italy), 26-29 November, 2002
6. ANSYS®, Reference Manual, Version 8.0.
7. "CMC FASTENERS FOR HOT STRUCTURES" H. Lange e M. Nickel.