This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Structures Technology for NASP
Annotation ability available
Sector:
Language:
English
Abstract
This paper summarizes some of the efforts to advance hypersonic structures technology through the National Aero-Space Plane (NASP) Structures Technology Maturation Program. The ranges of expected structural loads and results from analysis and test activities are described. Topics briefly covered include shock impingement effects on aerothermal loads, actively-cooled structures concepts and test results to date for leading edges and panels, design and fabrication of a carbon-carbon control surface, a program for predicting performance of metal matrix composites, an analysis and sizing procedure for thermal structures, and some recently-developed test fixtures for seals, thermal insulation, and actively-cooled panels.
Recommended Content
Aerospace Material Specification | Insulation, Thermal Silica Fiber |
Technical Paper | Investigations of Composite Materials for Their Applications in Designs of Vehicles |
Aerospace Material Specification | Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 34, Class 4, Grade 294, Style 7781 |
Authors
Citation
Camarda, C. and Murrow, H., "Structures Technology for NASP," SAE Technical Paper 902008, 1990, https://doi.org/10.4271/902008.Also In
References
- Wieting, Allan R. Update on Aerothermal loads Studies Proceedings of the Fifth National Aero-Space Plane Technology Symposium Paper No. 34 VI October 17-21 1988
- Holden, Michael S. Wieting, Allan R. Glass, Christopher E. Experimental Study of Shock Wave Interference Heating on a Cylindrical Leading Edge NASA CR 1014 May 1988
- Glass, C. E. Wieting, A. R. Holden, M. S. Swept Shock-on-Lip, A Comparison of Analytical and Experimental Results NASP TM 1085 November 1989
- Mezines, S. A. Active Cooled Panel Test Results Proceedings of Seventh National Aero-Space Plane Technology Symposium Paper No. 95 VI October 23-27 1989
- Nowak, Robert J. Olsen, George C. Baker, Ned R. Holden, Michael S. Slot Film Cooling Parametric Study Proceedings of Sixth National Aero-Space Plane Technology Symposium Paper No. 78 VI April 24-28 1989
- Camarda, Charles J. McGowan, David M. Leading Edges for NASP - A Status Report NASP TM 1022 June 1988
- Camarda, Charles J. Masek, Robert V. Design, Analysis, and Tests of a Shuttle-Type Heat-Pipe-Cooled Leading Edge AIAA Journal of Spacecraft and Rockets 18 1 71 88 January-February 1981
- Ho, T. Matza, C. Medford, J. Watabe, S. Design Concept Study for NASP Control Surface NASA CR 181713 October 1988
- DeAngelis, V. Michael Coordinator Workshop on Correlation of Hot Structures Test Data with Analysis I II NASA Ames Dryden Research Facility November 15-17 1988
- Stewart, James R. Thareja, Rajiv R. Wieting, Allan R. Morgan, Ken Application of Finite Element and Remeshing Technique to Shock Interference on a Cylindrical Leading Edge AIAA Paper No. 88-0368 January 1988
- Gladden, Herbert J. Melis, Matthew E. Mockler, Theodore T. Tong, Mike Thermal/Structural Analyses of Several Hydrogen-Cooled Leading-Edge Concepts for Hypersonic Flight Vehicles NASA TM 102391 January 1990
- Percy, Wendy C. Fields, Roger A. Buckling of Hot Structures Proceedings of Eighth National Aero-Space Plane Technology Symposium Paper No. 38 VI March 26-30 1990
- Chamis, C. C. Hopkins, D. A. Thermoviscoplastic Nonlinear Constitutive Relationships for Structural Analysis of High Temperature Metal Matrix Composites NASA TM-87291 1985
- Scotti, Stephen J. Liquid-Metal Convective Cooling of NASP Engine Cowl Lips NASP TM 1069 July 1989
- Murrow, Harold N. Results of Studies on Test Requirements for Structural Certification NASP TM 1055 April 1989
- Steinetz, Bruce M. Dellacorte, Christopher Seal Concept and Material Performance Evaluation for the NASP Engine Proceedings of Seventh National Aero-Space Plan Technology Symposium Paper No. 60 VI October 23-27 1989
- Sparks, Larry Dube', Bill Slifka, Andrew High Thermal Gradient Calorimeter--Initial Test Results Proceedings of the Sixth National Aero-Space Plane Technology Symposium Paper No. 11 VI April 24-28 1989
- Moore, Thomas C., Sr. High-Temperature Strain Gage Installation Techniques for Carbon/Carbon with Silicon Carbide Surfaces NASP TM 1113 May 1990
- Powell, Clemens A. Zorurmski, William E. A Summary of Acoustic Loads Activities Proceedings of the Fifth National Aero-Space Plane Technology Symposium Paper No. 35 VI October 18-21 1988