MSC.Nastran Bibliography

Aircraft/Aerospace: Space Shuttle

Balderes, T.; Mason, P.; Ranalli, E.; Zalesak, J.; Levy, A. Shuttle Wing Panel Stability Analysis, NASTRAN: Users' Exper., pp. 137-170, September, 1975, (NASA TM X-3278). 

Bergmann, H. W.; Robinson, James C.; Adelman, Howard M. Analysis of a Hot Elevon Structure, NASTRAN: Users' Exper., pp. 163-180, September, 1971, (NASA TM X-2378). 

Bernstein, Murray; Mason, Philip W.; Zalesak, Joseph; Gregory, David J.; Levy, Alvin. NASTRAN Analysis of the 1/8-Scale Space Shuttle Dynamic Model, NASTRAN: Users' Exper., pp. 169-242, September, 1973, (NASA TM X-2893). 

Brillhart, Ralph; Hunt, David L.; Kammer, Daniel C.; Jensen, Brent M.; Mason, Donald R. Modal Survey and Test-Analysis Correlation of the Space Shuttle SRM, Proc. of the 6th Int. Modal Analysis Conf., pp. 863-870, February, 1988. 

Brolliar, Steve; Bracklin, Joe. Nonlinear Analysis of the Solid Rocket Booster Aft Skirt Welds Using a Modified MSC/NASTRAN Superelement Approach, The MSC 1992 World Users' Conf. Proc., Vol. II, Paper No. 52, May, 1992. 

Call, V.; Mason, D. Space Shuttle Redesigned Solid Rocket Booster Structural Dynamic Predictions and Correlations of Liftoff, AIAA/SAE/ASME/ASEE 26th Joint Propulsion Conf., Paper No. AIAA 90-2081, July, 1990. 

Davis, Craig. Structural Optimization of the Space Shuttle Advanced Solid Rocket Booster Thrust Vector Control System Test Bed, The MSC 1992 World Users' Conf. Proc., Vol. II, Paper No. 32, May, 1992. 

Dobrowski, Alvin D.; Rowe, James. COMMAND Analysis of the Shuttle Thermal Protection System Tiles, Proc. of the Conf. on Finite Element Methods and Technology, Paper No. 15, March, 1981. 

Furuike, T.; Yahata, S. Vehicle Structural Analysis - Pre and Post Processor Data Handling, NASTRAN: Users' Exper., pp. 697-708, September, 1971, (NASA TM X-2378). 

Gieseke, R. K. Modal Analysis of the Mated Space Shuttle Configuration, NASTRAN: Users' Exper., pp. 221-236, September, 1971, (NASA TM X-2378). 

Giles, Gary L.; Dutton, John H. Application of NASTRAN to the Analysis of a Space Shuttle Orbiter Structure, NASTRAN: Users' Exper., pp. 451-464, September, 1971, (NASA TM X-2378). 

Grooms, H. R.; Yahata, S. Space Shuttle-The Need for Substructuring, NASTRAN: Users' Exper., pp. 769-778, September, 1971, (NASA TM X-2378). 

Kammer, Daniel C.; Jensen, Brent M.; Mason, Donald R. Test-Analysis Correlation of the Space Shuttle Solid Rocket Motor Center Segment, J. of Spacecraft, Vol. 26, No. 4, pp. 266-273, March, 1988. 

Ko, William L.; Olana, Timothy. Effect of Element Size on the Solution Accuracies of Finite-Element Heat Transfer and Thermal Stress Analyses of Space Shuttle Orbiter, Sixteenth NASTRAN Users' Colloq., pp. 79-127, April, 1988, (NASA CP-2505). 

Lui, C. Y.; Mason, D. R. Space Shuttle Redesigned Solid Rocket Motor Nozzle Natural Frequency Variations with Burn Time, AIAA/SAE/ASME 27th Joint Propulsion Conf., Paper No. AIAA 91-2301, June, 1991. 

Murbach, Marcus S. Shuttle Tie Thermal Analysis via NASTRAN, MSC/NASTRAN Users' Conf. Proc., Paper No. 10, March, 1983. 

Palmieri, F. Nonlinear Dynamic Analysis of STS Main Engine Heat Exchanger, Proc. of the 15th MSC/NASTRAN Eur. Users' Conf., October, 1988. 

Shu, James; McCann, David. Use of MSC/NASTRAN for the Thermal Analysis of the Space Shuttle Orbiter Braking System, The MSC 1987 World Users Conf. Proc., Vol. I, Paper No. 25, March, 1987. 

Singh, Sudeep K.; Engelhardt, Charlie. Dynamic Analysis of a Large Space Structure Using External and Internal Superelements, The MSC 1991 World Users' Conf. Proc., Vol. I, Paper No. 27, March, 1991. 

Thornton, E. A. Application of NASTRAN to a Space Shuttle Dynamics Model, NASTRAN: Users' Exper., pp. 421-438, September, 1971, (NASA TM X-2378). 

Ujihara, B. H.; Dosoky, M. M.; Tong, E. T. Improving a NASTRAN Dynamic Model with Test Data Using Linwood, Tenth NASTRAN Users' Colloq., pp. 74-86, May, 1982, (NASA CP-2249). 

Ujihara, Ben H.; Tong, Edward T. Differential Stiffness Effects, Fourteenth NASTRAN Users' Colloq., pp. 166-172, May, 1986.