- Sommer, S.C., Short, B.J., and Compton, D.L. “Free-Flight Measurements of Static and Dynamic Stability of Models of the Project Mercury Re-entry Capsule at Mach Numbers 3 and 9.5”, NASA TM X-373, 1960.
- Smith, R.P. “Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations And of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60”, NASA-Techdoc-19670022202, 1961.
- Reese, D.E., and Wehrend, W.R. “An Investigation of the Static and Dynamic Aerodynamic Characteristics of a Series of Blunt-Nosed Cylinder-Flare Models at Mach Numbers from 0.65 to 2.20, National Aeronautics and Space Administration”, NASA TM X-110, 1960.
- McDearmon, R., and Lawson, W. “Investigation of the Normal Force, Axial Force, and Pitching Moment Characteristics of Blunt Low Fineness Ratio Bodies of Revolution at a Mach number of 3.55”, National Aeronautics and Space Administration, Technical memorandum X-467, 1961.
- Compton, D.L. “Free-Flight Measurements of Drag and Static Stability for a Blunt-Nosed 10 Deg Half-Angle Cone At Mach Number 15”, technical memorandum X-507, 1961.
- Willidm, C., Moseley, Jr., Robert Moore, JK, undJuck E.H. “Stability Characteristics of the Apollo Command Module”, NASA TN-D-3890, 1967.
- William, C., Moseley, J., Ralph, E.G. and Jack, E.H. “Aerodynamic Stability Characteristics of the Apollo Command Module”, NASA TN-D-4688, 1968.
- Murphy, K. J., Bibb, K. L., Brauckmann, G. J., Rhode, M. N., Owens, B., Chan, D. T., Walker, E. L., Bell, J. H., and Wilson, T. M. “Orion Crew Module Aerodynamic Testing”, 29th AIAA Applied Aerodynamics Conference, Hawaii, 2011.
- Bibb, K., Walker, E., Brauckmann, G., and Robinson, P. “Development of the Orion Crew Module Static Aerodynamic Database”, Part II: Subsonic/Supersonic, 29th AIAA Applied Aerodynamics Conference, Hawaii, 2011.
- Stroud, K.J. and Klaus, D.M., “Spacecraft Design Considerations for Piloted Reentry and Landing”, NASA Technical reports, ID No. 20080026216, 2008.
- Mehta, R.C. “Computations of Flowfield over Reentry Modules at High Speed”, Chapter 16, Computational Simulations and Applications, InTech, 2011.
- Kazemba, C.D., Braum, R. D., Clark, I.G. and Schoenenberger, M. “Survey Of Blunt Body Dynamic Stability In Supersonic Flow”, AIAA Atmospheric Flight Mechanics Conference, Minneapolis, 2012.
- Ramezani, M., Abdolahi, S., Ebrahimi, M. “Estimation of the Aerodynamic Coefficients of Re-Entry Body in Continuum Flow”, The 13th Conference of Iranian Aerospace Society, Tehran, 2014. (in Persian)
- Fremaux, C., Johnson, R. “Subsonic Dynamic Stability Tests of a Sample Return Entry Vehicle”, 4th International Planetary Probe Workshop, ID 20060045567, United States, 2006.
- Nichols, J. and Nierengarten E. “Aerodynamic Characteristics Of Blunt Bodies”, JPL Technical report No. 32-677, Jet Propulsionon laboratory, California Institute of Technology, 1964.
- Abdolahi, S., Ramezani, M. Ebrahimi, M., “Investigation of the Effect of the Forebody Shape on the Center of the Pressure During Re-entry”, 3rd National & 1st International Conference on Applied Research Electrical, Mechanical & Mechatronics Engineering, Tehran, 2016 (in Persian) .
- Tahsini, A.M. “Conceptual Designe of Aerodynamic Heating of Spacecraft”, Technical Report No. ARI-93-10-NSLE1-AER-AHE-1-1, 2015. (in Persian)
- Fazilati, J. “Conceptual Designe of Energy Absorbent, Anti Shock and Heat Shield of Spacecraft”, Technical Report No. ARI-93-10-NSLE1-SEP-LSA-1-1, 2015 (in Persian).
- Ebrahimi, M. “Conceptual Designe of Recovery System of Spacecraft”, Technical Report No. ARI-93-10-NSLE1-REC-PAR-1-1, 2015 (in Persian).
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