Spacecraft Flight Mechanics

Author:

Sforza Pasquale M.

Publisher

Elsevier

Reference42 articles.

1. Allen, H. J. (1957). Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance. NACA TN 4048.

2. “Studies of high L/D ratio hypersonic configurations”, Fourth International Congress of the Aeronautical Sciences;Becker,1964

3. Spacecraft propulsion;Brown,1996

4. Modeling and computation of boundary layer flows;Cebeci,2005

5. Crawford, D. H., & McCauley, W. D. (1957). Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylinder in the langley 11-inch hypersonic tunnel at a mach number of 6.8. NACA Report 1323.

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