Aerodynamic Stability of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle
暂无分享,去创建一个
[1] C. C. Horstman,et al. Free-flight measurements of aerodynamic viscous effects on lifting re-entry bodies. , 1967 .
[2] R. S. Crowder,et al. Apollo entry aerodynamics. , 1969 .
[3] Richard W. Powell,et al. Aerodynamic requirements of a manned Mars aerobraking transfer vehicle , 1991 .
[4] Donn B. Kirk,et al. Aerodynamic Behavior of the Viking Entry Vehicle: Ground Test and Flight Results , 1978 .
[5] William Willcockson,et al. Mars Pathfinder Heatshield Design and Flight Experience , 1999 .
[6] P. Levine,et al. Factors influencing the design and performance of mars entry vehicles. , 1965 .
[7] D. H. Greenshields,et al. Entry vehicles for space programs , 1969 .
[8] J. Gielis. A generic geometric transformation that unifies a wide range of natural and abstract shapes. , 2003, American journal of botany.
[9] H. Miura,et al. Aerobrake design studies for manned Mars missions , 1991 .