Abstract
This chapter introduces the historical and technical background to the technology that is required for entry, whether from orbit or beyond, into the atmosphere of the various celestial bodies within our solar system. It opens with a historical description of the forms of atmospheric entry technology that have been employed on various missions to date. The physical constraints on the design of atmospheric entry vehicles are then described in broad terms. The atmospheric properties of the various near-Earth planets are then described: these properties have distinct bearing on the type of technology that is appropriate for any particular mission. Following a discussion of the range of modern computational techniques that exist for dealing with the very difficult problem of simulating the behavior of atmospheric entry vehicles, the chapter closes with a short perspective on future developments in the field.
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References
Braun, R.D., and Manning, R.M., “Mars Entry, Descent and Landing Challenges,” Journal of Spacecraft and Rockets, Vol. 44, No. 2, 2007, pp. 310-323.
Anderson, J.D., Jr., Introduction to Flight, 4th ed., McGraw-Hill, Boston, 2000.
Cox, R.N., and Crabtree, L.F., Elements of Hypersonic Aerodynamics, Academic Press, New York, (1965).
Koppenwallner, G., “Fundamentals of Hypersonics: Aerodynamics and Heat Transfer.” In: Hypersonic Aerodynamics, Von Karman Institute for Fluid Dynamics, Saint Genese, Belgium, 1984.
Horvath, T.J., Zalameda, J.N., Wood, W.A., Berry, S.A., Schwartz, R.J., Dantowitz, R.F., Spisz, T.S., and Taylor J.C., “Global Infrared Observations of Roughness Induced Transition on the Space Shuttle Orbiter,” RTO Applied Vehicle Technology Panel Specialists’ Meeting, San Diego, USA, 2012.
Anonymous, Guide to Reference and Standard Atmosphere Models. AIAA G-003C-2010, 2010.
Powers, B.G., “Space Shuttle Longitudinal Landing Flying Qualities,” Journal of Guidance, Control and Dynamics, Vol. 9, No. 5, 1986, pp. 566-572.
Reese, J.M., Gallis, M.A., and Lockerby, D.A., “New directions in fluid dynamics: non-equilibrium aerodynamic and microsystem flows,” Philosophical Transactions of the Royal Society, Part A, Mathematical, Physical and Engineering Sciences, Vol. 361, 2003, pp. 2967-2988.
Lockerby D.A., Reese, J.M., and Struchtrup, H., “Switching criteria for hybrid rarefied gas flow solvers,” Proceedings of the Royal Society, Part A, Mathematical, Physical and Engineering Sciences, Vol. 465, 2009, pp. 1581-1598.
Wilmoth, R.G., Blanchard, R.C., and Moss, J.N., “Rarefied transitional bridging of blunt body aerodynamics,” In: Brun R et al. (eds.) 21st International Symposium of Rarefied Gas Dynamics, Marseille, France, 1998.
Macrossan, M.N., “Scaling parameters for hypersonic flow: correlation of sphere drag data,” In: Ivanov MS, Rebrov AK (eds.), 25th International Symposium on Rarefied Gas Dynamics, St. Petersburg, Russia, 2007.
Wilhite, A.W., Arrington, J.P., and McCandless, R.S., “Performance aerodynamics of aero-assisted orbital vehicles,” AIAA Paper 84-0406, 1984.
Mitcheltree, R.A., Wilmoth, R.G., Cheatwood, F.M., Brauckmann, G.J., and Greene, F.A., “Aerodynamics of Stardust Sample Return Capsule,” Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 429-435.
Desai, P.N., Mitcheltree, R.A., and Cheatwood, F.McN, “Entry Trajectory Issues for the Stardust Sample Return Capsule,” International Symposium on Atmospheric Reentry Vehicles and Systems, Arcachon, France, 1999.
Muylaert, J., Walpot, L., Rostand, P., Rapuc, M., Brauckmann, G., Paulson, J., Trockmorton, D., and Weilmuenster, K., “Extrapolation from wind tunnel to flight: Shuttle Orbiter aerodynamics,” AGARD-AR-319-Vol-2 Hypersonic Experimental and Computational Capability, Improvement and Validation, 1998.
Bertin, J.J., and Cummings, R.M., “Critical Hypersonic Aerothermodynamic Phenomena,” Annual Review of Fluid Mechanics, Vol. 38, 2006, pp. 129-157.
Greenshields, C.J., and Reese, J.M., “The structure of shock waves as a test of Brenner’s modifications to the Navier-Stokes equations,” Journal of Fluid Mechanics, Vol. 580, 2007, pp. 407-429.
Bird, G.A., Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon Press, Oxford, 1994.
Gallis, M.A., Bond, R.B., and Torczynski, J., “A kinetic-theory approach for computing chemical-reaction rates in upper-atmosphere hypersonic flows,” Journal of Chemical Physics, Vol. 131, No. 12, 2009, pp. 124311/1-124311/13.
Anderson, J.D., Jr., Hypersonic and High Temperature gas Dynamics, McGraw-Hill, New York, 1989.
Further Reading
Hirschel, E.H., and Weiland, C., Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, Progress in Astronautics and Aeronautics Series, American Institute of Aeronautics and Astronautics, 2009.
Murthy, T.K.S, Computational Methods in Hypersonic Aerodynamics, Fluid Mechanics and Its Applications, Springer, 2010.
Park, C., Nonequilibrium Hypersonic Aerothermodynamics, John Wiley & Sons, 1990.
Schweikart, L., and Hallion, R.P., The Hypersonic Revolution: Case Studies in the History of Hypersonic Technology, Vols. 1-3, Air Force History and Museums Program, U.S. Government Printing Office, 2003.
Vinh, N.X., Hypersonic and Planetary Entry Flight Mechanics, University of Michigan Press, 1980.
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Brown, R., Scanlon, T., Reese, J. (2014). Introduction to Atmospheric Transit. In: Macdonald, M., Badescu, V. (eds) The International Handbook of Space Technology. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-41101-4_5
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