Abstract
Sample return from asteroids and comets beyond the main belt is considered to be one of the most worthwhile future deep space missions [1]. Japan Aerospace Exploration Agency (JAXA) is currently entertaining a Jupiter Trojan sample return mission using a solar power sail [2], following the heritage of the Hayabusa sample return mission [3]. Because of high orbital energy corresponding to outer bodies, a sample return capsule (SRC) for such a future mission is expected to reenter the Earth’s atmosphere at velocities higher than 14 km/s and, hence, to encounter much severer aerodynamic heating environments than those of any past SRCs. Especially, the radiative heat transfer is considered to play a significant role in heat transfer processes in the shock layer, since the radiative heat transfer exponentially increases with the atmospheric flight velocity. To optimize the aerothermal design of the SRC and to minimize the mass of the thermal protection system (TPS) equipped with the SRC aeroshell, it is essentially required to accurately predict the aerothermal environments around the SRC along the reentry trajectory.
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References
Committee on the Planetary Science Decadal Survey: Vision and voyages for planetary science in the decade 2013–2022. The National Academies, Washington DC (2011)
Kawaguchi, J., Power Sail Working Group: A solar power sail mission for a Jovian orbiter and Trojan asteroid flybys. IAC-04-Q.2.A.03. In: 55th International Astronautical Congress, Vancouver, Canada (2004)
Kawaguchi, J., Fujiwara, A., Uesugi, T.: Hayabusa - Its technology and science accomplishment summary and Hayabusa-2. IAC-06-A3.5.2. In: 57th International Astronautical Congress, Valencia, Spain (2006)
Fujita, K., Takayanagi, H., Matsuyama, S., Yamada, K., Abe, T.: Assessment of convective and radiative heating for Jupiter Trojan sample return capsule. AIAA Paper 2014–2673. In: 11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Atlanta, USA (2014)
Detra, R.W., Kemp, N.H., Riddell, F.R.: Addendum to heat transfer to satellite vehicles reentering the atmosphere. Jet Propul. 27(12), 1256–1257 (1957)
Tauber, M.E., Sutton, K.: Stagnation-point radiative heating relations for earth and Mars entries. J. Spacecr. Rocket. 28(1), 40–42 (1991)
Fujita, K., Suzuki, T., Matsuyama, S., Yamada, T., Abe, S.: Numerical reconstruction of Hayabusa sample return capsule flight environments. AIAA Paper 2011–3477. In: 42nd AIAA Thermophysics Conference, Honolulu, USA (2011)
Fujita, K., Sumi, T., Yamada, T., Ishii, N.: Heating environments of a venus entry capsule in a trail balloon mission. J. Thermophys. Heat Transf. 20(3), 507–516 (2006)
Fujita, K., Matsuyama, S., Suzuki, T.: Prediction of forebody and aftbody heat transfer rate for Mars aerocapture demonstrator. AIAA Paper 2012–3001. In: 43rd AIAA Thermophysics Conference, New Orleans, USA (2012)
Park, C., Jaffe, R.L., Partridge, H.: Chemical-kinetic parameters of hyperbolic earth entry. J. Thermophys. Heat Transf. 15(1), 76–90 (2001)
Fujita, K., Mizuno, M., Ishida, K., Ito, T.: Spectroscopic flow evaluation in inductively coupled plasma wind tunnel. J. Thermophys. Heat Transf. 22(4), 685–694 (2008)
Fujita, K., Matsukawa, Y., Yamada, T., Ishii, N.: Evaluation of heat transfer rates of Venus entry capsules along flight trajectories. AIAA Paper 2006–3580. In: 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, San Francisco, USA (2006)
Nishimura, S., Takayanagi, H., Nomura, S., Fujita, K., Matsui, M.: Speeding up of shock wave for future missions and spectroscopic measurement of strong shock wave. ISTS Paper 2015-e-32. In: 30th International Symposium on Space Technology and Science, Kobe, Japan (2014)
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Fujita, K., Takayanagi, H., Matsuyama, S., Nishimura, S., Yamada, K., Abe, T. (2017). Experimental and Numerical Assessment of Aerothermal Environments About Jupiter Trojan Sample Return Capsule. In: Ben-Dor, G., Sadot, O., Igra, O. (eds) 30th International Symposium on Shock Waves 2. Springer, Cham. https://doi.org/10.1007/978-3-319-44866-4_10
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DOI: https://doi.org/10.1007/978-3-319-44866-4_10
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