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Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon Read chapter Read first chapter

2019 | OriginalPaper | Chapter

Research on Shock-Induced Aerothermodynamics for Future Planetary Explorations

Authors : K. Fujita, T. Suzuki, H. Takayanagi, T. Ozawa, S. Nomura, N. Takizawa, S. Matsuyama, A. Lemal, M. Mizuno

Published in: 31st International Symposium on Shock Waves 1

Publisher: Springer International Publishing

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Abstract

Researches on shock-induced aerothermodynamics are conducted at Chofu Aerospace Center (CAC) of Japan Aerospace Exploration Agency (JAXA) for future planetary explorations currently entertained in JAXA. The hyper-velocity shock tube (HVST) simulates the thermochemical properties in the shock layer of hypersonic systems in flight, while the hyper-velocity expansion tube (HVET) reproduces those in the wake region of the test model. The hypersonic rarefied wind tunnel (HRWT) enables us to directly measure the rarefied aerodynamics of hypersonic systems in transition flows. The light-gas gun (LGG) allows us to clearly understand the wake flow structure of capsules in supersonic flight, from which the parachute ejection conditions are determined. Numerical investigations of shock-induced aerothermodynamics are overviewed as well.

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previous chapter Shock Compression Spectroscopy Under a Microscope
next chapter Kinetic Shock Tubes: Recent Developments for the Study of Homogeneous and Heterogeneous Chemical Processes
Literature
1.
G. Yamada, T. Suzuki, H. Takayanagi, K. Fujita, Development of shock tube for ground testing reentry aerothermodynamics. Trans. Jpn. Soc. Aeronaut. Space Sci. 54, 51 (2011)CrossRef
2.
S. Nishimura, H. Takayanagi, S. Nomura, K. Fujita, M. Matsui, Speeding up of shock wave for future missions and spectroscopic measurement of strong shock wave, ISTS Paper 2015-e-32
3.
K. Fujita, H. Takayanagi, S. Matsuyama, K. Yamada, T. Abe, Assessment of convective and radiative heating for Jupiter Trojan sample return capsule, AIAA Paper 2014–2673
4.
T. Kawakami, S. Nomura, S. Nishimura, K. Fujita, M. Matsui, Electron temperature and number density measurement by fast-sweep Langmuir probe a head of shock waves, Paper 2C6, Annual meeting of the Japan Society for Aeronautical and Space Sciences (2016)
5.
K. Fujita, S. Matsuyama, T. Suzuki, Prediction of forebody and aftbody heat transfer rate for mars aerocapture demonstrator, AIAA Paper 2012–3001
6.
H. Takayanagi, S. Nomura, A. Lemal, K. Fujita, Measurement of carbon dioxide infrared radiation in the afterbody of a mars entry capsule, AIAA Paper 2017–1369
7.
T. Ozawa, K. Fujita, T. Suzuki, Development of an aerodynamic measurement system for hypersonic rarefied flows. Rev. Sci. Instrum. 86, 15105 (2015)CrossRef
8.
T. Ozawa, T. Suzuki, K. Fujita, Experimental and computational investigation of rarefied hypersonic aerodynamics. AIAA J. 53, 3327 (2015)CrossRef
9.
K. Fujita, A. Noda, Rarefied aerodynamics of a super low altitude test satellite, AIAA Paper 2009–3606
10.
T. Ozawa, T. Suzuki, K. Fujita, Pitot pressure analyses in CO2 condensing rarefied hypersonic flows. AIP Conf. Proc. 1786, 190010 (2016)CrossRef
11.
K. Fujita, Air intake performance of air breathing ion engines. J. Jpn. Soc. Aeronaut. Space Sci. 52, 514 (2004)
12.
S. Umetani, S. Nomura, H. Takayanagi, K. Fujita, M. Matsui, Development of two-stage light gas gun for investigation on dust sampler of mars aero-flyby sample collection, ISTS Paper 2015-e-31
13.
S. Nomura, K. Ito, S. Matsuyama, K. Fujita, Visualization of wake flows of supersonic mars entry capsule with light gas gun, ISTS Paper 2017-e-14 (2017)
14.
T. Matsuzaki, K. Ishida, Y. Watanabe, K. Miho, H. Itagaki, T. Yoshinaka, Construction and characteristics of the 750 kW arc heated wind tunnel, NAL-TM-760 (2001)
15.
H. Takayanagi, M. Mizuno, K. Fujii, T. Sakai, K. Fujita, Application of two-photon absorption laser-induced fluorescence to atomic species in JAXA 750kW arc heated wind tunnel. Trans. Jpn. Soc. Aeronaut. Space Sci. 57, 101 (2014)CrossRef
16.
K. Fujita, M. Mizuno, K. Ishida, T. Ito, Spectroscopic flow evaluation in inductively coupled plasma wind tunnel. J. Thermophys. Heat Transf. 22, 685 (2008)CrossRef
17.
K. Fujita, DSMC-QCT analysis of CO internal relaxation and dissociation by CO-O collisions. J. Jpn. Soc. Aeronaut. Space Sci. 57, 405 (2009)
18.
S. Matsuyama, K. Fujita, CFD application examples in development of a mars entry capsule, part I: hypersonic aerothermodynamics, Paper 1E12. The 49th Fluid Dynamics Conference/The 35th Aerospace Numerical Simulation Symposium (2017)
19.
S. Matsuyama, K. Fujita, CFD application examples in development of a mars entry capsule, part II: supersonic/subsonic aerodynamics, Paper 1E13. The 49th Fluid Dynamics Conference/The 35th Aerospace Numerical Simulation Symposium (2017)
20.
T. Ozawa, S. Nomura, T. Kawakami, A. Lemal, K. Fujita, Simulation of ionization and electronic excitation in hypersonic shock tube flows using DSMC, ISTS Paper 2017-e-18
21.
K. Fujita, T. Suzuki, M. Mizuno, K. Fujii, Comprehensive flow characterization in a 110-kW inductively-coupled-plasma heater. J. Thermophys. Heat Transf. 23, 840 (2009)CrossRef
22.
T. Suzuki, K. Fujita, T. Yamada, Y. Inatani, N. Ishii, Post-flight TPS analysis of Hayabusa reentry capsule. J. Spacecr. Rocket. 51, 96 (2014)CrossRef
23.
A. Lemal, K. Bando, S. Nomura, H. Takayanagi, K. Fujita, Prediction of nonequilibrium peak radiation during earth’s atmosphere suborbital reentry. J. Thermophys. Heat Transf. (in press, 2017a)
24.
A. Lemal, H. Takayanagi, S. Nomura, K. Fujita, Simulations of CO2 equilibrium infrared radiation measurements. J. Thermophys. Heat Transf. (in press, 2017b)
Metadata
Title
Research on Shock-Induced Aerothermodynamics for Future Planetary Explorations
Authors
K. Fujita
T. Suzuki
H. Takayanagi
T. Ozawa
S. Nomura
N. Takizawa
S. Matsuyama
A. Lemal
M. Mizuno
Copyright Year
2019
Book
31st International Symposium on Shock Waves 1

Print ISBN: 978-3-319-91019-2

Electronic ISBN: 978-3-319-91020-8

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-3-319-91020-8_6

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