Aerodecelerator Performance of Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry
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[1] Kojiro Suzuki,et al. Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon , 2011 .
[2] Takashi Abe. A Self-consistent Tension Shell Structure for Application to Aerobraking Vehicle and its Aerodynamic Characteristics , 1988 .
[3] Kojiro Suzuki,et al. Reentry demonstration of deploy able and flexible aeroshell for atmospheric-entry vehicle using sounding rockets , 2012 .
[4] Kojiro Suzuki,et al. Hypersonic Wind Tunnel Test of a Flare-type Membrane Aeroshell for Atmospheric Entry Capsules , 2010 .
[5] Yasunori Nagata,et al. Attitude dynamics for flare-type membrane aeroshell capsule in reentry flight experiment , 2013 .
[6] Ian Gauld Clark,et al. Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator , 2009 .
[7] Takashi Abe,et al. Reentry Demonstration of Flare-type Membrane Aeroshell for Atmospheric Entry Vehicle using a Sounding Rocket , 2011 .
[8] R.D. Braun,et al. Supersonic Inflatable Aerodynamic Decelerators For Use on Future Robotic Missions to Mars , 2008, 2008 IEEE Aerospace Conference.
[9] Takashi Abe,et al. Examination of Radio Frequency Blackout for an Inflatable Vehicle During Atmospheric Reentry , 2014 .
[10] Henry S. Wright,et al. Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview , 2011 .
[11] Antony Jameson,et al. Lower-upper implicit schemes with multiple grids for the Euler equations , 1987 .
[12] Ryan A. Stephan,et al. Inflatable Re-Entry Vehicle Experiment (IRVE) Design Overview , 2005 .
[13] Takashi Abe,et al. Aerodynamic Heating Around Flare-Type Membrane Inflatable Vehicle in Suborbital Reentry Demonstration Flight , 2015 .
[14] Kazuhiko Yamada,et al. Structural Strength of Flare-Type Membrane Aeroshell Supported by Inflatable Torus against Aerodynamic Force , 2011 .
[15] J. Smagorinsky,et al. GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS , 1963 .
[16] C. Justus,et al. The NASA/MSFC Global Reference Atmospheric Model: 1999 Version (GRAM-99) , 1995 .
[17] Eiji Shima,et al. Parameter-Free Simple Low-Dissipation AUSM-Family Scheme for All Speeds , 2011 .
[18] David Evans,et al. Postflight Analysis of Inflatable Reentry and Descent Technology Blackout During Earth Reentry , 2009 .
[19] Reuben R. Rohrschneider,et al. Survey of Ballute Technology for Aerocapture , 2007 .
[20] Takashi Abe,et al. Suborbital reentry demonstration of inflatable flare-type thin-membrane aeroshell using a sounding rocket , 2015 .
[21] Atsushi Hashimoto,et al. Toward the Fastest Unstructured CFD Code "FaSTAR" , 2012 .
[22] Takashi Abe,et al. Aerodynamic Simulation of Inflatable Re-Entry Vehicle Performance in Low Speed Wind Tunnel , 2014 .
[23] Kazuhiko Yamada,et al. Asia Workshop on Computational Fluid Dynamics ( 6 AWCFD )-1-NUMERICAL SIMULATION OF HYPERSONIC FLOW AROUND FLARE-TYPE AEROSHELL WITH TORUS FRAME , 2009 .
[24] F. Menter,et al. Ten Years of Industrial Experience with the SST Turbulence Model , 2003 .
[25] Yusuke Takahashi,et al. Advanced validation of CFD-FDTD combined method using highly applicable solver for reentry blackout prediction , 2016 .
[26] Tomohiro Narumi,et al. Flare-Type Membrane Aeroshell Flight Test at Free Drop from a Balloon , 2009 .
[27] Christopher Lee Tanner. Aeroelastic analysis and testing of supersonic inflatable aerodynamic decelerators , 2012 .
[28] Caskey,et al. GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS I . THE BASIC EXPERIMENT , 1962 .