Performance of Transpiration-Cooled Heat Shields for Reentry Vehicles
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Title
Performance of Transpiration-Cooled Heat Shields for Reentry Vehicles
Authors
Keywords
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Journal
AIAA JOURNAL
Volume 58, Issue 2, Pages 830-841
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2019-12-18
DOI
10.2514/1.j058515
References
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Note: Only part of the references are listed.- Influence of shock waves on supersonic transpiration cooling
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- Emissivity, catalycity and microstructural characterization of ZrB2–SiCfiber based UHTC at high temperature in a non-equilibrium air plasma flow
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- (2010) A. Gülhan et al. EXPERIMENTS IN FLUIDS
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- Stardust Entry Reconstruction
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- (2010) Hannah Boehrk et al. JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
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- (2009) Christopher O. Johnston et al. JOURNAL OF SPACECRAFT AND ROCKETS
- Optical Emission Spectroscopy During Plasmatron Testing of ZrB2-SiC Ultrahigh-Temperature Ceramic Composites
- (2009) Mickaël Playez et al. JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
- Transpiration Cooling Using Liquid Water
- (2009) Arnold Van Foreest et al. JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
- Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
- (2008) K. A. Heufer et al. AIAA JOURNAL
- Reentry Motion and Aerodynamics of the MUSES-C Sample Return Capsule
- (2008) Nobuaki ISHII et al. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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