Chemical Nonequilibrium Viscous Shock-Layer Analysis over Ablating Surface of Superorbital Re-Entry Capsule
スポンサーリンク
概要
- 論文の詳細を見る
The aerodynamic heating environment with ablation injection and the mass loss rate of the ablator under the superorbital re-entry condition of the MUSES-C sample return capsule are numerically studied by solving the Viscous shock-layer (VSL) equations wit
- 宇宙航空研究開発機構の論文
著者
-
Fujita K
Kyoto Univ. Kyoto Jpn
-
Abe T
Institute Of Space And Astronautical Science
-
Fujita Kazuhisa
Institute of Space and Astronautical Science (ISAS)
-
Abe Takashi
Institute of Space and Astronautical Science (ISAS)
-
Suzuki Kojiro
Department of Advanced Energy, Graduate School of Frontier Sciences, The University of Tokyo
-
Suzuki Kojiro
Department Of Advanced Energy Graduate School Of Frontier Sciences The University Of Tokyo
-
Suzuki K
Department Of Advanced Energy Graduate School Of Frontier Sciences The University Of Tokyo
-
Fujita Kazuhisa
Institute Of Space And Astronautical Science
-
Abe Takashi
Institute Of Space And Astronautical Science
関連論文
- Relationship between large tubules and dentin caries in human deciduous tooth
- Percentile curves for food acceptance response scores in assessing chewing functions in adults
- Assessment of Forebody and Backbody Radiative Heating Rate of Hypervelocity Reentry Capsule
- Influences of Transport Model on Heating Rate of Reentry Vehicles
- Chemical Nonequilibrium Viscous Shock-Layer Analysis over Ablating Surface of Superorbital Re-Entry Capsule
- Oveview of Research for Prediction of Aerodynamic Heating Environment during a Super-Orbital Reentry Flight of MUSES-C Reentry Capsule
- Low-Temperature Metalorganic Chemical Vapor Deposition of GaAs on Si by Alternate Gas Flow of the Source Materials
- Two-Dimensional Shape Optimization of Hypersonic Vehicles Considering Transonic Aerodynamic Performance
- Relationship between number of present teeth and nutritional intake in institutionalized elderly
- Effect of the Flow Non-uniformity on the Mixing Layer at the Interface of Parallel Supersonic Flows
- Experimental Study of Nonequilibrium Phenomena behind Strong Shock Waves Generated in Super-orbital Reentry Flight
- Utilization of Expansion Tube for MUSES-C Reentry Simulation
- Study for Dynamically Unstable Motion of Reentry Capsule
- Development of a Radiation Analysis Code for Hypervelocity Reentry Applications
- Rarefied Aerodynamics of MUSES-C Sample Return Capsule
- Trajectory-based Coupled Analysis of Viscous Shock Layer and Charring Material Ablation at Stagnation Point
- CROSS SECTION MEASUREMENTS AND THE ORBITING EFFECT IN SLOW CHARGE TRANSFER COLLISIONS OF HIGHLY CHARGED IONS
- Newly Devised Measuring Device for Vertical Maxillomandibular Registration
- VALUE AND LIMITATIONS OF PULSED DOPPLER ECHOCARDIOGRAPHY IN THE DIAGNOSIS OF PROSTHETIC VALVE DYSFUNCTION : Doppler, RI : I : 48 Annual Scientific Meeting, Japanese Circulation Society
- 105 A LIVING-DONOR LIVER TRANSPLANTATION RECIPIENT DIAGNOSED WITH DIABETES MELLITUS AFTER DISCONTINUATION OF IMMUNOSUPPRESSIVE THERAPY
- Diagnostic ability of MDCT to assess right hepatic artery invasion by perihilar cholangiocarcinoma with left-sided predominance
- Semi-quantification of Endolymphatic Size on MR Imaging after Intravenous Injection of Single-dose Gadodiamide: Comparison between Two Types of Processing Strategies
- Effect of Rarefied Gas Dynamics on Response of Air Data Sensor System for Atmospheric Entry Vehicle Flying at High Altitudes