Cover image for Thermal Design of Aeroassisted Orbital Transfer Vehicles.
Thermal Design of Aeroassisted Orbital Transfer Vehicles.
Title:
Thermal Design of Aeroassisted Orbital Transfer Vehicles.
Author:
Nelson, H. F.
ISBN:
9781600863523
Personal Author:
Physical Description:
1 online resource (573 pages)
Series:
Progress in Astronautics and Aeronautics ; v.96

Progress in Astronautics and Aeronautics
Contents:
Cover -- Title -- Copyright -- Table of Contents -- Preface -- Editorial Committee -- Chapter I. Flowfield Analysis -- Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles -- Complete Flowfields Over Low- and Wide-Angle AOTV Conceptual Configurations -- AOTV Bluff Body Flow-Relaxation Algorithm -- Direct Simulation of Transitional Flow for Hypersonic Re-entry Conditions -- Chapter II. Trajectories -- Performance Evaluation of the Atmospheric Phase of Two Aeromaneuvering Orbital Transfer Vehicles -- Performance Aerodynamics of Aeroassisted Orbital Transfer Vehicles -- Multiple Pass Trajectories for an Aeroassisted Orbital Transfer Vehicle -- Impact of Atmospheric Uncertainties and Viscous Interaction Effects on the Performance of Aeroassisted Orbital Transfer Vehicles -- Analytical Characterization of AOTV Perigee Aerothermodynamic Regime -- Chapter III. Thermal Protection -- Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions -- Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept -- An AOTV Aeroheating and Thermal Protection Study -- Aerothermodynamic Heating Analysis of Aerobraking and Aeromaneuvering Orbital Transfer Vehicles -- Thermal Response of an Aeroassisted Orbital Transfer Vehicle with a Conical Drag Brake -- Low Lift-to-Drag Aerobrake Heat-Transfer Test at Mach 10 -- Calculation of Nonequilibrium Radiation in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles -- Air Radiation Revisited -- Chapter IV. Surface Effects -- Temperature-Dependent Reaction Rate Expressions for Oxygen Recombination -- Surface-Slip Equations for Low Reynolds Number Multicomponent Air Flow -- Comparison of Viscous Shock-Layer Heating Analysis with Shuttle Flight Data in Slip Flow Regime.

Problems of Rate Chemistry in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles -- Progress in Noncatalytic Surfaces for Metallic Heat Shields -- Author Index.
Local Note:
Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2017. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
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