Title Thermal design of aeroassisted orbital transfer vehicles / edited by H.F. Nelson

Published New York : American Institute of Aeronautics and Astronautics, ©1985

Click on the following:
ProQuest Ebook Central

Copies

Description 1 online resource Series Progress in astronautics and aeronautics ; v. 96 Progress in astronautics and aeronautics ; v. 96. 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 VehiclesMultiple 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 StudyAerothermodynamic 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 FlowComparison 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 Notes "Technical papers selected from the AIAA 22nd Aerospace Sciences Meeting, January 1984, and the AIAA 19th Thermophysics Conference, June 1984, and subsequently revised for this volume." Bibliography Includes bibliographical references and index Notes Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL English Print version record digitized 2010 HathiTrust Digital Library committed to preserve pda MiAaHDL Subject Orbital transfer (Space flight) Space vehicles -- Thermodynamics. Space vehicles -- Atmospheric entry. Space vehicles -- Thermodynamics -- Congresses Space vehicles -- Atmospheric entry -- Congresses Orbital transfer (Space flight) Space vehicles -- Atmospheric entry Space vehicles -- Thermodynamics Genre/Form Conference papers and proceedings Form Electronic book Author Nelson, H. F AIAA Aerospace Sciences Meeting (22nd : 1984 : Reno, Nev.) AIAA Thermophysics Conference (19th : 1984 : Snowmass, Colo.) LC no. 85003853 ISBN 9781600863523 1600863523 0915928949 9780915928941 1600865712 9781600865718

  Permalink