Author: H. F. NelsonPublisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 592
Book Description
Thermal Design of Aeroassisted Orbital Transfer Vehicles
Author: H. F. NelsonPublisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 592
Book Description
Thermal Design of an Aero-assisted Orbital Transfer Vehicle
Author: Marcus S. MurbachPublisher:
ISBN:
Category : Reusable space vehicles
Languages : en
Pages : 104
Book Description
Thermal Design of Aeroassisted Orbital Transfer Vehicles
Author: Aerospace Sciences Meeting. 22, 1984, Reno, Nev..Publisher:
ISBN:
Category :
Languages : en
Pages : 566
Book Description
Design and Performance Analysis of an Aero-maneuvering Orbital-transfer Vehicle Concept
Author: Approximate Heat-transfer and Wall-temperature Calculations for Aeroassisted Orbital Transfer Vehicles
Author: Samir M. DeshpandePublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 174
Book Description
System Design Concepts and Requirements for Aeroassisted Orbital Transfer Vehicles
Author: M.I. CruzDesign Study of an Integrated Aerobraking Orbital Transfer Vehicle
Author: Aeroassisted Orbit Transfer Vehicle Trajectory Analysis
Author: Thermal Design Principles of Spacecraft and Entry Bodies
Author: Jerry BevansPublisher: Elsevier
ISBN: 0323142117
Category : Science
Languages : en
Pages : 876
Book Description
Progress in Astronautics and Aeronautics, Volume 21: Thermal Design Principles of Spacecraft and Entry Bodies is a collection of technical papers drawn mainly from the American Institute of Aeronautics and Astronautics Third Thermophysics Specialist Conference, held in Los Angeles, California on June 24-26, 1968 This volume is divided into three parts. The first part covers some aspects of thermal processes and design, including thermal analysis, convection, radiation, ablation, and space rocket effects. The second part surveys the remote measurements of the thermophysical and thermal radiation properties and joint conductance, which are critical criteria for space thermal design. The third part focuses on the space environmental effects on thermal coatings. This part deals first with the theory of radiative degradation, followed by a presentation of the laboratory measurements. This part also looks into the results of several flight experiments. This book will be of great value to thermophysicists, space engineers, and designers who are working in the space science fields.
Author: Thomas John McGuire