Propulsion Space Science and Space Exploration - 1st Edition - ISBN: 9780123956828, 9780323149648

Propulsion Space Science and Space Exploration

1st Edition

Editors: C Morrow
eBook ISBN: 9780323149648
Imprint: Academic Press
Published Date: 1st January 1961
Page Count: 456
Tax/VAT will be calculated at check-out Price includes VAT (GST)
30% off
30% off
30% off
30% off
30% off
20% off
20% off
30% off
30% off
30% off
30% off
30% off
20% off
20% off
30% off
30% off
30% off
30% off
30% off
20% off
20% off
54.95
38.47
38.47
38.47
38.47
38.47
43.96
43.96
43.99
30.79
30.79
30.79
30.79
30.79
35.19
35.19
72.95
51.06
51.06
51.06
51.06
51.06
58.36
58.36
Unavailable
Price includes VAT (GST)
× DRM-Free

Easy - Download and start reading immediately. There’s no activation process to access eBooks; all eBooks are fully searchable, and enabled for copying, pasting, and printing.

Flexible - Read on multiple operating systems and devices. Easily read eBooks on smart phones, computers, or any eBook readers, including Kindle.

Open - Buy once, receive and download all available eBook formats, including PDF, EPUB, and Mobi (for Kindle).

Institutional Access

Secure Checkout

Personal information is secured with SSL technology.

Free Shipping

Free global shipping
No minimum order.

Description

Ballistic Missile and Aerospace Technology, Volume III: Propulsion, Space Science and Space Exploration covers the proceedings of the Sixth Symposium on Ballistic Missile and Aerospace Technology, held in University of Southern California, Los Angeles, on August 29-31, 1961. This book contains three parts encompassing 18 chapters that explore the components of the propulsion systems, space science and experiments, and exploration of the moon and planets. Part I demonstrates first the advantage of using factorial experimental designs for a wide variety of missile propulsion design problems. This topic is followed by an outline of the component designs of rocket design simulators and a systematic method for determination of ablation rates in a corrosive environment. This part also presents an analysis of the open cycle technique for the removal of afterheat from a nuclear rocket and the design conditions for convergent nozzles. Part II describes the determination of the magnetic dipole of TIROS II, a spin-stabilized meteorological satellite, as well as a method for the acquisition of meteorological data, which provides information not readily available on a global scale and/or in real time. Part III discusses the principles of small payload dropping for space exploration; the geological problems involved in the location of a lunar base; and the features of a planetary entry vehicle. This concluding part also examines the degree of radiation safety resulting from different lunar spacecraft design and mission operations and the feasibility of placing and maintaining space vehicles in the earth-moon libration points. Aerospace engineers and scientists will find this book invaluable.

Table of Contents


Contributors

Preface

Propulsion Systems and Components

The Use of Statistical Design in Missile Propulsion Studies

Comparison of High-Altitude Simulators for Rocket Testing

A Preliminary Vehicle Installation Study for Project Sunflower

Practical Design Considerations and Their Implications for High Mass Fraction, Glass Filament Reinforced Plastic Case Motors

Autogenous Pressurization System Analysis of Propellant Tank Pressurization

A Systematic Method for Determination of Ablation Rates in a Corrosive Environment

Nuclear Rocket Engine Afterheat Removal

The Effect of Secondary Waste Heat on Space Vehicle Radiator Area

Curved Nozzles

Space Science and Experiments

Measuring the Magnetic Dipole of a Satellite

Extracting and Processing Meteorological Data Obtained from an IR/Radar Satellite

Geomagnetic Field Perturbations Due to Trapped Particles

Diffraction Limitations in Detecting Distant Targets by Their Shadows

Exploration of the Moon and Planets

Exploration of the Atmosphere of Venus with a Small Payload

Geological Problems in the Location of a Lunar Base

Planetary Landing and Observation Package

Evaluation of Space Radiation Safety Procedures in the Design and Operation of Some Early Manned Lunar Vehicles

The Use of the Earth-Moon Libration Points as Terminals for Space Stations

Details

No. of pages:
456
Language:
English
Copyright:
© Academic Press 1961
Published:
Imprint:
Academic Press
eBook ISBN:
9780323149648

About the Editor

C Morrow