Ballistic Missile and Space Electronics - 1st Edition - ISBN: 9780123955197, 9780323149334

Ballistic Missile and Space Electronics

1st Edition

Editors: C Morrow
eBook ISBN: 9780323149334
Imprint: Academic Press
Published Date: 1st January 1961
Page Count: 464
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Ballistic Missile and Space Technology, Volume II: Propulsion and Auxiliary Power Systems focuses on the exchange of technical information and ideas among engineers and scientists working on ballistic missile and space programs, including hypersonics, aerodynamic heating, material structures, propulsion, communications, computers, and bioastronautics.

The selection first offers information on the method for the interpretation of radiographic film of large solid propellant rockets and Soviet rocket propulsion. Discussions focus on applications, large Soviet liquid rocket engines, futuristic propulsion schemes, and Soviet rocket vehicles. The text then examines several criteria for determining the propellant bias for optimum performance of liquid propellant stages and precision determination of vacuum specific impulse from trajectory data.

The manuscript tackles charged metal droplets for propulsion, versatile ion source for propulsion, and electrogasdynamic analysis of ion jet neutralization. The book also reviews pulsed plasma accelerator employing electrodes and electrostatic lift for space vehicles. Topics include energy relations, electric induction effects, electrical charging of objects in space, and factors affecting the performance of plasma accelerators.

The selection is a primary reference for readers interested in space electronics.

Table of Contents



Propellant Technology

Application of the Density Ratio Method for the Interpretation of Radiographic Film of Large Solid Propellant Rockets

Soviet Rocket Propulsion

A Discussion of Several Criteria for Determining the Propellant Bias for Optimum Performance of Liquid Propellant Stages

Precision Determination of Vacuum Specific

Impulse from Trajectory Data

Ion Propulsion

Charged Metal Droplets for Propulsion

A Versatile Ion Source for Propulsion

Electrogasdynamic Analysis of Ion Jet Neutralization

A Pulsed Plasma Accelerator Employing Electrodes

Electrostatic Lift for Space Vehicles

Parametric Performance Studies of Electrical Thrust Generators for Space Applications

Heat Transfer and Materials

Experimental Determination of Solid Rocket

Nozzle Heat Transfer Coefficient

Auxiliary Power Systems

Nuclear Space Power - Snap II

A One-Megawatt Nuclear Electrical Power Plant for Space Applications

Bleed Gas from a Solid Propellant Rocket Engine to Power an Auxiliary Power Supply

Isotopic Fueled Thermionic Generators


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© Academic Press 1961
Academic Press
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About the Editor

C Morrow

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