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Aeronautical and Navigational Electronics, IRE Transactions on

Issue 1 • Date March 1958

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  • IRE Transactions on Aeronautical and Navigational Electronics

    Publication Year: 1958 , Page(s): c1
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  • IRE Professional Group on Aeronautical and Navigational Electronics

    Publication Year: 1958 , Page(s): c2
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  • Table of contents

    Publication Year: 1958 , Page(s): 1
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  • Frontispiece

    Publication Year: 1958 , Page(s): 2
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  • Cooling Airborne Electronics

    Publication Year: 1958 , Page(s): 3
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  • General Aspects of Cooling Airborne Electronic Equipment

    Publication Year: 1958 , Page(s): 4 - 9
    Cited by:  Papers (1)
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    A brief introduction and review is presented of the problems of protecting and cooling airborne electronic equipment in present and future high-speed devices. The thermal characteristics associated with high-speed flight of manned and unmanned vehicles are related to the thermal problems of irreversible electrical and magnetic components which possess upper bounds of temperature for reliable opera... View full abstract»

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  • Problems Arising in High-Speed Aircraft Due to Cooling Requirements of Electronic Equipment

    Publication Year: 1958 , Page(s): 10 - 15
    Cited by:  Papers (1)
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    High-speed aircraft require the successful operation of large quantities of electronic equipment. The problem of providing a suitable environment for such equipment is of interest to both airplane and electronic designers. A proposal is offered by which cooling provisions may be standardized for airplanes of widely varying performance. Basic design parameters for the development of such a system a... View full abstract»

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  • Temperature Limits, Ratings, and Natural Cooling Procedures for Avionic Equipment and Parts

    Publication Year: 1958 , Page(s): 15 - 24
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    The results of adequate cooling of electronic parts are gains in part life and reliability. An engineering compromise between ideal electronic part temperature and the thermal point of diminishing return must be evaluated not only with respect to desired life, but also in terms of the electronic circuit and cooling efficiencies. This paper outlines the flow of heat within, through, and from heat p... View full abstract»

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  • Forced-Air Direct-Contact Cooling of Airborne Electronic Equipment

    Publication Year: 1958 , Page(s): 25 - 29
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    A brief explanation of the principles of forced-air direct-contact cooling is given, and it is shown that the heat density of the electronic part being cooled determines essentially the range of applicability of this method. The discussion then progresses to cooling problems arising when this concept is applied to airborne electronic equipment. Several techniques are presented for obtaining high h... View full abstract»

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  • Cold Plate Design for Airborne Electronic Equipment

    Publication Year: 1958 , Page(s): 30 - 35
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    A solution to the problem of cooling certain types of high heat-dissipating airborne electronic equipment is the modification of the equipment chassis to incorporate a simple plate-fin heat exchanger, sometimes called a ¿cold plate.¿ In this paper equations for cold plates are developed and the effect of variations in fin configuration on performance are discussed. Theoretical and experimental r... View full abstract»

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  • Why and How Should High-Speed Aircraft Electronics Be Liquid Cooled?

    Publication Year: 1958 , Page(s): 36 - 46
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    Based on weight penality comparisons of ultimate heat sinks for electronic equipment cooling, the use of expendable evaporants and fuel is indicated for high supersonic flight. Centralized ram air should be the alternate coolant during subsonic flight. System integration is best accomplished with a recirculating liquid transfer system, which is relatively easy to control and which is characterized... View full abstract»

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  • An Evaporative-Gravity Technique for Airborne Equipment Cooling

    Publication Year: 1958 , Page(s): 47 - 52
    Cited by:  Papers (2)
    Save to Project icon | Request Permissions | Click to expandAbstract | PDF file iconPDF (1082 KB)  

    In airborne electronic packages, for either thermal or electrical reasons cooling air often is not ducted directly over the components but is passed through a heat exchanger. Consequently, the thermal path between the heat exchanger and the components must be of low impedance to result in efficient heat transfer. The high heat transfer coefficients obtainable as a liquid boils and condenses permit... View full abstract»

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  • Temperature Measurement

    Publication Year: 1958 , Page(s): 52 - 57
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    The quality of heat transfer data depends, to a large extent, on the accuracy of temperature measurements. Errors in temperature measurement may be due to calibration errors and/or application errors. This paper describes some common methods of temperature measurement and estimates the precision commonly attainable with these devices. The calibration of thermometers is also discussed. The problems... View full abstract»

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  • Radio Rack Cooling in Present Commercial Aircraft

    Publication Year: 1958 , Page(s): 58 - 63
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    Limited heat dissipation from the necessarily compact electronic equipment installations of airline aircraft has been a problem to commercial air carriers for many years. To deal with this problem, United Air Lines, in August, 1955, began equipping fleet aircraft with a forced air electronic equipment cooling system, with the following objectives: 1) improvement of electronic equipment reliability... View full abstract»

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  • Radiation Pattern Efficiencies of Some Suppressed HF Aircraft Antennas

    Publication Year: 1958 , Page(s): 64
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    First Page of the Article
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  • Abstracts

    Publication Year: 1958 , Page(s): 65
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  • PGANE News

    Publication Year: 1958 , Page(s): 66 - 68
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  • Contributors

    Publication Year: 1958 , Page(s): 69 - 70
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  • Suggestions to authors

    Publication Year: 1958 , Page(s): 71
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  • Institutional listings

    Publication Year: 1958 , Page(s): 71a
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Aims & Scope

This Transactions ceased publication in 1960. The new retitled publication is IEEE Transactions on Aerospace and Electronic Systems.

Full Aims & Scope