Producing high quality eggs

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Effect of humidity and turning of eggs before incubation on hatching results

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The effect of angle of turning eggs during incubation on hatchability

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Effect of pre-incubation on the hatchability of chicken eggs

This bulletin reports on Department of Poultry Husbandry research project 40, Care of Hatching Eggs--P. [2].Digitized 2007 AES.Includes bibliographical references (page 12)

A bibliography on the search for extraterrestrial intelligence

This report presents a uniform compilation of works dealing with the search for extraterrestrial intelligence. Entries are by first author, with cross-reference by topic index and by periodical index. This bibliography updates earlier bibliographies on this general topic while concentrating on research related to listening for signals from extraterrestrial intelligence

Effect of multiple plane turning of eggs during incubation on hatchability

Includes bibliographical references (page [2])

Effect of holding temperature on hatchability of chicken eggs

This bulletin reports on Department of Poultry Husbandry research project 40, Care of Hatching Eggs--P. [2].Digitized 2007 AES.Includes bibliographical references (page 12)

Reducing spoilage in shell eggs by the use of fungicides

Digitized 2007 AES.Includes bibliographical references (pages 30-31)

Maintaining quality in shell eggs by heat treatment

Digitized 2007 AES.Includes bibliographical references (page 22)

Development of a rotating gravity gradiometer for earth orbit applications (AAFE)

Some preliminary mission studies are described along with the design, fabrication, and test of a breadboard model of an earth orbital, rotating gravity gradiometer with a design goal of 10 to the minus 11th power/sec sq (0.01 EU) in a 35-sec integration time. The proposed mission uses a Scout vehicle to launch one (or two orthogonally oriented) spin-stabilized satellites into a 330-km circular polar orbit some 20 days before an equinox. During the short orbital lifetime, the experiment would obtain two complete maps of the gravity gradient field with a resolution approaching 270 km (degree 75). The breadboard model of the gradiometer demonstrated a combined thermal and electronic noise threshold of 0.015 EU per data channel. The design changes needed to reduce the noise to less than 0.01 EU were identified. Variations of the sensor output signal with temperature were experimentally determined and a suitable method of temperature compensation was developed and tested. Other possible error sources, such as sensor interaction with satellite dynamics and magnetic fields, were studied analytically and shown to be small