PKK Library Search for 'au:"Eggleston,John M"'

A STUDY OF THE OPTIMUM VELOCITY CHANGE TO INTERCEPT AND RENDEZVOUS

By Eggleston,John M. Nasa, Washington, D.C. 1962 . 43 , Bound With Nasa Tn D-1021-1028 &1030

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A PRELIMINARY STUDY OF THE USE OF FINITE-THRUST ENGINES FOR ABORT DURING LAUNCH OF SPACE VEHICLES

By Mcgowan,William A. Nasa, Washington, D.C. 1961 . 23 , Bound With Nasa Tn D-701-12, 714-20

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A PRELIMINARY STUDY OF SOME ABORT TRAJECTORIES INITIATED DURING LAUNCH OF A LUNAR MISSION VEHICLE

By Eggleston,John M. Nasa, Washington, D.C. 1961 . 27 , Bound With Nasa Tm X-507-22,540-81,Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80

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A STUDY OF THE POSITIONS AND VELOSCITIES OF A SPACE STATION AND A FERRY VEHICLE DURING RENDEZVOUS AND RETURN

By Eggleston,John M. Nasa, Washington, D.C. 1961 . 39 , Bound With Nasa Tr R-80-86,88-90

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TRAJECTORY CONTROL FOR VEHICLES ENTERING THE EARTH`S ATMOSPHERE AT SMALL FLIGHT-PATH ANGLES

By Eggleston,John M. Nasa, Washington, D.C. 1961 . 29 , Bound With Nasa Tr R-81-88,90

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Analytical evaluation of a method of midcourse guidance for rendezvous with earth satellites [NASA TN D-883]

By Eggleston, John M.. Nasa Washington 1961 . 61p

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