Optimum interception of a ballistic missile at intermediate range

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dc.contributor.authorFaulkner, Frank David.
dc.contributor.departmentMathematics and Mechanics
dc.contributor.departmentMathematics and Mechanics
dc.date.accessioned2013-04-29T23:28:00Z
dc.date.available2013-04-29T23:28:00Z
dc.date.issued1961-10
dc.descriptionIssued simultaneously as Report No. DS-11641 Boeing Airplane Co. Seattle, Washingtonen_US
dc.description.abstractThe problem studied in this paper is that of obtaining optimum trajectories, such as the one for effecting interception of a target following a known course above the sensible atmosphere, with minimum fuel consumption, or in minimum time c A procedure is given for determining the trajectory on a digital computer, and some conditions are given for the corresponding optimum trajectories,. The methods apply generally to problems wherein the range and time are not too great and the terminal velocity is irrelevant.en_US
dc.description.urihttp://archive.org/details/optimumintercept00faul
dc.format.extent15 leaves ; 28 cm.en_US
dc.identifier.npsreportResearch Paper No. 29
dc.identifier.urihttps://hdl.handle.net/10945/31835
dc.publisherMonterey, CA; Naval Postgraduate School
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.subject.lcshBallistic missilesen_US
dc.titleOptimum interception of a ballistic missile at intermediate rangeen_US
dc.typeTechnical Reporten_US
dspace.entity.typePublication
relation.isDepartmentOfPublicatione933b810-c7ae-4aca-b25d-51d56c56a970
relation.isDepartmentOfPublication.latestForDiscoverye933b810-c7ae-4aca-b25d-51d56c56a970
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