Optimum interception of a ballistic missile at intermediate range

dc.contributor.author	Faulkner, Frank David.
dc.date	1961-10
dc.date.accessioned	2013-04-29T23:28:00Z
dc.date.available	2013-04-29T23:28:00Z
dc.date.issued	1961-10
dc.identifier.uri	https://hdl.handle.net/10945/31835
dc.description	Issued simultaneously as Report No. DS-11641 Boeing Airplane Co. Seattle, Washington	en_US
dc.description.abstract	The 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.uri	http://archive.org/details/optimumintercept00faul
dc.format.extent	15 leaves ; 28 cm.	en_US
dc.language.iso	en_US
dc.publisher	Monterey, California. Naval Postgraduate School	en_US
dc.rights	This 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.lcsh	Ballistic missiles	en_US
dc.title	Optimum interception of a ballistic missile at intermediate range	en_US
dc.type	Technical Report	en_US
dc.identifier.npsreport	Naval Postgraduate School (U.S.) Research paper ; no. 29.

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