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dc.contributor.authorDivision 6 Staffen_US
dc.date.accessioned2009-06-17T14:01:06Z
dc.date.available2009-06-17T14:01:06Z
dc.date.issued1954-09-24en_US
dc.identifier6M-3076en_US
dc.identifier.urihttp://hdl.handle.net/1721.3/41275
dc.description.abstractThe simulation required for the investigation of the ability of the SAGE System to guide the F-99 Interceptor was completed and the results sorted with the help of IBM equipment. The results of 14,200 separate interceptions were presented in graphical form to evaluate the effects of quantization size, sampling rate, target altitude, target maneuver, target-height errors, as well as some modifications of the missile itself, including the effects of seeker control in the dive, and the size of the seeker search raster. A complete description of the results were published in 6M-3060.en_US
dc.language.isoenen_US
dc.publisherLincoln Laboratory - Division 6en_US
dc.relation.ispartofseriesDivision 6 Administrative Memo 6M-3076en_US
dc.relation.ispartofseriesProject Whirlwind Collection, MC665en_US
dc.titleSecret supplement to biweekly report for September 24, 1954en_US
dc.typeTechnical Reporten_US


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