DocumentCode
952342
Title
Automatic Rocket Impact Predictor
Author
Duncan, Louis D.
Author_Institution
U. S. Army Signal Missile Support Agency, White Sands Missile Range, N. M.
Issue
42403
fYear
1960
Firstpage
243
Lastpage
245
Abstract
The ARIP was designed to improve rocket impact predictions. Previous procedures involved lag time in wind measuring which could not be fully accounted for in an x-time firing decision. This lag time assumes an importance in direct proportion to the magnitude of the wind weighting factors, which with some free flight rockets could be as large as 50 per cent of the total wind effect. Five Aerovane anemometer sensors distributed in the first 100-foot layer provide the data via mechanical and electronic coupling to a computer which has been preset for the ballistic values of a particular rocket. The computer output then activates an X-Y plotter which has been previously zeroed for all other cumulative displacement effects.
Keywords
Artificial satellites; Earth; Fluid flow measurement; Meteorology; Military computing; Missiles; Rockets; Testing; Vehicles; Wind forecasting;
fLanguage
English
Journal_Title
Military Electronics, IRE Transactions on
Publisher
ieee
ISSN
0096-2511
Type
jour
DOI
10.1109/IRET-MIL.1960.5008228
Filename
5008228
Link To Document