Journal
Scientific and technical journal «Priborostroenie»
UDK629.191
Issue:3 (57)
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COORDINATES CORRECTION METHOD FOR AIMING MARK OF SPACE ROCKET
Annotation
The problem of aiming mark choice to ensure the rocket separated part fall in a given Earth surface area is considered. Analytical solution is presented which allows for determination of aiming mark with minimal prestarting correction of flight program.
Keywords
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