Three durations of flight between different points of rocket trajectories are shown to be useful in the approximate computation of apogee. Data from a number of flights of known apogee are necessary to establish the effects of thrust and drag which are ignored in these computations. The results obtained from a number of Black Brant II flights are presented and discussed. (Author)
Some Results of Rocket Apogee Computation from Flight Duration
1965
2 pages
Report
No indication
English
Manned Spacecraft , Sounding rockets , Apogee , Flight , Time , Canada , Rocket trajectories , Thrust , Drag , Mathematical analysis , Reprints , Black Brant
Some results of rocket apogee computation from flight duration
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