Three durations of flight between different points of rocket trajectories are shown to be useful in approximate computation of apogee; data from number of flights of known apogee are necessary to establish effects of thrust and drag which are ignored in these computations; results obtained from flights of Black Brant II rockets, launched by National Research Council at Churchill Research Range, are presented and discussed.
Some results of rocket apogee computation from flight duration
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 12 , n 4
1966
3 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Failure Analysis of Solid Rocket Apogee Motors
NTIS | 1972
|Failure analysis of solid rocket apogee motors
NTRS | 1972
|