The horizontal and the vertical launching of missiles like Space Shuttle, in the function of the differences in the starting weight at the fixed effective weight is given. The problem is mathematically modelled considering the variable starting angle (0 = horizontal launching, 90 = vertical launching). The results of this analysis has shown that the horizontal launching has following priorities: the effective weight is greater, the fuel consumption is lower, thw whole missile is lighter and cheaper. The stability criterion was decisive by the implementation of vertical launching procedure in the case of Space Shuttle. The second problem of horizontal launching is that lower orbites are arrived at the same end-velocity. (Jarc)
Komparativna analiza nekih slucajeva lansiranja raketoplana
Vergleichsanalyse einiger Faelle des lancierens der Raumfaehre
Comparative analysis of some cases in launching missiles
Tehnika ; 36 , 10 ; 943-945
1987
3 Seiten, 4 Bilder, 9 Quellen
Aufsatz (Zeitschrift)
Serbo-Croatian
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