7. Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays

7. Static Approach Application in Analysis of Gas-Dynamic Parameters in Launch Vehicle Vented Bays

Sirenko V. N., Il’enko P. V., Semenenko P. V.

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Kosm. teh. Raket. vooruž. 2017 (1); 43-47
 
Language: Russian
Annotation:
The methodology is proposed of probabilistic assessment of fulfilment of the requirements to gas dynamic parameters in launch vehicle vented bays in the cases when it is impossible to categorically ensure satisfaction of all limitations. By the example of Zenit LV it is shown that when using the statistic assessment, it is possible to considerably expand the launch vehicles application field from the viewpoint of ensuring required conditions in the spacecraft area.

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