Determination of the hazardous zones in the impact areas of separated parts of launch vehicles under the uncertain altitude of their initial destruction
|1Gladky, EG |
1Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
|Kosm. nauka tehnol. 2015, 21 ;(6):49–55|
|Section: Space Environment Monitoring and Space Debris|
|Publication Language: Russian|
The main hazard for ground facilities during launch vehicle (LV) nominal flight is in the separated parts (SP) impact areas. SP impact areas are specially allocated to ensure safety along LV ground tracks. The paper deals with a risk assessment model for facilities in the SP impact area, which takes into account the uncertainty of the altitude of SP initial destruction. Practical use of the developed model for determining hazardous area, within which the risks for people exceed the allowable level, is described. We show that the obtained hazardous area allows more adequate determination of the size of allocated area for SP impact.
|Keywords: altitude of initial destruction, fragmentation, hazardous area., impact area, launch vehicle, risk of damage facility, separated part|
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