Safety conditions for the separation of aerospace system stages

Heading: 
Space-Rocket Complexes
1Panov, AP, 2Gusynin, VP, 3Serdyuk, II, 4Karpov, AS
1Space Research Institute of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Kyiv, Ukraine
2State Space Agency of Ukraine, Kyiv, Ukraine
3State Enterprise «O.K. Antonov Aviation Science and Technology Complex», Kiev, Ukraine
4State Enterprise "Antonov", Kyiv, Ukraine
Kosm. nauka tehnol. 1999, 5 ;(1):108–111
https://doi.org/10.15407/knit1999.01.108
Publication Language: Russian
Abstract: 
Safety conditions are formulated for the separation of the stages of aerospace systems in the horizontal take-off. Control over the fulfillment of these conditions during the flight permits shock-free separation of the stages and prevention of a dangerous thermal and acoustic influence of top-stage rocket engines on the carrier plane.
Keywords: aerospace system, carrier plane, rocket engines
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References: 
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