1. Combustion possibility assessment for separating launch-vehicle components during atmospheric phase of descent trajectory. (June 2019) Authors: Trushlyakov, V.; Zharikov, K.; Davydovich, D. Journal: Acta astronautica Issue: Volume 159(2019) Page Start: 540 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
2. Improving of technical characteristics of launch vehicles with liquid rocket engines using active onboard de-orbiting systems. (September 2017) Authors: Trushlyakov, V.; Shatrov, Ya. Journal: Acta astronautica Issue: Volume 138(2017) Page Start: 19 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
3. Interaction of the Gas-vapor Mixture and Air on the Condition Drainage System of Space Launch Vehicles When Filling Cryogenic Propellant. (2017) Authors: Trushlyakov, V.; Zharikov, K. Journal: Procedia engineering Issue: Volume 174(2017) Page Start: 11 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
4. Method of heating of the separated parts of launch vehicle during the atmospheric phase of the descent trajectory. (April 2019) Authors: Trushlyakov, V.; Panichkin, A.; Lempert, D.; Shatrov, Ya.; Davydovich, D. Journal: Acta astronautica Issue: Volume 157(2019) Page Start: 1 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
5. The designing of launch vehicles with liquid propulsion engines ensuring fire, explosion and environmental safety requirements of worked-off stages. (February 2017) Authors: Trushlyakov, V.; Shatrov, Ya.; Sujmenbaev, B.; Baranov, D. Journal: Acta astronautica Issue: Volume 131(2017) Page Start: 96 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
6. The Use of Pyrotechnic Composition for Dispersing Fairings During Atmospheric Re-entry. (2017) Authors: Trushlyakov, V.; Davydovich, D. Journal: Procedia engineering Issue: Volume 174(2017) Page Start: 4 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
7. Thermodynamic model of the evaporation process of liquid residues of the propellant components in the orbital stage of the launch vehicle. (September 2018) Authors: Trushlyakov, V.; Kudentsov, V.; Matyushin, D.; Buryak, A. Journal: Acta astronautica Issue: Volume 150(2018) Page Start: 63 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗
8. Utilization of thermite energy for re-entry disruption of detachable rocket elements made of composite polymeric material. (September 2018) Authors: Monogarov, K.; Trushlyakov, V.; Zharikov, K.; Dron, M.; Iordan, Yu; Davydovich, D.; Melnikov, I.; Pivkina, A. Journal: Acta astronautica Issue: Volume 150(2018) Page Start: 49 Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗