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pro vyhledávání: '"Sankaran Sathiyavageeswaran"'
Autor:
Lakshmi Venkatakrishnan, Karthikeyan Natarajan, Sankaran Sathiyavageeswaran, Jayaprakash N. Murugan
Publikováno v:
Journal of Spacecraft and Rockets. 58:1671-1680
Ignition overpressure (IOP) is a principal dynamic load experienced by a launch vehicle during liftoff. The IOP arises due to the sudden ignition of the solid rocket boosters (SRBs) of a launch veh...
Autor:
Jopaul K. Ignatius, Sankaran Sathiyavageeswaran, Venkata Ramakrishna Vankadari, Dileep Pasala
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811558610
Launch vehicle stages and sub-assemblies experience severe dynamic loads due to extreme launch vibration environment, thrust oscillations from solid motors, etc. Launch vehicle/spacecraft structural members and ground support structures suffer higher
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4bc4b04c9aba1588070df2c9bb8720f4
https://doi.org/10.1007/978-981-15-5862-7_25
https://doi.org/10.1007/978-981-15-5862-7_25
Autor:
Sankaran Sathiyavageeswaran, Jayaprakash N. Murugan, Karthikeyan Natarajan, Lakshmi Venkatakrishnan
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811556920
Launch vehicles experience peak vibro-acoustics stress during its captive firing or liftoff. The starting pressure rise transient in solid rocket motor chamber and subsequent flow of supersonic jet exhaust from the rocket nozzle generate high-intensi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3dc4898d38ac766c976fc8c4f1f61e1
https://doi.org/10.1007/978-981-15-5693-7_17
https://doi.org/10.1007/978-981-15-5693-7_17
Autor:
Lakshmi Venkatakrishnan, Sankaran Sathiyavageeswaran, Karthikeyan Natarajan, P. Suriyanarayanan
Publikováno v:
The Journal of the Acoustical Society of America. 144:1704-1704
The ignition of the solid rocket booster strap-on and the following IOP wave have a severe influence on the dynamic as well as the acoustic loads experienced by a launch vehicle during lift-off. The jet from the strap-on interacts with the core jet a