Titlebook: Integrated Design for Space Transportation System; B.N. Suresh,K. Sivan Book 2015 Springer Nature India Private Limited 2015 Aerodynamics.

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B. N. Suresh,K. Sivanner in which he has carried out his analysis which provides us with so many fresh perspectives. It is our intention that this new book series should provide those who work int he emerging discipline of mathematicseducation with an essential resource, and at a time of considerable concern about the w

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Space Transportation Systems: Introduction and Design Challenges,re onboard, and in such cases, the transportation systems have to meet the stringent requirements of human rating. Therefore, various aspects of the optimum and robust design of such STS satisfying all specified conditions are discussed in this chapter. The functional requirements of STS to transpor

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Integrated Design Aspects of Space Transportation System,) requirements analyses, (c) subsystems definition, (d) concept analyses and definition and (e) design. Design iterations are necessary to understand the interaction among subsystems, interfaces between various disciplines and relation between various design functions to meet the specified requireme

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Astrodynamics,luence the higher altitude orbital motions. Solutions for such motions are achieved by solving restricted three body problem, considering the Earth’s gravity force as the central gravity field whereas the perturbing gravitational force is from the third body such as Moon. Depending on the type of tr

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Space Transportation Requirements and Launching of Satellites, influence of Earth’s gravity field and aerodynamic drag during atmospheric flight phase causes the energy loss and to compensate these losses extra energy has to be provided. All these effects need to be considered for configuring STS to provide the necessary energy to the satellite. The satellites

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Space Transportation System Configuration, Staging and Performance,n optimum vehicle sizing and configuration, exhaustive trade-off studies are required. The studies have to address existing technologies and advanced new technologies with respect to performance improvements, performance requirements, demonstrations, process technologies, advanced technology develop

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Mission Design,ds and radio visibility for continuous tracking coverage during ascent phase are other essential parts of mission design. There are number of constraints like thermal loads on the spacecraft, the vehicle subsystems during ascent phase and jet plumes of reaction control system thrusters interacting w