標題: Titlebook: Integrated Design for Space Transportation System; B.N. Suresh,K. Sivan Book 2015 Springer Nature India Private Limited 2015 Aerodynamics. [打印本頁] 作者: 實體 時間: 2025-3-21 17:20
書目名稱Integrated Design for Space Transportation System影響因子(影響力)
書目名稱Integrated Design for Space Transportation System影響因子(影響力)學科排名
書目名稱Integrated Design for Space Transportation System網(wǎng)絡公開度
書目名稱Integrated Design for Space Transportation System網(wǎng)絡公開度學科排名
書目名稱Integrated Design for Space Transportation System被引頻次
書目名稱Integrated Design for Space Transportation System被引頻次學科排名
書目名稱Integrated Design for Space Transportation System年度引用
書目名稱Integrated Design for Space Transportation System年度引用學科排名
書目名稱Integrated Design for Space Transportation System讀者反饋
書目名稱Integrated Design for Space Transportation System讀者反饋學科排名
作者: TIA742 時間: 2025-3-21 21:05
http://image.papertrans.cn/i/image/468485.jpg作者: DEMUR 時間: 2025-3-22 00:33 作者: FLINT 時間: 2025-3-22 06:33
978-81-322-3466-1Springer Nature India Private Limited 2015作者: MUMP 時間: 2025-3-22 11:13 作者: 壁畫 時間: 2025-3-22 16:22
Integrated Design Aspects of Space Transportation System,gation, guidance and control (NGC) systems, vehicle avionics, stage auxiliary systems, thermal systems, etc. It is essential to integrate the requirements of these systems to obtain the best design for the specified mission, and the design iterations are inevitable to arrive at a good design. The in作者: 寬宏大量 時間: 2025-3-22 17:03
Astrodynamics,ntral gravitational force and other disturbing forces. This chapter deals with astrodynamics which explains the motion of celestial bodies as well as human-made satellites under the influence of gravitational force field of celestial bodies and other external forces. Orbital motions of Low Earth Orb作者: 轎車 時間: 2025-3-22 23:10 作者: Melatonin 時間: 2025-3-23 04:34
Space Transportation System Configuration, Staging and Performance,the defined spacecraft into the specified orbit. To achieve these objectives, STS is configured with suitable propulsion systems to impart the required equivalent velocity to the satellite, after accounting for the various velocity losses the vehicle encounters during its mission. This chapter discu作者: Eructation 時間: 2025-3-23 08:46 作者: COMA 時間: 2025-3-23 13:23 作者: 頌揚本人 時間: 2025-3-23 17:22 作者: Dealing 時間: 2025-3-23 20:30
Propulsion Systems,e specified satellite. Different categories of propulsion systems such as chemical propulsion, electric propulsion, nuclear propulsion, solar sail, etc. are being used in various applications of space missions, depending on the requirements. For the boost phase with the present day technologies, che作者: tariff 時間: 2025-3-23 23:47 作者: 無底 時間: 2025-3-24 05:38
Structures and Materials,lant tanks, motor cases, payload fairing and interstage structures. The entire structure of the vehicle has to support all associated secondary elements like mechanisms, pyros, avionics, actuators, etc. Structures are classified as primary and secondary structures. Load-bearing structures like the s作者: corpuscle 時間: 2025-3-24 08:54
Thermal Systems and Design, and several other?sensitive elements. All thermal effects such as local heating rate and total heat load are to be analyzed in detail to understand the thermal loads during flight. Thermal environment of the vehicle and subsystems caused by aerodynamic heating depends mainly on their external confi作者: gerrymander 時間: 2025-3-24 13:12 作者: BLANC 時間: 2025-3-24 15:43 作者: Proponent 時間: 2025-3-24 22:35 作者: disciplined 時間: 2025-3-25 00:49
B. N. Suresh,K. Sivanarly, for the first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be作者: ovation 時間: 2025-3-25 04:59
B. N. Suresh,K. Sivanarly, for the first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be作者: 冷峻 時間: 2025-3-25 10:31
B. N. Suresh,K. Sivanthe first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be the first作者: Sigmoidoscopy 時間: 2025-3-25 12:27
B. N. Suresh,K. Sivanarly, for the first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be作者: 廢止 時間: 2025-3-25 16:37 作者: 撫慰 時間: 2025-3-25 22:27 作者: brother 時間: 2025-3-26 03:33
B. N. Suresh,K. Sivanarly, for the first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be作者: 講個故事逗他 時間: 2025-3-26 04:31
B. N. Suresh,K. Sivanthe first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be the first作者: 恃強凌弱 時間: 2025-3-26 11:28 作者: 極深 時間: 2025-3-26 13:49
B. N. Suresh,K. Sivanthe first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be the first作者: mitral-valve 時間: 2025-3-26 17:33
arly, for the first author. Both the Editorial Board and the Publisher are delightedt hat the first author in this series isw ell able to meet the challenge. Professor Freudenthal needs no introduction toanyone in the Mathematics Education field and it is particularly fitting that his book should be作者: 軟弱 時間: 2025-3-26 22:52 作者: Pde5-Inhibitors 時間: 2025-3-27 03:36 作者: Concomitant 時間: 2025-3-27 06:58 作者: 失誤 時間: 2025-3-27 12:01 作者: 讓步 時間: 2025-3-27 15:28 作者: LUT 時間: 2025-3-27 21:51 作者: Bureaucracy 時間: 2025-3-28 00:42
s should provide those who work int he emerging discipline of mathematicseducation with an essential resource, and at a time of considerable concern about the w978-90-277-2261-4978-0-306-47235-0Series ISSN 0924-4921 Series E-ISSN 2214-983X 作者: Angioplasty 時間: 2025-3-28 03:15 作者: 盲信者 時間: 2025-3-28 10:12 作者: Substitution 時間: 2025-3-28 10:52
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作者: 延期 時間: 2025-3-28 16:48 作者: 外貌 時間: 2025-3-28 22:47 作者: 啞劇 時間: 2025-3-29 02:22
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作者: 加花粗鄙人 時間: 2025-3-29 05:29
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作者: 奇怪 時間: 2025-3-29 07:52
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作者: Rotator-Cuff 時間: 2025-3-29 15:18
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作者: 有惡意 時間: 2025-3-29 15:49
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作者: Afflict 時間: 2025-3-29 22:04
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作者: ENDOW 時間: 2025-3-30 00:02 作者: CLAM 時間: 2025-3-30 06:18
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作者: 萬神殿 時間: 2025-3-30 11:15
Flight Mechanics,t the response of the vehicle and subsystems. To achieve the error-free design, the various models used for the vehicle, subsystems, environment, forces and moments generated by the respective systems as well as the dynamics of the systems under the influence of the forces and moments have to repres作者: Chagrin 時間: 2025-3-30 16:25 作者: STRIA 時間: 2025-3-30 18:05
Aerodynamics of Launch Vehicles,systems complicates the aerodynamic flows with unfavourable additional aerodynamic loads. The unsteady pressure fluctuations are due to shock oscillations during the transonic regime and local aeroacoustic loads due to flow separation because of protrusions form a major input for the qualification o作者: 釋放 時間: 2025-3-30 23:34 作者: 完成才能戰(zhàn)勝 時間: 2025-3-31 02:21
