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Spacecraft Systems Engineering [[electronic resource]]
| Spacecraft Systems Engineering [[electronic resource]] |
| Autore | Fortescue Peter |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Chicester, : Wiley, 2011 |
| Descrizione fisica | 1 online resource (725 p.) |
| Disciplina |
629.47
629.474 |
| Altri autori (Persone) |
SwinerdGraham
StarkJohn |
| Soggetto topico |
Astronautics - Systems engineering
Astronautics -- Systems engineering Materials -- Congresses Space vehicles - Design and construction Space vehicles -- Design and construction Structural dynamics -- Congresses TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-283-24036-X
9786613240361 1-118-30298-2 1-119-97100-4 1-119-97101-2 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
SPACECRAFT SYSTEMS ENGINEERING; CONTENTS; List of Contributors; Preface to the Fourth Edition; Preface to the Third Edition; Preface to the Second Edition; Preface to the First Edition; List of Acronyms; 1 INTRODUCTION; 1.1 Payloads and Missions; 1.2 A System View of Spacecraft; 1.3 The Future; 2 THE SPACECRAFT ENVIRONMENT AND ITS EFFECT ON DESIGN; 2.1 Introduction; 2.2 Pre-Operational Spacecraft Environments; 2.3 Operational Spacecraft Environments; 2.4 Environmental Effects on Design; 3 DYNAMICS OF SPACECRAFT; 3.1 Introduction; 3.2 Trajectory Dynamics; 3.3 General Attitude Dynamics
3.4 Attitude Motion of Specific Types of Spacecraft3.5 Oscillatory Modes; 3.6 In Conclusion; Appendix: The Inertia Matrix; 4 CELESTIAL MECHANICS; 4.1 Introduction; 4.2 The Two-body Problem-Particle Dynamics; 4.3 Specifying the Orbit; 4.4 Orbit Perturbations; 4.5 Restricted Three-body Problem; 5 MISSION ANALYSIS; 5.1 Introduction; 5.2 Keplerian Orbit Transfers; 5.3 Mission Analysis; 5.4 Polar LEO/Remote-Sensing Satellites; 5.5 Satellite Constellations; 5.6 Geostationary Earth Orbits (GEO); 5.7 Highly Elliptic Orbits; 5.8 Interplanetary Missions; 6 PROPULSION SYSTEMS; 6.1 Systems Classification 6.2 Chemical Rockets6.3 Spacecraft Propulsion; 6.4 Electric Propulsion; 7 LAUNCH VEHICLES; 7.1 Introduction; 7.2 Basic Launch Vehicle Performance and Operation; 7.3 Spacecraft Launch Phases and Mission Planning; 7.4 The Ariane 5 Launch Vehicle; 7.5 US Crewed Launch Systems; 7.6 Small Launchers and Reusable Sub-Orbital Vehicles; 7.7 Re-Entry into Earth's Atmosphere; 7.8 Specific Launch Costs and Reliability; 8 SPACECRAFT STRUCTURES; 8.1 Introduction; 8.2 Design Requirements; 8.3 Material Selection; 8.4 Analysis; 8.5 Design Verification; 8.6 Impact Protection; 8.7 Configuration Examples 8.8 The Future of Space Structures9 ATTITUDE CONTROL; 9.1 Introduction; 9.2 ACS Overview; 9.3 The Spacecraft Attitude Response; 9.4 Torques and Torquers; 9.5 Attitude Measurement; 9.6 ACS Computation; 10 ELECTRICAL POWER SYSTEMS; 10.1 Introduction; 10.2 Power System Elements; 10.3 Primary Power Systems; 10.4 Secondary Power Systems: Batteries; 10.5 Power Management, Distribution and Control; 10.6 Power Budget; 11 THERMAL CONTROL OF SPACECRAFT; 11.1 Introduction; 11.2 The Thermal Environment; 11.3 Thermal Balance; 11.4 Thermal Analysis; 11.5 Thermal Design; 11.6 Thermal Technology 11.7 Thermal Design Verification11.8 Example of Satellite Thermal Design-XMM/Newton; 12 TELECOMMUNICATIONS; 12.1 Introduction; 12.2 Techniques of Radio Communications; 12.3 The Communications Payload; 12.4 Conclusion; 13 TELEMETRY, COMMAND, DATA HANDLING AND PROCESSING; 13.1 Introduction; 13.2 System Architecture; 13.3 Telemetry Data Formatting; 13.4 Telecommand; 13.5 Communication Techniques and Protocols; 13.6 On-Board Data Handling (OBDH) and Processing; 13.7 Technology; 13.8 Tools and Controlling Documents; 14 GROUND SEGMENT; 14.1 Introduction; 14.2 The Ground Station 14.3 Flight Dynamics |
| Record Nr. | UNINA-9910139607303321 |
Fortescue Peter
|
||
| Chicester, : Wiley, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Spacecraft systems engineering [[electronic resource] /] / edited by Peter Fortescue, Graham Swinerd, John Stark
| Spacecraft systems engineering [[electronic resource] /] / edited by Peter Fortescue, Graham Swinerd, John Stark |
| Edizione | [4th ed.] |
| Pubbl/distr/stampa | Chicester, : Wiley, 2011 |
| Descrizione fisica | 1 online resource (xxxii, 691 p.) : ill |
| Disciplina | 629.474 |
| Altri autori (Persone) |
FortescuePeter W
SwinerdGraham StarkJohn P. W |
| Soggetto topico |
Space vehicles - Design and construction
Astronautics - Systems engineering |
| ISBN |
9781119971009 (e-book)
9780470750124 (hbk.) 1-283-24036-X 9786613240361 1-118-30298-2 1-119-97100-4 1-119-97101-2 |
| Classificazione | TEC002000 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1 INTRODUCTION -- 2 THE SPACECRAFT ENVIRONMENT AND ITS EFFECT ON DESIGN -- 3 DYNAMICS OF SPACECRAFT -- 4 CELESTIAL MECHANICS -- 5 MISSION ANALYSIS -- 6 PROPULSION SYSTEMS -- 7 LAUNCH VEHICLES -- 8 SPACECRAFT STRUCTURES -- 9 ATTITUDE CONTROL -- 10 ELECTRICAL POWER SYSTEMS -- 11 THERMAL CONTROL OF SPACECRAFT -- 12 TELECOMMUNICATIONS -- 13 TELEMETRY, COMMAND, DATA HANDLING AND PROCESSING -- 14 GROUND SEGMENT -- 15 SPACECRAFT MECHANISMS -- 16 SPACECRAFT ELECTROMAGNETIC COMPATIBILITY ENGINEERING -- 17 ASSEMBLY, INTEGRATION AND VERIFICATION -- 18 SMALL SATELLITE ENGINEERING AND APPLICATIONS -- 19 PRODUCT ASSURANCE -- 20 SPACECRAFT SYSTEM ENGINEERING -- INDEX. |
| Record Nr. | UNINA-9910677937903321 |
| Chicester, : Wiley, 2011 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho
| Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho |
| Pubbl/distr/stampa | [S.l.], : Bentham e Books, [2010] |
| Descrizione fisica | 1 online resource (194 p.) |
| Disciplina | 629 |
| Altri autori (Persone) | HoSook-Ying |
| Soggetto topico |
Space vehicles - Design and construction
Structural analysis (Engineering) |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60805-024-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 01 Title.pdf; 02 Cover Page; 04 eBooks End User License Agreement-Website; 05 Content; 06 FOREWORD by Dr CT Liu; 07 Preface; 08 List of Contributors; 09 Nomenculture; 10 chapter 1 Fatigue life assessment paper V2a; 11 chapter 2 Generic design procedures for the repair of acoustically damaged panels Final a2; 12 chapter 3 aerothermostructural analysis_j; 13 chapter 4 Ebook-Zhuang20100202b; 14 chapter 5 Fracture Andrei and John 15a; 15 chapter 6 NDE solid rocket3; 16 chapter 7 solid rocket SIA5a; 17 INDEX |
| Record Nr. | UNINA-9910460145903321 |
| [S.l.], : Bentham e Books, [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho
| Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho |
| Pubbl/distr/stampa | [S.l.], : Bentham e Books, [2010] |
| Descrizione fisica | 1 online resource (194 p.) |
| Disciplina | 629 |
| Altri autori (Persone) | HoSook-Ying |
| Soggetto topico |
Space vehicles - Design and construction
Structural analysis (Engineering) |
| ISBN | 1-60805-024-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 01 Title.pdf; 02 Cover Page; 04 eBooks End User License Agreement-Website; 05 Content; 06 FOREWORD by Dr CT Liu; 07 Preface; 08 List of Contributors; 09 Nomenculture; 10 chapter 1 Fatigue life assessment paper V2a; 11 chapter 2 Generic design procedures for the repair of acoustically damaged panels Final a2; 12 chapter 3 aerothermostructural analysis_j; 13 chapter 4 Ebook-Zhuang20100202b; 14 chapter 5 Fracture Andrei and John 15a; 15 chapter 6 NDE solid rocket3; 16 chapter 7 solid rocket SIA5a; 17 INDEX |
| Record Nr. | UNINA-9910785590303321 |
| [S.l.], : Bentham e Books, [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho
| Structural failure analysis and prediction methods for aerospace vehicles and structures [[electronic resource] /] / edited by Sook-Ying Ho |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | [S.l.], : Bentham e Books, [2010] |
| Descrizione fisica | 1 online resource (194 p.) |
| Disciplina | 629 |
| Altri autori (Persone) | HoSook-Ying |
| Soggetto topico |
Space vehicles - Design and construction
Structural analysis (Engineering) |
| ISBN | 1-60805-024-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 01 Title.pdf; 02 Cover Page; 04 eBooks End User License Agreement-Website; 05 Content; 06 FOREWORD by Dr CT Liu; 07 Preface; 08 List of Contributors; 09 Nomenculture; 10 chapter 1 Fatigue life assessment paper V2a; 11 chapter 2 Generic design procedures for the repair of acoustically damaged panels Final a2; 12 chapter 3 aerothermostructural analysis_j; 13 chapter 4 Ebook-Zhuang20100202b; 14 chapter 5 Fracture Andrei and John 15a; 15 chapter 6 NDE solid rocket3; 16 chapter 7 solid rocket SIA5a; 17 INDEX |
| Record Nr. | UNINA-9910825637303321 |
| [S.l.], : Bentham e Books, [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Technology of lunar soft lander / / Deng-Yun Yu, Ze-Zhou Sun, He Zhang
| Technology of lunar soft lander / / Deng-Yun Yu, Ze-Zhou Sun, He Zhang |
| Autore | Yu Deng-Yun |
| Pubbl/distr/stampa | Gateway East, Singapore : , : Springer, , [2021] |
| Descrizione fisica | 1 online resource (xxviii, 565 pages) : illustrations |
| Disciplina | 629.47 |
| Collana | Space Technology Library |
| Soggetto topico | Space vehicles - Design and construction |
| ISBN | 981-15-6580-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Foreword By Fanpei Lei -- Foreword By Peijian Ye -- Preface I -- Preface II -- Contents -- Acronyms -- 1 Introduction -- 1.1 Significance of and General Approaches to Lunar Exploration -- 1.1.1 Significance of Lunar Exploration -- 1.1.2 General Approaches to Lunar Exploration -- 1.2 Status of Lunar Lander Technology Development Outside China -- 1.2.1 Development of Lunar Lander Technology in the Soviet Union [1, 14] -- 1.2.2 Development of Lunar Lander Technology in the United States [1, 6−13] -- 1.3 China's Lunar Exploration Program -- 1.3.1 General Plan of CLEP -- 1.3.2 Brief Information on Chang'E Probes -- 1.4 Technical Challenges to Development of Lunar Lander [5, 14, 16] -- 1.5 Summary -- References -- 2 Environment Analysis of Lunar Soft Landing Exploration -- 2.1 Introduction -- 2.2 Lunar Radiation Environment -- 2.2.1 Galactic Cosmic Rays -- 2.2.2 Solar Energetic Particles -- 2.2.3 Plasma Environment in Lunar Orbit -- 2.3 Lunar Thermal Environment -- 2.3.1 Solar Radiation -- 2.3.2 Lunar Albedo -- 2.3.3 Lunar Radiation -- 2.3.4 Earth Albedo -- 2.3.5 Earth Radiation -- 2.4 Lunar Landform and Topography -- 2.4.1 Lunar Landform -- 2.4.2 Lunar Topography -- 2.5 Lunar Soil and Dust -- 2.5.1 Physical Properties -- 2.5.2 Mechanical Properties -- 2.5.3 Electromagnetic Properties -- 2.6 Other Lunar Environments -- 2.6.1 Lunar Gravity -- 2.6.2 Near Vacuum Environment of the Moon -- 2.6.3 Illumination Environment on the Lunar Surface -- 2.7 Summary -- References -- 3 System Design of Lunar Lander -- 3.1 Introduction -- 3.2 Principles of System Design -- 3.3 Mission Analysis -- 3.3.1 Analysis of Mission Characteristics -- 3.3.2 Analysis of Landing Site -- 3.3.3 Analysis of Flight Profile -- 3.3.4 Analysis of Environment Effects -- 3.3.5 Analysis of Payload Configuration -- 3.4 Trajectory Design -- 3.4.1 Overview of Flight Profile.
3.4.2 Constraints of Trajectory Design -- 3.4.3 Determination of Landing Window -- 3.4.4 Analysis of Circumlunar Orbit -- 3.4.5 Determination of LTO -- 3.4.6 Analysis of Launch Window -- 3.5 System Components and Specifications -- 3.5.1 System Components -- 3.5.2 Major System Specifications -- 3.5.3 Propellant Budget -- 3.6 System Configuration Design -- 3.6.1 Design Principles -- 3.6.2 System Configuration -- 3.7 Planning of TT& -- C Link -- 3.8 Design of Powered Descent and Soft Landing -- 3.8.1 Initial Status and Setup of Powered Descent -- 3.8.2 Process of Powered Descent and Soft Landing -- 3.8.3 Landing Cushion -- 3.8.4 Downloading of Descent Images -- 3.9 Analysis and Simulation of Landing Stability -- 3.10 Summary -- References -- 4 Structure and Mechanism Technology of Lunar Lander -- 4.1 Introduction -- 4.2 Structural and Mechanism Features of Lunar Lander -- 4.2.1 Structural Features of Lunar Lander -- 4.2.2 Mechanism Features of Lunar Lander -- 4.3 Design and Verification of Lunar Lander Structure -- 4.3.1 Structural Design -- 4.3.2 Structural Analysis of Lunar Lander -- 4.3.3 Structural Tests of Lunar Lander -- 4.4 Mechanism Design and Verification of Lunar Lander -- 4.4.1 Solar Panel Mechanism -- 4.4.2 Separation Mechanism for Lunar Rover -- 4.4.3 Transfer Mechanism for Lunar Rover -- 4.5 Summary -- References -- 5 Thermal Control Technology of Lunar Lander -- 5.1 Introduction -- 5.2 Current Status of Thermal Control Technology -- 5.3 Thermal Technical Characteristics -- 5.3.1 Design Constraints -- 5.3.2 Technical Characteristics -- 5.4 Design Methodology -- 5.4.1 Principles of Thermal Design -- 5.4.2 Design of Thermal Control -- 5.4.3 Thermal Analysis and Calculation -- 5.5 Typical Technologies -- 5.5.1 Variable Thermal Conductive Technology -- 5.5.2 Protection Technology for High-Temperature Engine. 5.5.3 RHU Application Technology -- 5.5.4 Two-Phase Fluid Loop Technology -- 5.6 Testing and Verification -- 5.6.1 Thermal Balance Test of Lunar Lander -- 5.6.2 VCHP Test -- 5.6.3 Vacuum Thermal Insulation Testing of High-Temperature Heat Shield -- 5.6.4 Two-Phase Fluid Loop Test -- 5.6.5 Flight Testing on Orbit -- 5.7 Summary -- References -- 6 Power Technology of Lunar Lander -- 6.1 Introduction -- 6.2 Status of Power Supply Technology Development -- 6.3 Mission Requirements and Characteristics -- 6.3.1 Functional Requirements -- 6.3.2 Performance Requirements -- 6.3.3 Mission Characteristics and Analysis -- 6.4 Design Methodology -- 6.4.1 Design Principles -- 6.4.2 Illumination Conditions -- 6.4.3 Lightweight Design -- 6.4.4 Analysis of Space Environmental Effects -- 6.4.5 Energy Balance Analysis -- 6.4.6 Analysis of Power System Architecture -- 6.5 Typical Technology -- 6.5.1 Design of Power Controller -- 6.5.2 Design of Battery Pack -- 6.5.3 Design of Solar Cell Circuits -- 6.5.4 Design of Hibernation and Awakening Control -- 6.5.5 Power Supply Reuse Between Probes -- 6.6 Testing and Verification -- 6.6.1 Contents of Verification -- 6.6.2 Verification of Hibernation and Awakening -- 6.6.3 Verification of Large Incident Angle for Solar Cells -- 6.6.4 Extreme Temperature Verification of Solar Cells Performance -- 6.7 Summary -- References -- 7 Guidance, Navigation and Control Technology of Lunar Lander -- 7.1 Introduction -- 7.2 Development of GNC Technology -- 7.3 Analysis of Technical Characteristics -- 7.4 Design Methodology -- 7.4.1 System Configuration -- 7.4.2 Operational Modes -- 7.4.3 Component Design -- 7.4.4 Software Design [7] -- 7.4.5 Autonomous Failure Diagnosis and Handling Logic Design -- 7.5 Typical Technology -- 7.5.1 Procedure of GNC Powered Descent Phase [8] -- 7.5.2 Powered Descent Trajectory Design. 7.5.3 Navigation Method for Powered Descent Phase -- 7.5.4 Guidance Law Design of Powered Descent Process -- 7.5.5 Hazard Detection and Safe Landing Area Selection Method [9] -- 7.5.6 Attitude Control Method for Powered Descent Process [10] -- 7.6 Testing and Verification -- 7.6.1 Key Navigation Sensors Calibration -- 7.6.2 GNC Subsystem Flight Testing -- 7.6.3 Hardware-in-the-Loop Test [11] -- 7.7 Summary -- References -- 8 Propulsion Technology of Lunar Lander -- 8.1 Introduction -- 8.2 Development Status [2, 3] -- 8.3 Design Constraints and Analysis -- 8.3.1 Configurational Constraints -- 8.3.2 Functional Requirements -- 8.3.3 Technical Specification Requirements [4] -- 8.3.4 Flight Environment -- 8.3.5 Long-Term Storage Environment on Lunar Surface -- 8.4 Propulsion Subsystem Design [5-7] -- 8.4.1 Fundamental Design Conditions -- 8.4.2 Determination of Major Specifications of Propulsion Subsystem -- 8.4.3 Design of Propellant Feed System [4] -- 8.4.4 Electronics Design of Propulsion Subsystem -- 8.4.5 AIT Design of Propulsion Subsystem -- 8.4.6 Major Components Design for Propulsion Subsystem -- 8.4.7 Ground Test and Propellant Filling of Propulsion Subsystem -- 8.5 Testing and Verification of Propulsion Subsystem -- 8.5.1 Subsystem Ground Hot Firing -- 8.5.2 Throttling Engine Test -- 8.5.3 Propellant Tank Test -- 8.5.4 Long-Term Pressure-Bearing Storage Test of Gas Tank -- 8.5.5 Propellant Filling Test -- 8.6 Summary -- References -- 9 OBDH Technology of Lunar Lander -- 9.1 Introduction -- 9.2 Development Status -- 9.3 Analysis of Technical Characteristics -- 9.3.1 Mission Analysis -- 9.3.2 Constraints -- 9.4 Design Methodology -- 9.4.1 Principles of Design -- 9.4.2 System Architecture and Configuration -- 9.4.3 Miniaturized and Integrated System Design -- 9.4.4 Bus Network Design -- 9.4.5 Information Management Design. 9.4.6 Design of Spacecraft Autonomous Management -- 9.4.7 Reliable Design of Highly-Integrated and Lightweight Devices -- 9.4.8 Software Design -- 9.5 Testing and Verification -- 9.5.1 Simulation and Test Environment for OBDH Subsystem -- 9.5.2 Content of Verification -- 9.6 Summary -- References -- 10 TT& -- C and Telecommunication Technology of Lunar Lander -- 10.1 Introduction -- 10.2 Development Status -- 10.3 Analysis of Technical Characteristics -- 10.3.1 Requirements -- 10.3.2 Mission Characteristics -- 10.3.3 Design Constraints -- 10.4 Design of Telemetry/Telecommand and Telecommunication Technology -- 10.4.1 Overview -- 10.4.2 Design Method -- 10.4.3 Telemetry/Telecommand and Telecommunication of Lunar Lander to Ground -- 10.4.4 Telecommunication Between Lunar Lander and Lunar Rover -- 10.5 Testing and Verification -- 10.5.1 Compact Field Test -- 10.5.2 Testing of Interface to Ground System -- 10.5.3 UHF Field Test -- 10.6 Summary -- References -- 11 Landing Gear Technology of Lunar Lander -- 11.1 Introduction -- 11.2 Development Status -- 11.3 Configuration and Technical Features of Landing Gear System -- 11.4 Common Cushion Methods and Their Features -- 11.4.1 Cellular Material Deformation -- 11.4.2 Deformation of Thin-Walled Metal Tube -- 11.4.3 Hydraulic Damping -- 11.4.4 Tensile Deformation of Special Material -- 11.5 Design of Landing Gear Mechanism -- 11.5.1 Requirements Analysis -- 11.5.2 Design and Simulation -- 11.6 Testing and Verification -- 11.6.1 Performance Verification of Cushion Material -- 11.6.2 Friction Test of Deployment and Cushion -- 11.6.3 Performance Testing of Lunar Surface Sensing Probe -- 11.6.4 Cushion Performance Test and Verification of Single Set of Landing Gear Mechanism -- 11.6.5 Simulation Verification of Combined Cushion Performance for Landing Gear Subsystem -- 11.7 Summary -- References. 12 Integration and Assembly Technology of Lunar Lander. |
| Record Nr. | UNISA-996466742003316 |
|
Yu Deng-Yun
|
||
| Gateway East, Singapore : , : Springer, , [2021] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
| ||
Technology of lunar soft lander / / Deng-Yun Yu, Ze-Zhou Sun, He Zhang
| Technology of lunar soft lander / / Deng-Yun Yu, Ze-Zhou Sun, He Zhang |
| Autore | Yu Deng-Yun |
| Pubbl/distr/stampa | Gateway East, Singapore : , : Springer, , [2021] |
| Descrizione fisica | 1 online resource (xxviii, 565 pages) : illustrations |
| Disciplina | 629.47 |
| Collana | Space Technology Library |
| Soggetto topico | Space vehicles - Design and construction |
| ISBN | 981-15-6580-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Foreword By Fanpei Lei -- Foreword By Peijian Ye -- Preface I -- Preface II -- Contents -- Acronyms -- 1 Introduction -- 1.1 Significance of and General Approaches to Lunar Exploration -- 1.1.1 Significance of Lunar Exploration -- 1.1.2 General Approaches to Lunar Exploration -- 1.2 Status of Lunar Lander Technology Development Outside China -- 1.2.1 Development of Lunar Lander Technology in the Soviet Union [1, 14] -- 1.2.2 Development of Lunar Lander Technology in the United States [1, 6−13] -- 1.3 China's Lunar Exploration Program -- 1.3.1 General Plan of CLEP -- 1.3.2 Brief Information on Chang'E Probes -- 1.4 Technical Challenges to Development of Lunar Lander [5, 14, 16] -- 1.5 Summary -- References -- 2 Environment Analysis of Lunar Soft Landing Exploration -- 2.1 Introduction -- 2.2 Lunar Radiation Environment -- 2.2.1 Galactic Cosmic Rays -- 2.2.2 Solar Energetic Particles -- 2.2.3 Plasma Environment in Lunar Orbit -- 2.3 Lunar Thermal Environment -- 2.3.1 Solar Radiation -- 2.3.2 Lunar Albedo -- 2.3.3 Lunar Radiation -- 2.3.4 Earth Albedo -- 2.3.5 Earth Radiation -- 2.4 Lunar Landform and Topography -- 2.4.1 Lunar Landform -- 2.4.2 Lunar Topography -- 2.5 Lunar Soil and Dust -- 2.5.1 Physical Properties -- 2.5.2 Mechanical Properties -- 2.5.3 Electromagnetic Properties -- 2.6 Other Lunar Environments -- 2.6.1 Lunar Gravity -- 2.6.2 Near Vacuum Environment of the Moon -- 2.6.3 Illumination Environment on the Lunar Surface -- 2.7 Summary -- References -- 3 System Design of Lunar Lander -- 3.1 Introduction -- 3.2 Principles of System Design -- 3.3 Mission Analysis -- 3.3.1 Analysis of Mission Characteristics -- 3.3.2 Analysis of Landing Site -- 3.3.3 Analysis of Flight Profile -- 3.3.4 Analysis of Environment Effects -- 3.3.5 Analysis of Payload Configuration -- 3.4 Trajectory Design -- 3.4.1 Overview of Flight Profile.
3.4.2 Constraints of Trajectory Design -- 3.4.3 Determination of Landing Window -- 3.4.4 Analysis of Circumlunar Orbit -- 3.4.5 Determination of LTO -- 3.4.6 Analysis of Launch Window -- 3.5 System Components and Specifications -- 3.5.1 System Components -- 3.5.2 Major System Specifications -- 3.5.3 Propellant Budget -- 3.6 System Configuration Design -- 3.6.1 Design Principles -- 3.6.2 System Configuration -- 3.7 Planning of TT& -- C Link -- 3.8 Design of Powered Descent and Soft Landing -- 3.8.1 Initial Status and Setup of Powered Descent -- 3.8.2 Process of Powered Descent and Soft Landing -- 3.8.3 Landing Cushion -- 3.8.4 Downloading of Descent Images -- 3.9 Analysis and Simulation of Landing Stability -- 3.10 Summary -- References -- 4 Structure and Mechanism Technology of Lunar Lander -- 4.1 Introduction -- 4.2 Structural and Mechanism Features of Lunar Lander -- 4.2.1 Structural Features of Lunar Lander -- 4.2.2 Mechanism Features of Lunar Lander -- 4.3 Design and Verification of Lunar Lander Structure -- 4.3.1 Structural Design -- 4.3.2 Structural Analysis of Lunar Lander -- 4.3.3 Structural Tests of Lunar Lander -- 4.4 Mechanism Design and Verification of Lunar Lander -- 4.4.1 Solar Panel Mechanism -- 4.4.2 Separation Mechanism for Lunar Rover -- 4.4.3 Transfer Mechanism for Lunar Rover -- 4.5 Summary -- References -- 5 Thermal Control Technology of Lunar Lander -- 5.1 Introduction -- 5.2 Current Status of Thermal Control Technology -- 5.3 Thermal Technical Characteristics -- 5.3.1 Design Constraints -- 5.3.2 Technical Characteristics -- 5.4 Design Methodology -- 5.4.1 Principles of Thermal Design -- 5.4.2 Design of Thermal Control -- 5.4.3 Thermal Analysis and Calculation -- 5.5 Typical Technologies -- 5.5.1 Variable Thermal Conductive Technology -- 5.5.2 Protection Technology for High-Temperature Engine. 5.5.3 RHU Application Technology -- 5.5.4 Two-Phase Fluid Loop Technology -- 5.6 Testing and Verification -- 5.6.1 Thermal Balance Test of Lunar Lander -- 5.6.2 VCHP Test -- 5.6.3 Vacuum Thermal Insulation Testing of High-Temperature Heat Shield -- 5.6.4 Two-Phase Fluid Loop Test -- 5.6.5 Flight Testing on Orbit -- 5.7 Summary -- References -- 6 Power Technology of Lunar Lander -- 6.1 Introduction -- 6.2 Status of Power Supply Technology Development -- 6.3 Mission Requirements and Characteristics -- 6.3.1 Functional Requirements -- 6.3.2 Performance Requirements -- 6.3.3 Mission Characteristics and Analysis -- 6.4 Design Methodology -- 6.4.1 Design Principles -- 6.4.2 Illumination Conditions -- 6.4.3 Lightweight Design -- 6.4.4 Analysis of Space Environmental Effects -- 6.4.5 Energy Balance Analysis -- 6.4.6 Analysis of Power System Architecture -- 6.5 Typical Technology -- 6.5.1 Design of Power Controller -- 6.5.2 Design of Battery Pack -- 6.5.3 Design of Solar Cell Circuits -- 6.5.4 Design of Hibernation and Awakening Control -- 6.5.5 Power Supply Reuse Between Probes -- 6.6 Testing and Verification -- 6.6.1 Contents of Verification -- 6.6.2 Verification of Hibernation and Awakening -- 6.6.3 Verification of Large Incident Angle for Solar Cells -- 6.6.4 Extreme Temperature Verification of Solar Cells Performance -- 6.7 Summary -- References -- 7 Guidance, Navigation and Control Technology of Lunar Lander -- 7.1 Introduction -- 7.2 Development of GNC Technology -- 7.3 Analysis of Technical Characteristics -- 7.4 Design Methodology -- 7.4.1 System Configuration -- 7.4.2 Operational Modes -- 7.4.3 Component Design -- 7.4.4 Software Design [7] -- 7.4.5 Autonomous Failure Diagnosis and Handling Logic Design -- 7.5 Typical Technology -- 7.5.1 Procedure of GNC Powered Descent Phase [8] -- 7.5.2 Powered Descent Trajectory Design. 7.5.3 Navigation Method for Powered Descent Phase -- 7.5.4 Guidance Law Design of Powered Descent Process -- 7.5.5 Hazard Detection and Safe Landing Area Selection Method [9] -- 7.5.6 Attitude Control Method for Powered Descent Process [10] -- 7.6 Testing and Verification -- 7.6.1 Key Navigation Sensors Calibration -- 7.6.2 GNC Subsystem Flight Testing -- 7.6.3 Hardware-in-the-Loop Test [11] -- 7.7 Summary -- References -- 8 Propulsion Technology of Lunar Lander -- 8.1 Introduction -- 8.2 Development Status [2, 3] -- 8.3 Design Constraints and Analysis -- 8.3.1 Configurational Constraints -- 8.3.2 Functional Requirements -- 8.3.3 Technical Specification Requirements [4] -- 8.3.4 Flight Environment -- 8.3.5 Long-Term Storage Environment on Lunar Surface -- 8.4 Propulsion Subsystem Design [5-7] -- 8.4.1 Fundamental Design Conditions -- 8.4.2 Determination of Major Specifications of Propulsion Subsystem -- 8.4.3 Design of Propellant Feed System [4] -- 8.4.4 Electronics Design of Propulsion Subsystem -- 8.4.5 AIT Design of Propulsion Subsystem -- 8.4.6 Major Components Design for Propulsion Subsystem -- 8.4.7 Ground Test and Propellant Filling of Propulsion Subsystem -- 8.5 Testing and Verification of Propulsion Subsystem -- 8.5.1 Subsystem Ground Hot Firing -- 8.5.2 Throttling Engine Test -- 8.5.3 Propellant Tank Test -- 8.5.4 Long-Term Pressure-Bearing Storage Test of Gas Tank -- 8.5.5 Propellant Filling Test -- 8.6 Summary -- References -- 9 OBDH Technology of Lunar Lander -- 9.1 Introduction -- 9.2 Development Status -- 9.3 Analysis of Technical Characteristics -- 9.3.1 Mission Analysis -- 9.3.2 Constraints -- 9.4 Design Methodology -- 9.4.1 Principles of Design -- 9.4.2 System Architecture and Configuration -- 9.4.3 Miniaturized and Integrated System Design -- 9.4.4 Bus Network Design -- 9.4.5 Information Management Design. 9.4.6 Design of Spacecraft Autonomous Management -- 9.4.7 Reliable Design of Highly-Integrated and Lightweight Devices -- 9.4.8 Software Design -- 9.5 Testing and Verification -- 9.5.1 Simulation and Test Environment for OBDH Subsystem -- 9.5.2 Content of Verification -- 9.6 Summary -- References -- 10 TT& -- C and Telecommunication Technology of Lunar Lander -- 10.1 Introduction -- 10.2 Development Status -- 10.3 Analysis of Technical Characteristics -- 10.3.1 Requirements -- 10.3.2 Mission Characteristics -- 10.3.3 Design Constraints -- 10.4 Design of Telemetry/Telecommand and Telecommunication Technology -- 10.4.1 Overview -- 10.4.2 Design Method -- 10.4.3 Telemetry/Telecommand and Telecommunication of Lunar Lander to Ground -- 10.4.4 Telecommunication Between Lunar Lander and Lunar Rover -- 10.5 Testing and Verification -- 10.5.1 Compact Field Test -- 10.5.2 Testing of Interface to Ground System -- 10.5.3 UHF Field Test -- 10.6 Summary -- References -- 11 Landing Gear Technology of Lunar Lander -- 11.1 Introduction -- 11.2 Development Status -- 11.3 Configuration and Technical Features of Landing Gear System -- 11.4 Common Cushion Methods and Their Features -- 11.4.1 Cellular Material Deformation -- 11.4.2 Deformation of Thin-Walled Metal Tube -- 11.4.3 Hydraulic Damping -- 11.4.4 Tensile Deformation of Special Material -- 11.5 Design of Landing Gear Mechanism -- 11.5.1 Requirements Analysis -- 11.5.2 Design and Simulation -- 11.6 Testing and Verification -- 11.6.1 Performance Verification of Cushion Material -- 11.6.2 Friction Test of Deployment and Cushion -- 11.6.3 Performance Testing of Lunar Surface Sensing Probe -- 11.6.4 Cushion Performance Test and Verification of Single Set of Landing Gear Mechanism -- 11.6.5 Simulation Verification of Combined Cushion Performance for Landing Gear Subsystem -- 11.7 Summary -- References. 12 Integration and Assembly Technology of Lunar Lander. |
| Record Nr. | UNINA-9910484883603321 |
|
Yu Deng-Yun
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||
| Gateway East, Singapore : , : Springer, , [2021] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression / / Charles J. Camarda
| Tests of graphite/polyimide sandwich panels in uniaxial edgewise compression / / Charles J. Camarda |
| Autore | Camarda Charles J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (76 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Structural stability
Buckling (Mechanics) Graphite - Testing Space vehicles - Design and construction Sandwich construction |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702505403321 |
|
Camarda Charles J.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Thermal-hydraulics for space power, propulsion, and thermal management system design [[electronic resource] /] / edited by William J. Krotiuk
| Thermal-hydraulics for space power, propulsion, and thermal management system design [[electronic resource] /] / edited by William J. Krotiuk |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1990 |
| Descrizione fisica | 1 online resource (348 p.) |
| Disciplina |
629.1 s
629.47/4 |
| Altri autori (Persone) | KrotiukWilliam J |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Space vehicles - Design and construction
Space vehicles - Thermodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-596-8
1-60086-377-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1. Overview of Thermal-Hydraulic Aspects of Current Space Projects""; ""Space Station Thermal Management Systems""; ""Thermal Design of the Space Station Free-Flying Platforms""; ""SP-100 Space Reactor Power System""; ""Advanced Multimegawatt Space Nuclear Power Concepts""; ""Propulsion Systems""; ""Chapter 2. Space Station Two-Phase Thermal Management""; ""Space Station Mechanical Pumped Loop""; ""Capillary Pumped Loop Supporting Technology""
""Chapter 3. Startup Thaw Concept for the SP-100 Space Reactor Power System""""Chapter 4. Calculational Methods and Experimental Data for Microgravity Conditions""; ""Chapter 5. Isothermal Gas-Liquid Flow at Reduced Gravity""; ""Chapter 6. Vapor Generation in Aerospace Applications""; ""Low-Gravity Flow Boiling""; ""Computation of Space Shuttle High-Pressure Cryogenic Turbopump Ball Bearing Two-Phase Coolant Flow""; ""Chapter 7. Reduced-Gravity Condensation""; ""Author Index"" |
| Record Nr. | UNINA-9910457247403321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1990 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Thermal-hydraulics for space power, propulsion, and thermal management system design [[electronic resource] /] / edited by William J. Krotiuk
| Thermal-hydraulics for space power, propulsion, and thermal management system design [[electronic resource] /] / edited by William J. Krotiuk |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1990 |
| Descrizione fisica | 1 online resource (348 p.) |
| Disciplina |
629.1 s
629.47/4 |
| Altri autori (Persone) | KrotiukWilliam J |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Space vehicles - Design and construction
Space vehicles - Thermodynamics |
| ISBN |
1-60086-596-8
1-60086-377-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1. Overview of Thermal-Hydraulic Aspects of Current Space Projects""; ""Space Station Thermal Management Systems""; ""Thermal Design of the Space Station Free-Flying Platforms""; ""SP-100 Space Reactor Power System""; ""Advanced Multimegawatt Space Nuclear Power Concepts""; ""Propulsion Systems""; ""Chapter 2. Space Station Two-Phase Thermal Management""; ""Space Station Mechanical Pumped Loop""; ""Capillary Pumped Loop Supporting Technology""
""Chapter 3. Startup Thaw Concept for the SP-100 Space Reactor Power System""""Chapter 4. Calculational Methods and Experimental Data for Microgravity Conditions""; ""Chapter 5. Isothermal Gas-Liquid Flow at Reduced Gravity""; ""Chapter 6. Vapor Generation in Aerospace Applications""; ""Low-Gravity Flow Boiling""; ""Computation of Space Shuttle High-Pressure Cryogenic Turbopump Ball Bearing Two-Phase Coolant Flow""; ""Chapter 7. Reduced-Gravity Condensation""; ""Author Index"" |
| Record Nr. | UNINA-9910781417703321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1990 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
