Advances in Solar Sailing

Name: Advances in Solar Sailing
Brand: Springer
Price: 373.43 EUR
Availability: OnlineOnly

Malcolm Macdonald(Editor)

Springer (Publisher)

1st Edition

Published on 3. February 2014

XXIV, 980 pages

E-Book

PDF with digital watermarking

System requirements

978-3-642-34907-2 (ISBN)

€373.43incl. 7% vat

System requirements

for PDF with digital watermarking

E-Book Single Licence

Available for download

Description

More details

Other editions

Content

Intro
Contents
Preface
Organizing Committee
Part I: Flight Programs
1 An overview of solar sail related activities at JAXA
I .Introduction
II.Ikaros Mission-how it was born and what was demonstrated
III. Solar Power Sail to Trojan Asteroids
IV. Preparation Activities for Solar Power Sail mission
V. Conclusion
References
2 An Overview of Solar Sail Propulsion within NASA
I. Introduction
II. Solar Sails In Perspective: 1990's to the Present
III. Potential Future Missions and Concepts
IV. Technology Development and Demonstrations
V. Conclusion
References
3 Overview of IKAROS Mission
I. Introduction
II. IKAROS Mission
III.Devolopment of IKAROS Spacecraft
IV. IKAROS Operation
V. Conclusion
References
4 How IKAROS Shape is Designed -Attitude Stability ofSpinning Solar Sail
I. Introduction
II. Derivation of Attitude Stability for Spinning Solar Sail
III. Designing Spinning Sail Spacecraft Configuration
IV. Numerical and In-Flight Evaluation of Stability
V. Conclusion
References
5 Evaluation of Sail Mechanics of IKAROS on its Slow-spinand Reverse-spin Operation
I. Introduction
II. Configuration of the Sail
III. Slow-spin Operation
IV. Numerical Analysis of the Shape of the Sail
V. Reverse-spin Operation
VI. Discussion
VII. Conclusion
References
6 Attitude and Orbit Prediction of IKAROS in Actual Flight Operation
I. Introduction
II. Characteristics of IKAROS
III. Search Operation
IV. Attitude Prediction
V. Orbit Prediction
VI. Results of Search Operation
VII. Analysis to Improve Trajectory Prediction
VIII. Summary
References
7 NanoSail - D Orbital and Attitude Dynamics
I. Introduction
II. Background
III. Analysis
IV. Models
V. Results
VI. Conclusions
References
8 Sunjammer : A Solar Sail Demonstration
Sunjammer Mission Overview
Deployment
Attitude Calibration
Thrust Calibration
Flyout and Other Extended Operations
References
9 Commercial Solar Sail Applications: Overview andUpdate on NASA's Sunjammer Mission
I. About Sunjammer
II. About SSHI
III. Precursor Private Solar Sail Efforts
IV. SSHI and Sunjammer
V. Post Sunjammer Commercial Infusion Activities and Opportunities
VI. Conclusion
VII. References
10 The Preliminary Design of the GOSSAMER-1 Solar SailMembrane and Manufacturing Strategies
I. Introduction
II. Sail Storage
III. Material Selection
IV. Membrane Design
V. Sail Membrane Manufacturing
VI. Conclusion
References
11 Demonstrator Flight Missions at the Surrey SpaceCentre involving Gossamer Sails
I. Introduction
II. CubeSail
III. DGOSS - Deployable Gossamer Sail for Deorbiting
IV. DeorbitSail
V. InflateSail
VI. Conclusions
References
12 ISS-based solar sail deployment experiment "BMSTU- Sail"
I. Introduction
II. Mission design
III. BMSTU-Sail picosatellite and launch device
IV. Data acquisition
V. Conclusion
References
Part II Mission Applications
13 Magnetic field measurements from a solar sail platformwith space weather applications
I. Motivation: An Introduction to the Near Earth Space Environment and Space Weather
II. Drivers of Geomagnetic Activity
III. Measurement of the Interplanetary Magnetic Field upstream of the Earth
IV. The Sunjammer solar sail mission
V. MAGIC: MAGnetometer from Imperial College
VI. Conclusion
References
14 The Solar Wind Analyser (SWAN) for the Sunjammer solar sail mission
I. Introduction
II. Measurement requirements
III. Instrument technical details
IV. Conclusi
Acknowledgments
References
15 Gossamer Roadmap Technology Reference Studyfor a Multiple NEO Rendezvous Mission
I. Introduction
II. Previous Work on Solar Sail Missions to NEOs
III. Study and Mission Objectives
IV. Solar Sailcraft Design
V. Preliminary Potential Mission Scenario
VI. Conclusions and Future Work
References
16 Gossamer Roadmap Technology Reference Study for aSub-L1 Space Weather Mission
I. Introduction
II. Mission Requirements
III. Mission Architecture
IV. Spacecraft Sizing
V. Trajectory Analysis
VI. Propulsion System Comparison
VII. Conclusions
Appendix A
References
17 Gossamer Roadmap Technology Reference Study for aSolar Polar Mission
I. Introduction
II. Mission Architecture & Analysis
III. System Analysis
IV. Conclusions
References
18 SOLARIS: Solar sail investigation of the Sun
I. Introduction
II. Scientific Objectives
III. Instrument and Mission Requirements
IV. Solar-sail mission design
V. Interest of the scientific community
VI. Conclusion
References
19 A Fractionated Space Weather Base at L5 using CubeSatsand Solar Sails
I. Introduction
II. Solar Sail Trajectory Calculation
III. Mission and Spacecraft Overview
IV. Engineering and Science Subsystems
V. Summary and Discussion
References
20 Design and Trade-offs of a Pole-Sitter Mission
I. Introduction
II. Mission Description and Propulsion Options
III. Mission Design
IV. Spacecraft Subsystems Sizing
V. Conclusions
References
21 Reduction of Martian Sample Return Mission LaunchMass with Solar Sail Propulsion
I. Introduction
II. Ground Rules and Assumptions
III. Orbiter Chemical Propulsion Mission Analysis
IV. Solar Sail Mission Analysis
V. Configurations
VI. Spacecraft Structure Analysis
VII. Solar Sail Structures
VIII. Power
IX. Avionics
X. Thermal Control
XI. Mass Properties
XII. Study Conclusion
References
22 Distributed Reflectivity Solar Sails for Extended MissionApplications
I. Introduction
II. Sail Attitude Control using Variable Reflectivity Distribution
III. Sail Shape Control using Variable Reflectivity Distribution
IV. Computation of Focal Length of Parabolic Sail Reflector
References
23 Alternative Application of Solar Sail Technology
I. Introduction
II. System Overview
III. Key Technology
IV. Design Details
V. Flight Results
VI. Prospect
References
24 Earth-crossing asteroids deflection with a sailcraft
I. Introduction
II. Options of Deflection Trajectories
III. Case Studies
IV. Concluding Remarks
Reference
25 Solar Sai ls and the Search for Dark Matter
I. Introduct ion
II . Dark Matter: Its Effect on Interstellar Probe Trajectories
III .Sailcraf t for a Mission to 10,000 AU
IV. Conclusions: Can We Conduct ~100-Year Extra-Solar Missions?
References
Part III Technology Activities
26 Light pressure measurement at DLR Bremen
I. Introduction
II. Theory
III. Test Facility LPMF
IV. Results
V. Conclusion
References
27 Realistic Solar Sail Thrust
I. Introduction
II. Ideal Solar Sail Characteristics
III. Non-ideal Sail Characteristics
IV. Realistic Solar Sail Characteristics
V. Solar Sailcraft Characteristic Performance Comparison
VI. Conclusion
References
28 Direct Thrust Efficiency for the L'Garde Sail Surfacewith a Linear Reflectivity Model
I. Introduction
II. Solar Radiation Force Modeling and the Linear Thrust Model
III. The L'Garde Sail Architecture and its Trough Shape
IV. Conclusion
References
29 Thrust Efficiency on an Idealized Deformable Sail
I. Introduction
II. Force efficiency and CM-CP offset
III. Impact of sail sag
IV. Model of a deformable sail
V. Conclusion
References
30 The Solar Radiation Pressure Force Models for a GeneralSail Surface Shape
I. Introduction
II. Sail Surface Assumption and the Differential Force & Moment
III. The Tensor Forms of the Total Force & Moment
IV. The Parameterized Forms of the Total Force & Moment
V. Some Properties for the Deformed Sail Surface
VI. Example
VII. Conclusions
Appendix
References
31 Applying Vector Scattering Theory to Solar-Photon SailThrust Modeling
I. Introduction
II. BRDF: a reminder
III. Solar-Sail Surface Modeling
IV. Polarization in SPS
V. Sail Reflectance Photon Momenta
VI. Numerical Results
VII. Conclusion and Next Development
References
32 The Solar Sail Materials (SSM) Project - Results ofActivities
I. Introduction
II. Project Objectives and Logic
III. Synthesis of Material Tests
IV. Synthesis of Breadboarding
V. Synthesis of FEM Activities
VI. Synthesis of System Activities
VII. Conclusions
References
33 Selection and Manufacturing of Membrane Materials forSolar Sails
I. Introduction:
II. Discussion:
III. Conclusions:
References:
34 The Complex Irradiation Facility at DLR-Bremen
I. Introduction
II. Overview of the configuration and instrumentation of the CIF
III. The radiation sources of the CIF
IV. Conclusion
References
35 H2 blister formation on metallic surfaces - a candidate fordegradation processes in space
I. Introduction
II. Temporal evolution of bubble formation
III. Formation possibility of H2 bubbles in the interplanetary medium, numerical analysis ofbubble growth.
IV. The effect of bubble formation on to the reflectivity
V. Conclusion
References
36 Solar Sail: Materials and Space Environmental Effects
I. Introduction
II. Solar Radiation
III. Temperature Dependence of Solar Sail Parameters
IV. Degradation of Solar Sail Materials by Solar Radiations
V. Discussion and Conclusions
References
37 Design and Sizing of theGOSSAMER Boom Deployment Concept
I. Introduction
II. Basic Concept
III. Boom Design
IV. Boom & Sail Deployment Unit Design
V. Conclusion
References
38 Bistable Over the Whole Length (BOWL) CFRP Boomsfor Solar Sails
I. Introduction
II. Bistability of thin composite shells
III. Challenges in the design of long bistable composite tubes
IV. Determining coiled curvature as a function of braid angle
V. Bistable Over the Whole Length (BOWL) booms
VI. New low-cost manufacturing technique
VII. Experimental analysis of bistable composite booms
VIII. Current applications of BOWL CFRP booms in large gossamer structures
IX. Discussion
X. Conclusion
References
Part IV Dynamics
39 Heliogyro Solar Sail Research at NASA
I. Introduction
II. HELIOS: A Reference Design Concept for Heliogyro Technology Development
III. Heliogyro Technology Development Activities
IV. Conclusion
References
40 Solarelastic Stability of the Heliogyro
I. Introduction
II. Model Description
III. Structural Results
IV. Solarelastic Results
V. Conclusion
References
41 Heliogyro Attitude Control Moment Authority via BladePitch Maneuvers
I. Introduction
II. Background
III. Discussion of Attitude Control Strategies
IV. Inversion of HGForce with Half-p strategy
V. Conclusions
Appendix
References
42 Dynamics of a Coupled Pendulum Model of a HeliogyroMembrane Blade
I. Introduction
II. Discrete Configuration of a Membrane
III. Dynamic Equations of Motion
IV. Continuous Equations
V. Natural Frequencies Observed from the Linearized Equations
VI. Simulation Results for a 3-dof Hanging Model
VII. Experiment Results for a 3-dof Model
VIII. Conclusion
References
43 Challenges Associated with System Identification andControl of a Heliogyro Membrane Blade
I. Introduction
II. Model Description
III. Simulation of Spinning Membrane Model
IV. Design of Controller
V. Stability robustness
VI. Conclusion
References
44 Two-blade solar sail dynamics
I. Introduction
II. Problem formulation
III. Mathematical model
IV. Numerical experiments
V. Estimation of design parameters
VI. Conclusion
References
45 Solar Sail Coning Control to Induce Orbital Effects inSpinning Versus Non-Spinning Sails
I. Solar Sail Introduction
II. Solar Sail Attitude Dynamics and Control
III. Solar Sail Coning Dynamics
IV. Natural Dynamics of Spinning Versus Non-Spinning Solar Sails
V. Dynamics of Spinning Versus Non-Spinning Solar Sails using Sail Coning Controller
VI. Conclusion
References
46 The Attitude Control of a Tri-Spin Solar Sail Satellite
I. Introduction
II. Spinning Sail Concept
III. Dynamic Model
IV. Attitude Control
V. Conclusion
References
47 Influence of Attitude Control on Orbital Plane Change forFlexible Solar Sail
I. Introduction
II. Coupled Dynamic Model of a Flexible Solar Sail
III. Optimal trajectory design for the transfer mission
IV. Analysis of the transfer mission of the flexible solar sail with attitude control
V. Conclusion
References
48 Coupled Attitude-orbit Dynamics and Control of ReflectivityModulated Solar Sail for GeoSail Formation Flying
I. Introduction
II. Force and Torque Models of Reflectivity Modulated Solar Sail
III. Attitude-orbit Coupled Dynamics of Reflectivity Modulated Solar Sail on a GeoSailOrbit
IV. Coupled Dynamics and Control of Relative Motion of Two Sails
V. Numerical Results
VI. Conclusion
References
49 Dynamical Analysis of The Deployment for A ReducedSpinning Solar Sail Model
I. Introduction
II. Two Steps Deployment Method
III. Modeling of Three Dimensional Yo-Yo Booms
IV. Numerical Simulations
V. Conclusion
References
Part V Advanced Concepts
50 Optimal Solar Sail Interplanetary Trajectories withConstant Cone Angle
I. Introduction
II. Mathematical Model
III. Mission Applications
IV. Conclusions
References
51 New Families of non-Keplerian Orbits: Solar SailMotion over Cylinders and Spheres
I. Introduction
II. Cylindrically constrained NKOs
III. Spherically constrained NKOs
IV. Conclusions
References
52 Families of periodic orbits for solar sails in the CRBTP
I. Introduction
II. The Solar Sail CRTBP
III. Numerical Continuation
IV. The Radial Case
V. The Non-Radial Case
VI. Conclusion
References
53 Periodic Motion for an Imperfect Solar Sail near an Asteroid
Introduction
The Augmented Hill for a Non-Perfectly Reflecting Solar Sail
Equilibrium Points
Periodic Orbits
Conclusions and Future Work
References
54 Variable-geometry solar sailing:the possibilities of the quasi-rhombic pyramid
I. Introduction
II. Geometry and mass properties
III. Mechanical layout
IV. Spacecraft data
V. Attitude motion
VI. Orbital motion
VII. Conclusions
References
55 Real Solar Sails Are Not Ideal, And Yes It Matters
I. Introduction
II. Non-Ideal Sail Behavior
III. Leeward Force
IV. Leeward Force Consequences 1: L1 Maneuvering
V. Leeward Force Consequences 2: Asteroid Formation Flying
VI. Conclusion
References
56 Inspection of a co-orbital solar sail using a microthrusterattitude control system
I. Introduction
II. The InspectorSat mission concept
III. Inspection and co-orbital motion manoeuvres
IV. µCPS thrust requirements
V. Conclusions
References
57 Deployment Simulations of the Space Tow Solar Sail
I. Introduction
II. Deployment Simulations
III. Deployment Analytical Solutions
IV. Conclusions
References
58 Electric solar Wind Sail: Deployment, Long-Term Dynamics, and Control Hardware Requirements
Introduction
Tether Planar Orbit Control Efficiency
Sail Spain Rate Evolution
Non-planar Tether Orbit Control
Conclusions and Discussion
References

System requirements

Save as PDF Copy link into clipboard

Schweitzer Fachinformationen

Advances in Solar Sailing

Description

More details

Other editions

Additional editions

Content

System requirements