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Engineering
Aerospace Engineering
Spacecraft Design
1. Fundamentals of Spacecraft Design
2. Mission Analysis and Orbit Design
3. Spacecraft Subsystems
4. Systems Engineering and Integration
5. Launch and Operations
Mission Analysis and Orbit Design
Orbital Mechanics Fundamentals
Two-Body Problem
Assumptions and Limitations
Analytical Solutions
Kepler's Laws of Planetary Motion
First Law: Elliptical Orbits
Second Law: Equal Areas
Third Law: Periods and Semi-Major Axis
Orbital Elements
Classical Orbital Elements
Semi-Major Axis
Eccentricity
Inclination
Right Ascension of Ascending Node
Argument of Periapsis
True Anomaly
Conversion Between State Vectors and Elements
Coordinate Systems
Earth-Centered Inertial
Earth-Centered Earth-Fixed
Local-Vertical Local-Horizontal
Types of Orbits
Low Earth Orbit
Altitude Range
Orbital Lifetime
Medium Earth Orbit
Altitude Range
Navigation Satellites
Geostationary Orbit
Geosynchronous vs. Geostationary
Station-Keeping
Highly Elliptical Orbit
Molniya Orbits
Tundra Orbits
Coverage Characteristics
Polar and Sun-Synchronous Orbits
Polar Orbit Characteristics
Sun-Synchronous Precession
Earth Observation Applications
Lagrange Points and Halo Orbits
Lagrange Point Locations
Stability and Applications
Halo Orbits
Lissajous Orbits
Trajectory Design
Launch Windows
Orbital Plane Alignment
Interplanetary Launch Windows
Interplanetary Trajectories
Hohmann Transfers
Transfer Time and Delta-v
Gravity Assists
Trajectory Planning
Energy Gain
Spiral Trajectories
Low-Thrust Transfers
Electric Propulsion Applications
Orbit Maneuvering
Plane Changes
Delta-v Requirements
Optimal Maneuver Points
Altitude Changes
Perigee and Apogee Adjustments
Orbit Insertion and De-orbiting
Capture Maneuvers
Controlled Re-entry
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1. Fundamentals of Spacecraft Design
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3. Spacecraft Subsystems