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Скачать клипы AEE462 Lecture 9, Part D ↓

AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers

AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers

AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude

AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude

AEE462 Lecture 9, Part B - Bi-Elliptic Transfers

AEE462 Lecture 9, Part B - Bi-Elliptic Transfers

AEE462 Lecture 9, Part A - The Oberth Effect

AEE462 Lecture 9, Part A - The Oberth Effect

Space Mechanics | Orbital Maneuver | Plane Change Maneuver

Space Mechanics | Orbital Maneuver | Plane Change Maneuver

Calculate Transit Time to Change Orbit in a Hohmann Transfer

Calculate Transit Time to Change Orbit in a Hohmann Transfer

Optimal Rocket Staging with Lagrange Multipliers

Optimal Rocket Staging with Lagrange Multipliers

Hohmann Transfers Explained Using BASIC Physics | Find Both Delta V's

Hohmann Transfers Explained Using BASIC Physics | Find Both Delta V's

AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation

AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation

AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem

AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem

5 - 4 - Impulsive Maneuvers and Co-Planar Orbital Transfers

5 - 4 - Impulsive Maneuvers and Co-Planar Orbital Transfers

AEE462 Lecture15a - Introduction to Spacecraft Design

AEE462 Lecture15a - Introduction to Spacecraft Design

Aerogravity Assist - The Gravity Assist on Steroids

Aerogravity Assist - The Gravity Assist on Steroids

AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time

AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time

AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit

AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit

Bielliptic transfer -  derivation of delta V

Bielliptic transfer - derivation of delta V

LSN 9 - Transforming a Position Vector and a Velocity Vector into the 6 Classical Orbital Elements

LSN 9 - Transforming a Position Vector and a Velocity Vector into the 6 Classical Orbital Elements

AEE462 lecture 14c - Gravitational Assist Maneuvers

AEE462 lecture 14c - Gravitational Assist Maneuvers

AEE462 Lecture 1, Part A/B - Orbits and the Greeks

AEE462 Lecture 1, Part A/B - Orbits and the Greeks

hohmann transfer orbit calculation

hohmann transfer orbit calculation

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