MAE 5540 Zoom Web Invitation
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Week 1
- Lecture 1, January 10 2022
- Introduction to Rocket Science
- Rocket Concepts Review
- Thrust
- Specific Impulse
- Rocket Equation Derivation
- Mass Budget Equation
- Ramifications of Rocket Equation
- Correction for "Gravity Losses"
- Gravity Turn
- Rocket Concepts Review
- Lecture 2, January 12 2022
- Ramifications of Rocket Equation
- Correction for "Gravity Losses"
- Gravity Turn
- Correction for Drag and Ballistic Losses
- Correction for "Gravity Losses"
- "Available Delta V Equation"
- Available vs Required Delta V
- Gravitational Model, Force and Potential Energy
- Orbital Velocity (Circular orbit)
- "Earth Boost" Velocity Component
- Ramifications of Rocket Equation
- Lecture 3, January 14 2022 (Virtual)
- Energy Analysis, Concluded
- Available vs Required Delta V Review
- Gravitational Model, Force and Potential Energy
- Orbital Velocity (Circular orbit)
- "Earth Boost" Velocity Component
- STS-114 Example
- Introduction to Space Shuttle Launch Problem
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Week 2
- Lecture 4, Janaury 19, 2022
- Homework 1 review
- "How will My Rocket Go?"
- Analytical Solution for Apogee Altitude
- Total Mechanical Energy of the Rocket
- "Pike" Launch Example
- Introduction to Kepler's laws
- N- and 2-body problem
- Introduction to Kepler's laws
- N- and 2-body problem
- Kepler's First Law
- Polar Form of Ellipse
- Polar form of ellipse equation
- Fixed and rotating coordinate frames
- Derivitive of position vector
- Introduction to Kepler's second law
- Swept Area Integral
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Week 3
- Lecture 6, January 24, 2022
- Kepler's Second Law, continued
- Swept Area Integral
- Eccentric and Mean Anomaly and Kepler's Equation
- Kepler's Second Law as Conservation of Angular Momentum
- Conservation of Angular Momentum
- Kepler's Third Law
- Magnitude of the Velocity Vector
- Summary Kepler's Law Summary
- Lecture 7, January 26, 2022
- Lecture 8, January 28, 2022 (Virtual)
- Vis Viva equation Concluded
- Applications of the Vis-Viva Equation
- Inroduction to Hohmann Transfer
- Orbital Plane Change Introduction
- GEO/GTO Transfer Options
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Week 4
- Lecture 9, January 31, 2022
- GEO/GTO Transfer Options Example (concluded)
- Homework 3 Preview, TT&C Satellite Transfer Problem
- Open Conic Sections
- Parabola
- Escape trajectory revisited
- Hyperbola
- Conic Section Summary
- Star Trek Example
- GEO/GTO Transfer Options Example (concluded)
- Lecture 10, February 2, 2022
- 2-D Equations of Motion (derivation)
- General vs.Ballistic 2-D Equations
- Numerical Integration Methods
- Lecture 11, February 4, 2022 (Virtual)
- Homework 2 Review
- Numerical Integration Methods
- Two-Step Trapezoidal Integrator
- 4th Order Runge-Kutta
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Week 5
- Lecture 12, February 7 2022
- HW 3 Review, TT&C Satellite Transfer Problem
- General vs.Ballistic 2-D Equations Review
- Integrators Concluded
- 2-Step Trapezoidal
- 4th Order Runge Kutta
- Example Problem, V2
- Lecture 13, February 9 2022
- Continuous Thrust EP Transfer Example
- Calculation the Initial State vector
- Calculating {a,e} from State vector {Vr, Vnu, r, nu}
- Project 1 Preview and Assignment
- Continuous Thrust EP Transfer Example
- Lecture 14, February 11 2022 (Virtual)
- Introduction to Propulsion Systems
- Properties of a Launch Vehicle and Spacecraft Thruster
- Thruster Versus Booster Vehicle Requirements
- Cold-Gas and
- Monoprop Cycles
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Week 6
- Lecture 15, February 14 2022
- Project Expectations Review
- Contunuous Thrust Transfer Examples
- Part a
- Low thrust continuous transfer (F=10 N, Isp =2000 sec)
- Impulsive Kick (Isp - 270 sec)
- Run using both RK and Trapezoidal Integrators
- Increase Delta T until Trapezoidal Integrator Fails
- Repeat using RK-integrator, compare results
- Compare to Hohmann Transfer
- Burn 1 Isp: 2000 sec
- Burn 2 Isp: 270 sec
- Part b
- High thrust continuous transfer (F = 2000 N, Isp =270 sec)
- Impulsive Kick (Isp - 270 sec)
- Compare to Hohmann Transfer
- Burn 1 Isp: 270 sec
- Burn 2 Isp: 270 sec
- Part c
- High thrust continuous transfer (F = 2000 N, Isp =270 sec)
- High thrust continuous final kick (F = 2000 N, Isp =270 sec)
- Compare to Hohmann Transfer
- Burn 1 Isp: 270 sec
- Burn 2 Isp: 270 sec
- Lecture 16, February 16 2022
- Introduction to Propulsion Systems (contunued)
- Monopropellant Systems
- Hydrazine
- Ionic Liquid "Green" Propellants
- Bi-Prop Systems
- Open/Closed Cycle Turbo Fed Systems
- Presssure Fed Systems
- Self-Pressurizing Systems
- Introduction to Solid Rockets
- Burn Profile Versus Grain Shape
- Burn Profile Versus Grain Shape
- Monopropellant Systems
- Introduction to Propulsion Systems (contunued)
- Lecture 17, February 18 2022 (Virtual)
- Introduction Solid Rockets (Continued)
- Burn Profile Versus Grain Shape
- Hybrid Rockets
- Relative Advantages/DisAdvantages of Chemical Rocket Systems
- Introduction to Elecric Propulsion
- Power Input Versus Thrust and Isp
- Overview of EP Technologies
- Thermal, Electrostatic, and Eelctromagnetic EP Concepts
- Ion and Hall Effect Thrusters
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Week 7
- Lecture 18, February 23 2022
- Worked OrbitTransfer Example
- Nuclear Propulsion
- Other Advanced Forms of Propulsion
- Review of Nozzle Theory
- Rocket Performance Parameters
- Isp, CF, Cstar
- Isp, CF, Cstar
- Lecture 19, February 25 2022 (Virtual)
- Review of Nozzle Theory
- Rocket Performance Parameters (continued)
- Isp, CF, Cstar, Maximum_Isp
- Non-Ideal Correction factors
- Space Shuttle SSME Calculation Example
New Zoom Link Beginning January 10, 2022
Stephen Whitmore is inviting you to a scheduled Zoom meeting.
Topic: MAE 5540 Lectures
Time: Jan 10, 2022 10:30 AM Mountain Time (US and Canada)
MWF, until Feb 28, 2022 (End of Week 7)
Join Zoom Meeting
https://usu-edu.zoom.us/j/85488662134?pwd=UUxSODFPaVFHZmw0TXhKNTk3cHJmUT09Meeting ID: 854 8866 2134
Passcode: 175548
Approximate Course Schedule Through Week 7, February 25, 2022
Lecture 5. January 21, 2022 (Virtual)