Unit 1
Principle of Rocket Propulsion – Rocket Equation – Development of Thrust – Nozzle Design – Effect of Atmosphere – Thermodynamic Thrust Equation – Characteristic Velocity – Performance Parameters.
Course Name | Rocket and Spacecraft Propulsion |
Course Code | 19AEE441 |
Program | B. Tech. in Aerospace Engineering |
Year Taught | 2019 |
Principle of Rocket Propulsion – Rocket Equation – Development of Thrust – Nozzle Design – Effect of Atmosphere – Thermodynamic Thrust Equation – Characteristic Velocity – Performance Parameters.
Liquid Propellant Rocket Engine – Cryogenic and Semi-cryogenic Engines – Basic Configuration – Types of Propellants – Propellant Feed Systems – Combustion of Liquid Propellants – Injectors and Thrust Chambers – Combustion Instability – Solid Propellant Fundamentals – Types of Solid Propellants – Propellant Processing and Manufacture – Grain Configuration – Igniter Hardware – Combustion of Solid Propellants – Hybrid Rocket Engines.
Electric Propulsion: Electrothermal and Electromagnetic Thrusters, Applications of Electric Propulsion, Electric Power Generation – Nuclear Propulsion – Operational Issues – Practical Approaches for Single Stage to Orbit Vehicles.
Course Objectives
Course Outcomes
CO – PO Mapping
PO/PSO/
CO |
PO1 | PO2 | PO3 | PO4 | PO5 | PO6 | PO7 | PO8 | PO9 | PO10 | PO11 | PO12 | PSO1 | PSO2 | PSO3 |
CO1 | 3 | 2 | 1 | 1 | 3 | ||||||||||
CO2 | 3 | 3 | 2 | 2 | 3 | 1 | |||||||||
CO3 | 2 | 3 | 3 | 3 | 1 | 3 | 2 | 2 | |||||||
CO4 | 1 | 1 | 2 | 2 | 2 | 3 | 1 | 1 | |||||||
CO5 | 2 | 2 | 1 | 1 | 1 | 2 | 3 | 1 | 1 |
Textbook(s)
Evaluation Pattern
Assessment | Internal | External |
Periodical 1 (P1) | 15 | – |
Periodical 2 (P2) | 15 | – |
*Continuous Assessment (CA) | 20 | – |
End Semester | – | 50 |
*CA – Can be Quizzes, Assignment, Projects, and Reports. |
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