This note
focuses on chemical rocket propulsion systems for launch, orbital, and
interplanetary flight. It teaches the modeling of solid, liquid-bipropellant,
and hybrid rocket engines. Topics covered includes: Rocket Nozzles and Thrust,
Ideal Nozzle Fluid Mechanics, Nozzle Design, Convective Heat Transfer,
Convective Heat Transfer, Liquid Cooling, Ablative Cooling, Film Cooling,
Selection of Propellant Mixtures, Solid Propellants, Liquid Propellants,
Pressurization and Pump Cycles, Liquid Motors, Turbopumps, Turbines, Mechanical
Design of Turbomachinery, Impulsive and Low-Thrust Maneuvers in Space.
Propulsion (Lat. pro-pellere, push forward) is
making a body to move (against natural forces), i.e. fighting against the
natural tendency of relative-motion to decay. Motion is relative to an
environment. Sometimes, propulsion is identified with thrust, the force pushing
a body to move against natural forces, and one might say that propulsion is
thrust (but thrust not necessary implies motion, as when pushing against a wall;
on the other hand, propulsion implies thrust).This PDF covers the following
topics related to Propulsion : Air-breathing Engines, Inlets and Combustion
Chambers, Nozzles, Compressors, Turbines.
Author(s): Dr. Maruthupandiyan, Associate Professor, Institute
of Aeronautical Engineering
This note explains the following
topics:Introduction to Aircraft Jet Propulsion, Jet Engine Cycles :
Thermodynamic Analysis of real cycles, Compressors and Turbines, Combustion
Systems, Intakes and Propelling Nozzles, Aircraft Engine Installed Performance,
Sizing and Matching, Ramjets, Scramjets and Pulsejets.
Author(s): Prof.
Bhaskar Roy and Prof. A M Pradeep
This note
focuses on chemical rocket propulsion systems for launch, orbital, and
interplanetary flight. It teaches the modeling of solid, liquid-bipropellant,
and hybrid rocket engines. Topics covered includes: Rocket Nozzles and Thrust,
Ideal Nozzle Fluid Mechanics, Nozzle Design, Convective Heat Transfer,
Convective Heat Transfer, Liquid Cooling, Ablative Cooling, Film Cooling,
Selection of Propellant Mixtures, Solid Propellants, Liquid Propellants,
Pressurization and Pump Cycles, Liquid Motors, Turbopumps, Turbines, Mechanical
Design of Turbomachinery, Impulsive and Low-Thrust Maneuvers in Space.
This note covers the following
topics: Operational Envelopes, Standard Atmosphere, Air-breathing Engines,
Aircraft Performance, Rocket Engines, Gas Dynamics, H-K Diagram, Normal shock
wave, Flow with heat addition, Flow with friction, Mach Train and Pseudo-shock,
Brayton Cycle, Parametric Cycle Analysis, Ramjet, Turbojet, Turbofan.