Author name: Gurupriya Dey Sarkar

The Rolls-Royce Olympus 593 engine is a turbojet engine used on the Concorde supersonic airliner. The propulsive efficiency of any jet engine, including the Olympus 593, is a measure of how effectively the engine converts the thermal energy of combusted fuel into useful thrust. The propulsive efficiency is a crucial parameter in evaluating the performance […]

Pulsed Detonation Engines (PDEs) are a type of propulsion system that relies on detonations of fuel and oxidizer mixtures to generate thrust. In a PDE, combustion occurs through detonations, where the combustion process is supersonic. PDEs are known for potentially achieving high thermodynamic efficiency due to the nature of the detonation process. The propulsive efficiency

The propulsive efficiency of an aerospike engine is a measure of how effectively the engine converts the thermal energy of combusted propellant into useful thrust. Aerospike engines are a type of rocket engine designed to maintain optimal performance across a range of altitudes, addressing some of the limitations of traditional bell-shaped nozzles. The propulsive efficiency

Nuclear pulse propulsion is a theoretical propulsion technology that involves detonating nuclear explosions behind a spacecraft. The concept was primarily explored for interplanetary or interstellar travel, and it relies on the principle of using nuclear explosions to propel a spacecraft forward. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket

The propulsive efficiency of a pulsejet engine is a measure of how effectively the engine converts the chemical energy of fuel into useful thrust. It’s important to note that pulsejet engines are known for their simplicity and high thrust-to-weight ratios but are generally not as fuel-efficient as some other propulsion systems. They are often used

The propulsive efficiency of a Stirling engine is a measure of how well the engine converts thermal energy into useful mechanical work. In the context of a Stirling engine, it represents the efficiency of converting heat input into mechanical power. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine,

The propulsive efficiency of a liquid propellant rocket engine is a measure of how effectively the chemical energy stored in the liquid propellants is converted into kinetic energy of the exhaust gases, resulting in thrust. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine, indicating how well it converts

The propulsive efficiency of a rocket engine is defined as the ratio of the kinetic energy of the exhaust gases to the thermal energy released by the propellant. For a nuclear thermal rocket engine, this efficiency is particularly relevant, as it involves the conversion of thermal energy from a nuclear reactor into kinetic energy of

The thrust coefficient of an aircraft is a dimensionless parameter that relates the thrust produced by the aircraft’s propulsion system to the dynamic pressure of the incoming air. For the C-130 Hercules, additional considerations may include payload capacity, range, and endurance. While the specific design and performance characteristics of the C-130 Hercules may not be

The Lockheed P-3 Orion is a maritime patrol aircraft, and the concept of a thrust coefficient is not commonly used to characterize its performance. The thrust coefficient is typically associated with propulsion systems like jet engines or propellers. The thrust coefficient is defined as the ratio of the thrust force produced by the propulsion system