Author name: Gurupriya Dey Sarkar

Bipropellant rocket engines use two separate substances as fuel and oxidizer. The propellant components react chemically in the combustion chamber to produce thrust. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine, indicating how well it converts propellant energy into useful thrust. Practical rocket engines often have propulsive efficiencies […]

Monopropellant rocket engines use a single substance as both fuel and oxidizer. The propellant decomposes or undergoes a chemical reaction to produce thrust. Specific details, such as the heating value of the propellant, mass flow rates, and mixture ratio values, would need to be obtained from engine performance data or technical specifications for the specific

Pressure-fed rocket engines rely on the pressure of stored gases to force propellants into the combustion chamber. They are often used in smaller rockets and spacecraft. Specific details, such as the heating value of the propellant, mass flow rates, and mixture ratio values, would need to be obtained from engine performance data or technical specifications

Satellite launch vehicles are designed to transport payloads, such as satellites, into orbit. The propulsive efficiency of a specific launch vehicle is influenced by design parameters, operating conditions, and other factors. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine, indicating how well it converts propellant energy into useful

For specific details such as the heating value of the propellant, mass flow rates, and mixture ratio values for the Falcon 9 rocket, these would need to be obtained from SpaceX’s technical specifications or performance data. The efficiency of the Falcon 9 rocket is influenced by design parameters, operating conditions, and other factors. The Falcon

Reusable launch vehicles are designed to be recovered and reused for multiple flights, and their propulsive efficiency is influenced by the design and performance of the reusable stages. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine, indicating how well it converts propellant energy into useful thrust. Practical rocket

Expendable launch vehicles are designed for one-time use, and their propulsive efficiency is influenced by the design and performance of the rocket stages. The propulsive efficiency is a crucial parameter in evaluating the performance of a rocket engine, indicating how well it converts propellant energy into useful thrust. Practical rocket engines often have propulsive efficiencies

A multistage rocket consists of multiple stages stacked on top of each other, with each stage having its engines and propellant. When a stage is depleted of propellant, it is jettisoned to reduce the mass the remaining stages need to accelerate. The total mixture ratio for all stages is considered to calculate the overall propulsive

Orbital rockets are designed to reach the velocity required for an object to stay in orbit around a celestial body, such as Earth. The efficiency of a specific orbital rocket can be influenced by design parameters, operating conditions, and other factors. Achieving high propulsive efficiency is crucial for maximizing payload capacity and achieving mission objectives.

Suborbital rockets are designed to reach altitudes above the Earth’s atmosphere but not to achieve orbital velocity. They are typically used for scientific research, testing, or commercial purposes such as space tourism. The efficiency of a specific suborbital rocket can be influenced by design parameters, operating conditions, and other factors. The propulsive efficiency is a