Propulsion Calculator

In pressure-fed propulsion, propellant pushes into the combustion chamber from a tank using pressure, not pumping. It’s simpler and more reliable than pump-fed systems but typically has lower performance. Where: ˙m˙ is the mass flow rate of propellant Ve​ is the effective exhaust velocity Pe​ is the pressure at the exit of the nozzle P0​ […]

Gravitational Losses calculator. refer to the energy loss that occurs when lifting an object against the force of gravity. Physicists commonly encounter this concept, particularly when analyzing systems involving potential energy or calculating the work done against gravitational forces. Where: m is the mass of the object (in kilograms), g is the acceleration due to

the term “Total Impulse calculator” to describe the overall effect of a force applied over a period of time. It defines it as the integral of thrust (force) over the time during which one applies the thrust. Total impulse, fundamentally, represents the cumulative effect of a force exerted over a specific duration, pivotal in the

The net thrust formula for a jet engine, such as a turbojet or turbofan, can be derived based on the principle of conservation of momentum and the mass flow rate of air and fuel through the engine. where: ˙m˙ is the mass flow rate of air (and fuel, if applicable) through the engine (kg/s), Ve​

Ambient pressure thrust refers to the force generated by a propulsion system, such as a rocket engine or jet engine, in an environment where the pressure is relatively high, such as at sea level. This thrust is influenced by the ambient atmospheric pressure, which affects the engine’s ability to push against the surrounding air or

Thrust vectoring Calculator is a technique used in aircraft and rocket engines to manipulate the direction of thrust. The formula for calculating the effect of thrust vectoring depends on various factors such as the angle of deflection, engine thrust, and the distance between the engine’s center of thrust and the aircraft’s center of gravity. One

The specific thrust of an engine is a measure of its efficiency in converting fuel into thrust. It represents the thrust generated by the engine per unit mass flow rate of the exhaust gases expelled from the engine. In simpler terms, it quantifies how much thrust the engine produces for each unit of fuel burned

The thrust-to-weight ratio calculator as a measure in the field of aerospace engineering to assess the performance of an aircraft, spacecraft, or other vehicles equipped with propulsion systems. They define it as the ratio of the thrust produced by the propulsion system to the weight of the vehicle. Where: The engine or propulsion system produces

Exhaust velocity Calculator is a fundamental concept in rocket propulsion that describes the speed at which combustion gases exit a rocket engine. Exhaust velocity Calculator plays a crucial role in determining the performance, efficiency, and capabilities of a rocket. where: The specific impulse of the rocket engine (measured in seconds) is Isp. g is the

Rocketry and aerospace engineering typically associate with the concept of the Burnout Velocity Calculator. This concept, by calculating the velocity of a rocket at the precise moment its propellant is completely consumed, essentially defines what we know as the Burnout Velocity. Where: Vburnout is the burnout velocity (final velocity). Vinitial is the initial velocity (velocity at