Tsiolkovsky Rocket Equation evaluator uses Change in Rocket Velocity = Specific Impulse*[g]*ln(Wet Mass/Dry mass) to evaluate the Change in Rocket Velocity, The Tsiolkovsky Rocket Equation,also known as the ideal rocket equation, is a fundamental equation in astronautics that governs the motion of vehicles propelled by rocket engines, it provides a mathematical relationship between the change in velocity of a rocket, the effective exhaust velocity of its propellant, and the ratio of its initial and final masses. Change in Rocket Velocity is denoted by ΔV symbol.
How to evaluate Tsiolkovsky Rocket Equation using this online evaluator? To use this online evaluator for Tsiolkovsky Rocket Equation, enter Specific Impulse (Isp), Wet Mass (Mwet) & Dry mass (Mdry) and hit the calculate button.