7.5 million pounds or 160,000,000 horse power.
The amount of thrust a rocket has depends on its design, type, and size. For example, the Saturn V rocket used in the Apollo missions had a maximum thrust of about 7.5 million pounds-force (33.4 meganewtons). Different rockets can have thrust ranging from a few thousand pounds-force to tens of millions of pounds-force.
The amount of thrust needed to launch a rocket varies depending on the size, weight, and destination of the rocket. On average, rockets require anywhere from hundreds of thousands to millions of pounds of thrust to overcome Earth's gravity and achieve orbital velocity. For example, the Saturn V rocket used during the Apollo missions had a maximum thrust of 7.6 million pounds.
The thrust generated by a solid fuel rocket varies widely depending on its design, size, and the specific type of propellant used. Typically, solid rocket motors can produce thrust ranging from a few thousand pounds to several million pounds. For example, the Space Shuttle's Solid Rocket Boosters generated about 2.7 million pounds of thrust each at launch. The thrust can be calculated using the formula ( F = \dot{m} \cdot v_e ), where ( F ) is thrust, ( \dot{m} ) is the mass flow rate of the propellant, and ( v_e ) is the effective exhaust velocity.
Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.
The first stage of the Saturn V had five engines. At launch, each engine produced about 1,500,000 pounds (or 6,670,000 newtons, the SI unit of force) of thrust. The five engines therefore produced about 7,500,000 pounds or about 33.4 million newtons. As the rocket rose through the atmosphere, its thrust actually increased to almost nine million pounds due to the decreasing pressure of the surrounding air. At the same time, it got much lighter as it furiously burned its propellants. This caused the rocket's acceleration to increase to where it could have damaged its structure or the Apollo spacecraft on top. To keep acceleration under 4 "G's", the center or "inboard" engine was shut down about 26 seconds before the other four.
The amount of thrust a rocket has depends on its design, type, and size. For example, the Saturn V rocket used in the Apollo missions had a maximum thrust of about 7.5 million pounds-force (33.4 meganewtons). Different rockets can have thrust ranging from a few thousand pounds-force to tens of millions of pounds-force.
Enough to lift a small rocket 5-600 feet.
The amount of thrust needed to launch a rocket varies depending on the size, weight, and destination of the rocket. On average, rockets require anywhere from hundreds of thousands to millions of pounds of thrust to overcome Earth's gravity and achieve orbital velocity. For example, the Saturn V rocket used during the Apollo missions had a maximum thrust of 7.6 million pounds.
The thrust generated by a solid fuel rocket varies widely depending on its design, size, and the specific type of propellant used. Typically, solid rocket motors can produce thrust ranging from a few thousand pounds to several million pounds. For example, the Space Shuttle's Solid Rocket Boosters generated about 2.7 million pounds of thrust each at launch. The thrust can be calculated using the formula ( F = \dot{m} \cdot v_e ), where ( F ) is thrust, ( \dot{m} ) is the mass flow rate of the propellant, and ( v_e ) is the effective exhaust velocity.
Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.
5 Million Newtons was the pressure exerted by Saturn v rocket
8 million pounds
The pressure needed to lift off a rocket from the ground depends on various factors such as the weight of the rocket, gravitational force, air resistance, and the design of the rocket's propulsion system. Rockets use powerful engines to generate thrust that exceeds the force of gravity, allowing them to lift off. Typically, rocket engines produce millions of pounds of thrust to achieve liftoff.
The first stage of the Saturn V had five engines. At launch, each engine produced about 1,500,000 pounds (or 6,670,000 newtons, the SI unit of force) of thrust. The five engines therefore produced about 7,500,000 pounds or about 33.4 million newtons. As the rocket rose through the atmosphere, its thrust actually increased to almost nine million pounds due to the decreasing pressure of the surrounding air. At the same time, it got much lighter as it furiously burned its propellants. This caused the rocket's acceleration to increase to where it could have damaged its structure or the Apollo spacecraft on top. To keep acceleration under 4 "G's", the center or "inboard" engine was shut down about 26 seconds before the other four.
The saturn V first stage produced thirty-four mega newtons of thrust by five F-1 engines.
The amount of exposed surface area of the fuel
The weight of a Saturn V rocket just before launch is approximately 3 039 000 Kg.