The question isn't very meaningful because rockets don't work like regular engines or motors.
A gasoline engine or electric motor produces a certain force (torque) at a certain speed (RPM). Multiplying torque by speed gives output power, which can be measured in horsepower or watts. A motor can produce more force at a lower speed, or less force at a higher speed while still producing the same power.
But rockets produce a force (thrust) that doesn't depend on speed. If you bolt a rocket to a test stand so it can't move, then it can't produce any power at all no matter how much propellant it burns or thrust it generates. Only when the rocket can move will it develop mechanical power. That power will increase with speed even when thrust remains constant.
But if we redefine the "power" of a rocket as the rate at which it burns fuel and produces heat, we can come up with a well-defined number. The F-1 engines on the first stage of the Saturn V burned RP-1 (Rocket Propellant 1), a specially refined form of kerosene, and the five engines burned it at a total rate of about 4 tonnes (4000 kg) every second. Burning RP-1 yields about 43 megajoules of energy per kilogram, so that's works out to a heat power of 564 gigawatts or 757 million horsepower.
By comparison, the average amount of electricity generated in the entire United States averaged 455 gigawatts during 2010. That's right, the Saturn V produced more power than the entire US electric grid (on average), but of course it only did it for a couple of minutes.
The first stage of the Apollo rocket had about 7.5 million pounds of thrust, generated by five F-1 engines. This massive amount of thrust was needed to launch the rocket and overcome Earth's gravity.
The rocket to launch Apollo 13 was the Saturn 5 rocket.
The Saturn V rocket was the booster rocket used to launch all Apollo moon missions. It was the most powerful rocket ever built, standing over 360 feet tall and weighing over 6 million pounds.
The rocket that launched Apollo 3 was the Saturn IB rocket.
The rocket that was used for Apollo 11 was the Saturn five rocket.
1st stage developed 7,648,000 pounds force, 2nd stage developed 1,000,000 pounds force, 3rd stage developed 225,000 pounds force.
Apollo 11 was the name of the spaceflight as a whole, the rocket used was the Saturn V (Saturn 5). Figures of around 160 million horsepower at its peak have been brandished about, but a rockets power should really be measured by the thrust, in terms of pounds-force or Newtons. At its peak, the Saturn V rocket produced 7,648,000 pounds-force (34 million Newtons)
The first stage of the Apollo rocket had about 7.5 million pounds of thrust, generated by five F-1 engines. This massive amount of thrust was needed to launch the rocket and overcome Earth's gravity.
The rocket to launch Apollo 13 was the Saturn 5 rocket.
The Saturn V rocket was the booster rocket used to launch all Apollo moon missions. It was the most powerful rocket ever built, standing over 360 feet tall and weighing over 6 million pounds.
The rocket that launched Apollo 3 was the Saturn IB rocket.
The rocket that was used for Apollo 11 was the Saturn five rocket.
Apollo 13 and all the Apollo spacecrafts were launched aboard a Saturn V rocket.
The type of rocket that launced Apollo 11 into space is the same type of rocket that was used for all Apollo launchings. The Saturn V (five) multistage rocket was used.
The rocket chosen for the Apollo mission was the Saturn 5.
The Apollo 11 was launched on 16/7/1969.
The rocket that launched the Apollo spacecrafts was the Saturn V. There were no Apollo rockets that began with a T