8 million pounds
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∙ 12y agov = a t a = v / t Bonus: t = v / a
If the true value is t and the calculated or measured value is v then absolute error = |v - t|, the absolute value of (v - t).If v >= t then the absolute value is v - tif v
It depends on the speed: t = s/v
what is VVT-I
I assume that the "speed" equation is velocity equals distance divided by time (v=d/t). To get 't' on the left side, we'll multiply both sides by 't': (vt=dt/t) and the two 't's on the right side cancel out (because t divided by t is 1): (vt=d). Now we move the v to the right side by dividing both sides by 'v': (vt/v=d/v). Just the 't's in the step before, now we have a v divided by a v on the left side, so they cancel out, and our final equation is time equals distance divided by velocity: t=d/v
The saturn V first stage produced thirty-four mega newtons of thrust by five F-1 engines.
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.
None! NASA decomissioned Saturn V years ago - see: "How many humours are there in the human body?"
The F-1 engines used on the first stage of the Saturn V rocket produced about 1.5 million pounds of thrust each.
The Saturn V produced about 7.5 million pounds of thrust at liftoff, generated by its five powerful F-1 engines in the first stage. This immense power was needed to propel the large and heavy rocket off the ground and into space.
5 Million Newtons was the pressure exerted by Saturn v rocket
The Saturn V rocket weighed approximately 6.2 million pounds (2.8 million kg) when fully fueled and ready for launch.
Just 1, although it had multiple stages. To Clarify The Saturn V Rocket is a 3 stage rocket system as the Americans like to say The First stage had five individual main thrust engines Second had three Third stage had one
The Saturn V rocket did not land on the moon itself, but it was the launch vehicle that carried the Apollo spacecraft to the moon. The Apollo spacecraft then separated from the Saturn V rocket and landed on the moon during the Apollo missions. The first successful manned moon landing was Apollo 11 in 1969.
The rocket that launched the Apollo spacecrafts was the Saturn V. There were no Apollo rockets that began with a T
The "Saturn V" rocket was named after the Roman god, Saturn, and the "V" represented the five powerful F-1 engines used in its first stage.
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)