v = 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 F-1 engines used on the first stage of the Saturn V rocket produced about 1.5 million pounds of thrust each.
None! NASA decomissioned Saturn V years ago - see: "How many humours are there in the human body?"
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.
A Saturn V rocket could produce up to 7.5 million pounds of thrust at liftoff, making it one of the most powerful rockets ever built. This immense thrust was generated by the five massive F-1 engines in the first stage of the rocket.
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 had five rocket engines in its first stage, called the F-1 engines. These engines were responsible for providing the necessary thrust to lift the rocket off the ground and into space.
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.
There were eleven main engines on the Saturn V. Five on the first stage, five on the second stage and one on the third stage. This does not count the engine on the lunar lander. How do I know? I worked as an Aerospace Engineer on the first stage of the Saturn V during Apollo. My partner and I were the ONLY two women working on the Saturn V. Sara Howard, Author of "Something Funny Happened on the Way to the Moon" and "The Greatest Explosions in the Universe."
The Saturn V rocket used a combination of liquid oxygen and RP-1, a refined form of kerosene, as fuel. These propellants were used in the first stage of the rocket to provide the thrust needed for liftoff.
Yes, "Saturn V" and "Saturn 5" are referring to the same rocket. The correct designation is "Saturn V," with the "V" representing the Roman numeral for five.