5 Million Newtons was the pressure exerted by Saturn v rocket
Bottle Rocket grossed $407,488 in the domestic market.
The average temperature at the "surface" of Saturn is about minus 150 degrees Celsius. In fact that doesn't vary much from poles to equator. So, there not much of a maximum and minimum.
If the nose is pointy, the rocket will go faster, but if the rocket's nose is flat, it will just travel slower in the lower atmosphere, the height a rocket attains depends on the efficiancy of its engines, the amount of propellant carried and the launch profile. However, for a subsonic rocket (which is what most hobby rockets are) then a curved on not a pointy one is much better. I would suggest looking it up on wikipedia.
Because it works much better for the purpose than a bicycle would.
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.
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 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.
can i put a 350 rocket that comes out of a 69 cuttless into my 1990 caprice
The amount of fuel a rocket burns during liftoff depends on the specific rocket and mission. On average, a rocket like the Falcon 9 may burn around 400,000 to 700,000 gallons of fuel during liftoff. The Saturn V rocket used for the Apollo missions burned approximately 20 tons of fuel per minute during liftoff.
The smoke that comes out of the bottom of a rocket is its "exhaust", much like the smoke and steam you see from a car's exhaust pipe on a cold day. But most of it you can't see : a huge volume of expanding hot gases. When rocket fuel "burns" (whether it is liquid hydrogen, kerosene, or solid propellant), it combines with oxygen to release incredible amounts of heat energy. The released gases (water vapor, carbon dioxide, and other compounds) are rapidly heated and violently expand, and the only way out is through the nozzles at the base of the rocket. This thunderous rush of gases zooms out of the rocket, and according to Newton's law of action and reaction, the rocket is pushed in the other direction, which is ideally "up." It takes a lot of energy to lift a heavy rocket against gravity, and accelerate it to the high speed (40000 km/hr, or 25000 mph) that it needs to reach orbit. Once in space, however, it will continue to move without much help as it circles the Earth.
The Apollo program, which included the mission that took Neil Armstrong to the moon, cost approximately $25.4 billion in the 1960s. The specific cost of the Saturn V rocket that carried Armstrong and his crew is estimated to be around $185 million.
The space shuttle is not capable of leaving low earth orbit, a rocket like what the Apollo missions used (although much bigger) would be required.
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.
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There is no ice cream on Saturn