Thursday, October 29, 2015

Space Shuttle Propulsion

                In my last couple of blogs, I have been writing about nuclear power. For this blog and the next few to follow, I will be talking about some things relating to space travel. The subject that I will be writing about in this post will be the problems with propulsion for space travel today. For simplicity, the space craft that I will be examining will be the Space Shuttle.
                 The first thing that is a major problem is the fuel. An amazing amount of fuel is required to get anything into space. The fuel for the space shuttle weighed a total of 3,869,475lb, or nearly 1935 tons of fuel! That is more than 23 times the weight of the empty shuttle itself!
There were three different types of fuel used in the Space Shuttle. One was a mixture of liquid hydrogen and liquid Oxygen. This was contained in the Space Shuttle external tank, weighing a total of 1,621,722lb. This burns almost invisibly, and is the fire that is coming out of the bottom of the shuttle itself. The second type of fuel was a mix of 69.6% ammonium perchlorate as an oxidizer, 16% aluminum as a fuel, .4% iron oxide to control burn speed, 12.04% PBAN (Polybutadiene acrylonitrile) to hold the fuel together and act as a secondary fuel, and 1.96% an epoxy curing agent. This was contained in the Space Shuttle Solid Rocket Boosters, weighing 1,100,000lb each for a total of 2,200,000lb. This is the fuel that causes the classic huge plumes of smoke and fire during a launch. The last type of fuel used in the Space Shuttle was two chemicals that, when mixed, combusted to produce thrust. These two chemicals were monomethylhydrazine as a fuel, and dinitrogen tetroxide as an oxidizer. These were contained in the Space Shuttle Orbital Maneuvering System, with a combined weight of 47,753lb. These thrusters are small and mostly used in space, so you cannot see them during the launch.
All three of these fuels are either toxic and carcinogenic or cryogenically cooled, making them very difficult, expensive, and dangerous to handle. They also are impractical for more mass or longer travel, as this would require more fuel. This increase in fuel would need even more fuel to lift it. This means that at a certain amount of weight or distance to travel, it would simply require too much fuel or be too massive to achieve liftoff. In my opinion this needs much improvement. In my next blog, I will be writing about some ideas for improved fuel efficiency and different types of engines and fuels.

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