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I think I understand why objects heat up when going through the
atmosphere and therefore why re-entry vehicles need heat shielding. My question is why we don't need heat shielding when launching. Aren't we going through the same atmosphere? BigKhat |
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![]() wrote in message ups.com... I think I understand why objects heat up when going through the atmosphere and therefore why re-entry vehicles need heat shielding. My question is why we don't need heat shielding when launching. Aren't we going through the same atmosphere? BigKhat Not as fast. Less energy == less friction == less surface heating. |
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Most launch vehicles first go pretty much straight up to get past the
atmosphere. They use compact, high thrust, but not necessarily efficent, propellents like kerosene or solid fuel to lift the stack above most of the air, while minimizing the cross-section. It is only when they are free of the bulk of the atmosphere that they tilt over to get the horizontal velocity required for orbit. There they can use much more efficent, but slower burning and bulkier fuels like hydrogen. For example, the shuttle primarily uses solids for the first couple of minutes, which have high thrust, a narrow cross-section but dont last long. Once it drops the SRBs, it is essentially moving horizontally, burning hydrogen for six more minutes to reach orbital velocity. All that energy, of course, has to be expended within the atmosphere during entry. |
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I think I understand why objects heat up when going through the atmosphere and therefore why re-entry vehicles need heat shielding. My question is why we don't need heat shielding when launching. Aren't we going through the same atmosphere? Heres why. When you launch from the ground, you start moving through the thickest air you are going to encounter, but you are moving through it very *very* slowly, relative to the speeds when coming back in. When the shuttle, or any re-entering spacecraft coming in from orbit, starts to hit air, granted very thin air very high up, the spacecraft is flying at about 17,400 MPH, or about *five miles per second*. Wheras, on the way up, you don't hit such speeds until you're far more out of the athmosphere. And, on the way up, as you accelerate, the air is thinning out even faster, while on the way down, you need that air drag to slow you down, so you don't stick your pointy nose through it, but you point the thickest and widest part of your spacecraft frontwise so that you can catch more of the air, so that it's drag can slow you down. And, all that air drag does slow you down, from orbital speeds of five miles per second, to the 180 MPH speed of when the shuttle's tires contact the runway. Thats a lot of slowing down, and the air does it all for you, but in the process, it makes a LOT of heat as a result. Does that help ? Andre -- " I'm a man... But, I can change... If I have to... I guess. " The Man Prayer, Red Green. |
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![]() wrote: I think I understand why objects heat up when going through the atmosphere and therefore why re-entry vehicles need heat shielding. My question is why we don't need heat shielding when launching. Aren't we going through the same atmosphere? 1) Launchers often DO need heat shielding during launch. The nose of the shuttle's external tank is darkened and scorched a bit by launch. Notice how the nose of the ET is darkened here compared to the sides: http://www.orbit6.com/et/img/etank2.jpg But in this picture, the nose is the same color as the rest of the tank: http://www.orbit6.com/et/img/91etksc2.jpg 2) Yes, it's the same atmosphere, but the rocket is moving much slower during launch than re-entry. During launch, rockets are generally moving at only a couple thousand miles per hour before they're above most of the atmosphere. During re-entry, they hit the atmosphere at 17500mph. Mike Miller |
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