0 Members and 1 Guest are viewing this topic.
quote:Originally posted by XinWhat exactly causes objects to burn up in our atmosphere? Is it simply friction, and that faster moving objects get hotter quicker? Or does the atmosphere function like a sort of magnifying glass and causes the sun's ray to superheat? I never hear of rockets leaving the Earth's atmosphere experiencing any sort of "burn" as they enter space...but perhaps I'm not educated enough
quote:Is it possible to ascend to Earth from space in a way that won't cause a "burn out" entering the atmosphere? Is it possible to extend a pole, wire, string, etc from the Earth and attach it to the Space Station or something else out in orbit?
quote:Originally posted by XinWhat exactly causes objects to burn up in our atmosphere? Is it simply friction, and that faster moving objects get hotter quicker? Or does the atmosphere function like a sort of magnifying glass and causes the sun's ray to superheat? I never hear of rockets leaving the Earth's atmosphere experiencing any sort of "burn" as they enter space...but perhaps I'm not educated enough Is it possible to ascend to Earth from space in a way that won't cause a "burn out" entering the atmosphere? Is it possible to extend a pole, wire, string, etc from the Earth and attach it to the Space Station or something else out in orbit?I know I'm asking a lot of questions...just not having much luck finding any useful answers via Google and the curiousity is haunting me.
quote:The airframe of the SR-71 is very unique. To withstand the friction-generated heat at Mach 3+, over 90 percent of the airframe is made of titanium composite. Also to withstand heat, the main gear tires have been impregnated with aluminum and are filled with nitrogen.
quote:An approximate rule-of-thumb used by heat shield designers for estimating peak shock layer temperature is to assume the air temperature in kelvins to be equal to the entry speed in meters per second. For example, a spacecraft entering the atmosphere at 7.8 km/s would experience a peak shock layer temperature of 7800 K. This method of estimation is a mathematical accident and a consequence of peak heat flux for terrestrial entry typically occurring around 60 km altitude.
quote:Due to the great temperature changes in flight, the fuselage panels did not fit perfectly on the ground and were essentially loose. Proper alignment was only achieved when the airframe warmed up due to the air resistance at high speeds, causing the airframe to expand several inches. Because of this, and the lack of a fuel sealing system that could handle the extreme temperatures, the aircraft would leak its JP-7 jet fuel onto the runway before it took off. The aircraft would quickly make a short sprint, meant to warm up the airframe, and was then air-to-air refueled before departing on its mission. Cooling was carried out by cycling fuel behind the titanium surfaces at the front of the wings (chines). Nonetheless, once the plane landed no one could approach it for some time as its canopy was still hotter than 300 degrees Celsius. Non-fibrous asbestos was also used, as in non-ceramic automotive brakes, due to its high heat tolerance.
quote:Originally posted by XinIs it possible to extend a pole, wire, string, etc from the Earth and attach it to the Space Station or something else out in orbit?
quote:Originally posted by Hadrian I wonder what sort of music they will use. Maybe it will be a new genre "space elevator music"