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Reading a book about the X-15 program. Says that the pilots
hand-flew the reentry on the missions to space, the highest mission was 67 miles and several minutes outside of the atmosphere. Initial planning was for missions as high as 180 miles; that would obviously have been a much longer and higher speed reentry, I wonder if the pilot could hand-fly it? Don't think there was any automated way to do it back in the 1960s. Would it be possible for the pilots to hand-fly a space shuttle reentry? Or would an automatic system be required given the exacting parameters on a reentry from orbit? |
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In article ,
says... Reading a book about the X-15 program. Says that the pilots hand-flew the reentry on the missions to space, the highest mission was 67 miles and several minutes outside of the atmosphere. Initial planning was for missions as high as 180 miles; that would obviously have been a much longer and higher speed reentry, I wonder if the pilot could hand-fly it? Don't think there was any automated way to do it back in the 1960s. Actually there were electronics to help fly the aircraft. I Believe these were all analog (you can actually do a lot with analog control systems). But, there was no "modern" digital autopilot that would fly the entire reentry for them. Cite: Experience with the X-15 Adaptive Flight Control System https://www.nasa.gov/centers/dryden/...main_H-618.pdf Would it be possible for the pilots to hand-fly a space shuttle reentry? Or would an automatic system be required given the exacting parameters on a reentry from orbit? The pilot was trained to fly the shuttle manually during pretty much all stages of flight. But you can't fly a space shuttle with zero computers. The space shuttle has a digital control system (i.e. fly by wire). There were no cables connecting the flight controls directly to the control surfaces. Control surfaces were hydraulic and powered by the shuttle's APUs. That's why the shuttle had 4 redundant computers to control it (in case of hardware failure). It also had a fifth computer with completely different, but minimal, flight control software in case a software failure caused the 4 main computers to fail. Jeff -- All opinions posted by me on Usenet News are mine, and mine alone. These posts do not reflect the opinions of my family, friends, employer, or any organization that I am a member of. |
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On Tuesday, January 16, 2018 at 6:32:51 AM UTC-5, Jeff Findley wrote:
In article , says... Reading a book about the X-15 program. Says that the pilots hand-flew the reentry on the missions to space, the highest mission was 67 miles and several minutes outside of the atmosphere. Initial planning was for missions as high as 180 miles; that would obviously have been a much longer and higher speed reentry, I wonder if the pilot could hand-fly it? Don't think there was any automated way to do it back in the 1960s. Actually there were electronics to help fly the aircraft. I Believe these were all analog (you can actually do a lot with analog control systems). But, there was no "modern" digital autopilot that would fly the entire reentry for them. Cite: Experience with the X-15 Adaptive Flight Control System https://www.nasa.gov/centers/dryden/...main_H-618.pdf Would it be possible for the pilots to hand-fly a space shuttle reentry? Or would an automatic system be required given the exacting parameters on a reentry from orbit? The pilot was trained to fly the shuttle manually during pretty much all stages of flight. But you can't fly a space shuttle with zero computers. The space shuttle has a digital control system (i.e. fly by wire). There were no cables connecting the flight controls directly to the control surfaces. Control surfaces were hydraulic and powered by the shuttle's APUs. That's why the shuttle had 4 redundant computers to control it (in case of hardware failure). It also had a fifth computer with completely different, but minimal, flight control software in case a software failure caused the 4 main computers to fail. One of the books about the X-15 said that reentry had to be flown very precisely, as even at the best, it was close to the limits for heating on the airframe, g-forces on the airframe, aerodynamic forces on the airframe, and g-forces on the pilot. A small amount of miscalculation could push one or more of them beyond the danger point. That is why the limited the altitude flights to around 350,000 feet or 67 miles. |
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