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I was just watching the gemini DVD again. It said that an ejection
from the capsule probably wouldn't have been survivable because of the speed. why didn't Gemini use the escape tower like Mercury and Apollo? |
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Dale wrote:
I was just watching the gemini DVD again. It said that an ejection from the capsule probably wouldn't have been survivable because of the speed. why didn't Gemini use the escape tower like Mercury and Apollo? Henry Spencer answered this several years ago. Hopefully it's OK for me to simply repost what he wrote then: The switch to ejection seats apparently was motivated mostly by saving weight.... There's no doubt that using ejection seats saved weight, but was that the *main* reason? According to Jim Chamberlin (chief designer of the Mercury Mark II and Gemini's first project manager), much of it was motivated by his personal distaste for the complexity of the Mercury escape tower and associated automatic sequencing system, the large amount of time required to check out the system before flight, and associated penalties regarding reliability. See: On The Shoulders of Titans http://history.nasa.gov/SP-4203/ch2-5.htm The new design attacked a number of other Mercury trouble spots. Perhaps the most troublesome was the sequencing system. Chamberlin argued that one of his chief motives for keeping systems in the new design separated was to avoid the endless complications Mercury experienced because so many sequentially controlled operations were built into it. ..... What may have been the most complex sequencing of all was demanded by the automatic abort modes in Mercury, which depended on a rocket-propelled escape tower to pull the capsule away from the booster in an emergency during or just after liftoff. In Chamberlin's mind, "the sequencing of the escape system was one of the major problem areas in Mercury in all its aspects - its mechanical aspects in the first part of the program, and the electronic aspects later." .... [Chamberlin's] active distaste for escape towers made him eager to include ejection seats in his design. .... Titan II had power to spare, its total thrust being almost two and a half times that of Atlas. Not only could it easily lift the heavier spacecraft, but it could also carry the redundant systems that would make it a safer booster for manned space flight. .... Ejection seats not only promised to relieve a major source of trouble by getting rid of the escape tower, but they also furthered the concept of modularization, keeping each spacecraft system, so far as possible, independent. "The paramount objective in the program," according to Chamberlin, "was to dissociate systems." Ejection seats, in what he called "very happy coincidence that was fully realized at the time," also fitted in nicely with another design change, substituting paraglider for parachute recovery. - - - So, the Titan II and its propellants made it possible and the weight savings were a bonus, but it appears that the Chamberlin's desire to simplify Mercury systems, particularly the automatic sequencer, that persuaded him to replace the escape tower with ejection seats. -- Dave Michelson |
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![]() Pat Flannery wrote: Originally it was intended to recover Gemini on land using an inflatable Rogallo parawing and skids, and the ejection seats would have allowed the crew to escape if it didn't deploy correctly. This wasn't from the beginning of the program which used parachutes for recovery, but it did get as far as manned landing attempt which resulted in a crash, so the concept got dropped. One fallout of this was the horizontal landing attitude of the Gemini compared to the heatshield-first landing of Mercury and Apollo. Pat |
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On Sun, 26 Nov 2006 09:31:42 GMT, Dave Michelson wrote:
Dale wrote: I was just watching the gemini DVD again. It said that an ejection from the capsule probably wouldn't have been survivable because of the speed. why didn't Gemini use the escape tower like Mercury and Apollo? Henry Spencer answered this several years ago. Hopefully it's OK for me to simply repost what he wrote then: The switch to ejection seats apparently was motivated mostly by saving weight.... There's no doubt that using ejection seats saved weight, but was that the *main* reason? According to Jim Chamberlin (chief designer of the Mercury Mark II and Gemini's first project manager), much of it was motivated by his personal distaste for the complexity of the Mercury escape tower and associated automatic sequencing system, the large amount of time required to check out the system before flight, and associated penalties regarding reliability. snip Maybe the real answer as to why they chose ejection seats is simply because they could? ![]() option at the end of the flight, should the envisioned parawing fail. It seems to me that the experience gained with Mercury should have lessened the automatic sequencing hassles to be expected with Gemini. But simplicity is a virtue, regardless of whether or not an escape tower might have been easier to apply to Gemini after the lessons learned with Mercury. Ejection seats weren't an option with Apollo. Were the lessons learned with the Mercury escape system readily applied to Apollo, or were the two on separate but parallel design paths, and a lot of stuff had to be learned all over again with the Apollo LES? Dale Maybe you'll get an "I corrected an old and unauthorized repost from Henry" t-shirt, Dave ![]() |
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On Sun, 26 Nov 2006 03:54:11 -0600, Pat Flannery wrote:
Originally it was intended to recover Gemini on land using an inflatable Rogallo parawing and skids, and the ejection seats would have allowed the crew to escape if it didn't deploy correctly. This wasn't from the beginning of the program which used parachutes for recovery, but it did get as far as manned landing attempt which resulted in a crash, so the concept got dropped. One fallout of this was the horizontal landing attitude of the Gemini compared to the heatshield-first landing of Mercury and Apollo. At the beginning of the program, if the parawing hadn't been envisioned yet, were the parachutes to be in the nose of the craft? If so, how far along did the design get before the change? Was there any "fallout" from that? Sorry if these are dumb questions... Dale |
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Pat Flannery wrote:
Originally it was intended to recover Gemini on land using an inflatable Rogallo parawing and skids, and the ejection seats would have allowed the crew to escape if it didn't deploy correctly. If it didn't deploy correctly, wouldn't they just be ejecting into the failed parawing? All that cloth and the support lines would surely get in the way of a safe ejection if it partially deployed. Mark |
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![]() wrote in message oups.com... Pat Flannery wrote: Originally it was intended to recover Gemini on land using an inflatable Rogallo parawing and skids, and the ejection seats would have allowed the crew to escape if it didn't deploy correctly. If it didn't deploy correctly, wouldn't they just be ejecting into the failed parawing? All that cloth and the support lines would surely get in the way of a safe ejection if it partially deployed. No, since they could have ejected the failed parawing first. Mark |
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