#1
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KSC - what if
As we all know, KSC as we know it today really started as a facility to
launch missions to the Moon for the Apollo program. The VAB was designed to accommodate the Saturn V, and pads 39A, 39B and the fabled 39C were set up to facilitate mankind's assault on our nearest celestial neighbour. These facilities were designed around the Saturn-V, with the smaller Saturns also easily handled. The pads were situated far enough away from the manned facilities on the basis of blast radius (if something went seriously wrong) and acoustic range. Now, let's assume funding for Apollo continued rather than was axed, and let's assume Apollos 18 through 20 happened. Let's also assume the shuttle program commences in 1972 and is developed rapidly in a comparatively linear fashion, without the modifications suffered by what we know today; and with the shuttle AAP blossoms, with SkyLab being saved by a shuttle in 1978, and SkyLab II flying being serviced by shuttle instead of Saturn 1Bs. The decision is made to extend AAP to include a larger format space labs and the beginnings of an extended lunar research program, and so the Saturn-V variants are brought on board, like the Saturn MLV-V-4(S)-A, the Saturn MLV-V-4(S)-B, or even the Saturn V-23(L) or Saturn V-4X(U). With these larger vehicles and a greater level of activity (to say nothing of the increased diversity of launch vehicles), the existing infrastructure at KSC would hardly be up to the challenge. For starters, the VAB would be too small to accommodate the larger Saturns. Secondly, the pads might not be large enough. The LUTs wouldn't be large enough either, and with that all the pad infrastructure. With increased capacity comes increased power and therefore a larger blast radius should one of them go off on the pad, so the pads themselves might suddenly be found to be too close to the manned facilities. So - would NASA be forced to relocate operations, or would there be enough room at KSC to expand infrastructure so these monster rockets could operate from an established facility? Would the VAB be extended or would a newer building be established adjacent to it for larger vehicles? Would pads 39A and B be reserved for shuttle and new pads have to be built to accommodate the new run of Saturns, or would KSC be left as is and another facility entirely (Hawaii? Texas?) be constructed to run the larger systems? David -- per aspera ad astra |
#2
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David Sander wrote: So - would NASA be forced to relocate operations, or would there be enough room at KSC to expand infrastructure so these monster rockets could operate from an established facility? They woudl expand ops at Kennedy. They had plans for just that. I've got maps for the Post-Saturn launch pads around here, somewhere... Would the VAB be extended or would a newer building be established adjacent to it for larger vehicles? The VAB was big enough to handle any likely development of the Saturn. The *really* tall versions of Saturn would have required a crane mounted on top of the VAB, and final stacking occurs just outside the building. The VAB's capabilities as far as faster proccessing were never really put to the test. Would pads 39A and B be reserved for shuttle and new pads have to be built to accommodate the new run of Saturns, or would KSC be left as is and another facility entirely (Hawaii? Texas?) be constructed to run the larger systems? There were some semi-serious proposals for Hawaiian launch of the Nova rocket, but the logistics of the situation were basically prohibitive. Not that there wouldn't have been a bunch of NASA and contractor employees scrambling to get hired on in Hawaii.... I think the real trick would have been in getting Saturn V and Shuttle operating simultaneously. |
#3
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Scott Lowther wrote:
The VAB was big enough to handle any likely development of the Saturn. The *really* tall versions of Saturn would have required a crane mounted on top of the VAB, and final stacking occurs just outside the building. The VAB's capabilities as far as faster proccessing were never really put to the test. What about width though? The larger variants with SRBs or even liquid-fuelled strap-on boosters would have made any vehicle rather broad - the VAB's internal structure - and its doorways - barely appear capable of accommodating such a size. David -- per aspera ad astra |
#4
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"David Sander" wrote in message ... So - would NASA be forced to relocate operations, or would there be enough room at KSC to expand infrastructure so these monster rockets could operate from an established facility? Would the VAB be extended or would a newer building be established adjacent to it for larger vehicles? Would pads 39A and B be reserved for shuttle and new pads have to be built to accommodate the new run of Saturns, or would KSC be left as is and another facility entirely (Hawaii? Texas?) be constructed to run the larger systems? Lots of assumptions here... For one, that we'd outgrow the Saturn V or the simpler deratives anytime soon. I'm not convinced we would have. But... assuming that... I'm not convinced you would need separate pads for Shuttle (assuming the current design) and Saturn V. You'd need different MLPs for sure, but as the Saturn MLP contained everything it needed, you'd simply launch from that and ignore the RSS and like for the Shuttle, and vice versa. So, you'd probably need another MLP or two. Only two bays of the VAB have ever been outfitted for stacking. However, now VAB bay 2 is available as a "storm shelter" and you need room for storage and the ilke. So you may have been able to get away with keeping two bays for shuttle and 2 for Saturn and derivatives. And then of course the current design left room for up to 4 more bays. Outgrow that and then simply build across the "road" another VAB. And there was room (and I've seen one map) that shows room for 39D-F. The "drive" time from the VAB would have been VERY long though. So, I think KSC could have supported almost any realistic plans. David -- per aspera ad astra |
#5
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David Sander wrote: Scott Lowther wrote: The VAB was big enough to handle any likely development of the Saturn. The *really* tall versions of Saturn would have required a crane mounted on top of the VAB, and final stacking occurs just outside the building. The VAB's capabilities as far as faster proccessing were never really put to the test. What about width though? The larger variants with SRBs or even liquid-fuelled strap-on boosters would have made any vehicle rather broad - the VAB's internal structure - and its doorways - barely appear capable of accommodating such a size. Didn't need to. They would be stacked at the pad. |
#6
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Greg D. Moore (Strider) wrote: "David Sander" wrote in message ... So - would NASA be forced to relocate operations, or would there be enough room at KSC to expand infrastructure so these monster rockets could operate from an established facility? Would the VAB be extended or would a newer building be established adjacent to it for larger vehicles? Would pads 39A and B be reserved for shuttle and new pads have to be built to accommodate the new run of Saturns, or would KSC be left as is and another facility entirely (Hawaii? Texas?) be constructed to run the larger systems? Lots of assumptions here... For one, that we'd outgrow the Saturn V or the simpler deratives anytime soon. I'm not convinced we would have. But... assuming that... I'm not convinced you would need separate pads for Shuttle (assuming the current design) and Saturn V. More than a few Shuttle concepts called for the use of Saturn V first stage, either expendable, or with wings bolted on. My understanding is that the Boeing/Grumman concept for a flyback S-IC with an ET on the nose and a Shuttle hanging off the side of the ET came *exceedingly* close to beating out the solid strap-on concept. |
#7
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In message , Scott Lowther
writes David Sander wrote: Scott Lowther wrote: The VAB was big enough to handle any likely development of the Saturn. The *really* tall versions of Saturn would have required a crane mounted on top of the VAB, and final stacking occurs just outside the building. The VAB's capabilities as far as faster proccessing were never really put to the test. What about width though? The larger variants with SRBs or even liquid-fuelled strap-on boosters would have made any vehicle rather broad - the VAB's internal structure - and its doorways - barely appear capable of accommodating such a size. Didn't need to. They would be stacked at the pad. But I thought the whole point of the VAB was that you didn't build the stack at the pad. -- What have they got to hide? Release the ESA Beagle 2 report. Remove spam and invalid from address to reply. |
#8
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David Sander wrote: Would pads 39A and B be reserved for shuttle and new pads have to be built to accommodate the new run of Saturns, or would KSC be left as is and another facility entirely (Hawaii? Texas?) be constructed to run the larger systems? If they had any brains, it would be off to Christmas Island; almost exactly on the equator, and lots of nice empty sea off to its east. This got anything to do with MCS? How's everything going on that, anyway? Pat |
#9
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Scott Lowther wrote: There were some semi-serious proposals for Hawaiian launch of the Nova rocket, but the logistics of the situation were basically prohibitive. Not that there wouldn't have been a bunch of NASA and contractor employees scrambling to get hired on in Hawaii.... IIRC, NASA bought the land for the Nova pads at KSC; I wonder what ever became of that? I think the real trick would have been in getting Saturn V and Shuttle operating simultaneously. That would have been a real logistical nightmare, wouldn't it? You'd be dealing with Lox/Kerosene, Lox/LH2, and solids all at once- not to mention possibly trying to make the pads compatible for both types of vehicles... at this point, a horizontal take-off variant of the Faget design starts looking attractive. You could have a separate "Horizontal Assembly Building" to place the orbiter on top of the fly-back booster. Pat |
#10
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More than a few Shuttle concepts called for the use of Saturn V first stage, either expendable, or with wings bolted on. My understanding is that the Boeing/Grumman concept for a flyback S-IC with an ET on the nose and a Shuttle hanging off the side of the ET came *exceedingly* close to beating out the solid strap-on concept. thats really sad the saturn booster stage didnt win. much safer operations all these years. more importandly the saturn techniology would of had a chance to evolve, and mature. ith the saturn family still around, ISS could of been built easier in just a few pieces, and we would still of had heavy lift capacity. what a screw up......... .. .. End the dangerous wasteful shuttle now before it kills any more astronauts.... |
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