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Boeing's thinking bigger, and MUCH bigger.
Taking the Delta 4's inherant modularity, Boeing is considering major upgrades to the Delta 4 Heavy that could eventually take it to a Saturn V class (albeit heavily modified). http://www.boeing.com/defense-space/...2004-03-01.pdf Upgraded versions using modified existing pad structures would have a payload range of 30 to 45 metric tons to LEO and about 10 to 18 metric tons to escape velocity. Using a new pad structure and using from 5 to 7 CBCs with other upgrades, payload would range upwards to about 90 metric tons to LEO and around 35 tons to escape. In physical size alone, it would be about as large as the Saturn V due to its all-cryogenic tankage. A new 7-meter CBC with a BIG new cryo engine would start at Saturn V payloads. Shades of the M-1 and Nova, is all I can say.... There would be various upgrades of existing system as hinted at in the above document, more than I'll try to list here. The upper stage will have to grow, a lot, including the use of multiple RL or MB-60s, or even a new cryo engine. The RS-68 would also grow, and densified propellants are suggested, too. Naturally, LM will be thinking similar things with the Atlas V. Who needs Shuttle C, eh? Modular's the way to go. --Damon |
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"Damon Hill" wrote in message
34... Boeing's thinking bigger, and MUCH bigger. Taking the Delta 4's inherant modularity, Boeing is considering major upgrades to the Delta 4 Heavy that could eventually take it to a Saturn V class (albeit heavily modified). http://www.boeing.com/defense-space/...2004-03-01.pdf Upgraded versions using modified existing pad structures would have a payload range of 30 to 45 metric tons to LEO and about 10 to 18 metric tons to escape velocity. Using a new pad structure and using from 5 to 7 CBCs with other upgrades, payload would range upwards to about 90 metric tons to LEO and around 35 tons to escape. In physical size alone, it would be about as large as the Saturn V due to its all-cryogenic tankage. A new 7-meter CBC with a BIG new cryo engine would start at Saturn V payloads. Shades of the M-1 and Nova, is all I can say.... There would be various upgrades of existing system as hinted at in the above document, more than I'll try to list here. The upper stage will have to grow, a lot, including the use of multiple RL or MB-60s, or even a new cryo engine. The RS-68 would also grow, and densified propellants are suggested, too. Naturally, LM will be thinking similar things with the Atlas V. Who needs Shuttle C, eh? Modular's the way to go. --Damon Damon I agree that "Modular's the way to go". You have, without realising it, answered two of my main questions: What diameter would the New Booster Core be? and the really big question: Is this possible? Answer to the first question is: 7 metres and the second question is answered with an emphatic "Yes". I have to say that I don't like the idea of adding the GEM solids to the current configuration as it would be hugely complicated. However, the configuration with seven CBC's and two MB-60's is of great interest. Payload is much higher than I had anticipated and even higher than I dared hope for. I feel the NBC (the 7 metre core as mentioned in the .pdf)/4xCBC combination is the best way to go, but the payload can be easily achieved with just CBC's, then there is almost _no_ development cost. This beats anything I could have hoped for, let alone come up with. Thank you! ![]() -- Alan Erskine We can get people to the Moon in five years, not the fifteen GWB proposes. Give NASA a real challenge |
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"Alan Erskine" wrote in
: I agree that "Modular's the way to go". You have, without realising it, answered two of my main questions: What diameter would the New Booster Core be? and the really big question: Is this possible? Answer to the first question is: 7 metres and the second question is answered with an emphatic "Yes". That and a new pad infrastructure; hopefully a rail-mobile launch platform. Though I suspect Boeing and NASA are thinking that Delta 4 Huge would use VAB and a modified MLP. I do wish they'd located the manufacturing in the local area instead of in Alabama. I have to say that I don't like the idea of adding the GEM solids to the current configuration as it would be hugely complicated. However, the configuration with seven CBC's and two MB-60's is of great interest. Payload is much higher than I had anticipated and even higher than I dared hope for. I don't think that'd be too complicated, other than the modifications to the core CBC, since the mounting points would have to be moved 90 degrees and the pad connections would need additional protection. But otherwise there aren't many big changes in the existing design. A more powerful upper stage will be essential, and even clusters of RL/MB 60s might be marginal. Maybe RLX, a much larger expander cycle P&W's been studying. I feel the NBC (the 7 metre core as mentioned in the .pdf)/4xCBC combination is the best way to go, but the payload can be easily achieved with just CBC's, then there is almost _no_ development cost. This beats anything I could have hoped for, let alone come up with. Thank you! ![]() I thought you'd enjoy this. ![]() possibilities without breaking the bank for an all-new launch system, or the relatively inflexible Shuttle-C type concepts. Delta IV Huge, I like that idea... ![]() --Damon |
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On Fri, 28 May 2004 02:40:30 -0500, Damon Hill
wrote: Boeing's thinking bigger, and MUCH bigger. Taking the Delta 4's inherant modularity, Boeing is considering major upgrades to the Delta 4 Heavy that could eventually take it to a Saturn V class (albeit heavily modified). http://www.boeing.com/defense-space/...2004-03-01.pdf which claims... "Once in service, the Delta IV Heavy will be the world’s most powerful launch vehicle, able to place 13,160 kg (28,950 lb) into geosynchronous transfer orbit. Built for the U.S. Air Force’s Evolved Expendable Launch Vehicle program, the rocket is second in size only to the enormous Saturn V rocket that lifted Apollo into space." Er, pay no attention to that behemoth on the other side of the Banana River. Space Shuttle? What Space Shuttle? Brian |
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"Brian Thorn" wrote in message
... On Fri, 28 May 2004 02:40:30 -0500, Damon Hill wrote: Boeing's thinking bigger, and MUCH bigger. Taking the Delta 4's inherant modularity, Boeing is considering major upgrades to the Delta 4 Heavy that could eventually take it to a Saturn V class (albeit heavily modified). http://www.boeing.com/defense-space/...2004-03-01.pdf which claims... "Once in service, the Delta IV Heavy will be the world's most powerful launch vehicle, able to place 13,160 kg (28,950 lb) into geosynchronous transfer orbit. Built for the U.S. Air Force's Evolved Expendable Launch Vehicle program, the rocket is second in size only to the enormous Saturn V rocket that lifted Apollo into space." Er, pay no attention to that behemoth on the other side of the Banana River. Space Shuttle? What Space Shuttle? Brian Perhaps they're referring to payload capacity as opposed to physical 'size'. -- Alan Erskine We can get people to the Moon in five years, not the fifteen GWB proposes. Give NASA a real challenge |
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"Alan Erskine" wrote in
: "Brian Thorn" wrote in message ... "Once in service, the Delta IV Heavy will be the world's most powerful launch vehicle, able to place 13,160 kg (28,950 lb) into geosynchronous transfer orbit. Built for the U.S. Air Force's Evolved Expendable Launch Vehicle program, the rocket is second in size only to the enormous Saturn V rocket that lifted Apollo into space." Er, pay no attention to that behemoth on the other side of the Banana River. Space Shuttle? What Space Shuttle? Perhaps they're referring to payload capacity as opposed to physical 'size'. Perhaps so was Brian. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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"Jorge R. Frank" wrote in message
... "Alan Erskine" wrote in : "Brian Thorn" wrote in message ... "Once in service, the Delta IV Heavy will be the world's most powerful launch vehicle, able to place 13,160 kg (28,950 lb) into geosynchronous transfer orbit. Built for the U.S. Air Force's Evolved Expendable Launch Vehicle program, the rocket is second in size only to the enormous Saturn V rocket that lifted Apollo into space." Er, pay no attention to that behemoth on the other side of the Banana River. Space Shuttle? What Space Shuttle? Perhaps they're referring to payload capacity as opposed to physical 'size'. Perhaps so was Brian. Shuttle payload up to 23 tonnes. Delta IV Heavy payload up to 23.5 tonnes. -- Alan Erskine We can get people to the Moon in five years, not the fifteen GWB proposes. Give NASA a real challenge |
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"Alan Erskine" wrote in
: "Jorge R. Frank" wrote in message ... "Alan Erskine" wrote in : "Brian Thorn" wrote in message ... "Once in service, the Delta IV Heavy will be the world's most powerful launch vehicle, able to place 13,160 kg (28,950 lb) into geosynchronous transfer orbit. Built for the U.S. Air Force's Evolved Expendable Launch Vehicle program, the rocket is second in size only to the enormous Saturn V rocket that lifted Apollo into space." Er, pay no attention to that behemoth on the other side of the Banana River. Space Shuttle? What Space Shuttle? Perhaps they're referring to payload capacity as opposed to physical 'size'. Perhaps so was Brian. Shuttle payload up to 23 tonnes. Delta IV Heavy payload up to 23.5 tonnes. That shuttle figure is for the LWT. The SLWT adds a few tons to payload capacity. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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http://www.astronautix.com/stages/shuttank.htm
3.5 tonne payload increase. -- Alan Erskine We can get people to the Moon in five years, not the fifteen GWB proposes. Give NASA a real challenge |
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