Beat dem Ruskies to the moon! 2 D11 -P's and a D12 -3 Cluster will do it.

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We already had our second "Sputnik moment". It was on Sept 11, 2001.

I can see your point, but far more important and long-term in its effects on space will be the current financial mess... We're going to be looking at the "bad old days" of the 70's all over again, if we're LUCKY... Just like with Vietnam, this massive war spending, high energy costs, and shaky financial policy has led us into a financial mess that will take a LONG time to fix, if ever... and I'm fully convinced that we will see a LOT worse before it's all over with... and frankly, space is a VERY low priority... at least "civilian" space... DOD/AF has milspace covered, which is the part of space that has national security implications... NASA's manned and unmanned programs just flat aren't high priority missions, unlike the late 50's/early 60's where every manner of means for "dominating space" was being proposed and explored, and nobody really knew what was feasible and important and what wasn't, and everyone assumed that the enemy was going to "get there first" and control the planet via control of space. Therefore, NASA is MUCH more likely to see its budget continually shrink over the next decade or so, CERTAINLY not rise... If they're EXTREMELY lucky they might just manage to hold on to what they've got, simply because in the grand scheme of things it IS so small...

Financially, the optimal time to ever truly start cutting metal to build ships to go to Mars was near the end of the 1990's. The Cold War was over, and we had the money that could have been spent, if it was ever going to be spent. Well, actually, that did sort of happen, but in the form of ISS. And now the US has no means to send crews to the ISS, and in a few years (6 or so if they follow the plan like they did with killing the shuttle program) the ISS will outlive its useful life and be abandoned and de-orbited. And that will be another nail in the US manned space program's coffin, no more space stations.

ISS was a tremendous mistake... it's a nearly $200 billion dollar boondoggle that is basically performing the same sort of "effects on human health of long-term space missions in zero-gee" type stuff that the Russians have been doing on Salyuts and then Mir since the early 70's. (Granted, NASA considers the Russian numbers "garbage" and thus want to conduct their own research, their own way, and get their own conclusions, but we could have done this sort of thing on a MUCH smaller and simpler station.) Most of the ISS crew's time is taken up with maintenance and keeping the station running... very little is actually left over for science, and the flood of public/corporate research that was supposed to come flocking to ISS has never materialized (just like all the promises that industry would be tripping over each other to get into "space based manufacturing", which was the mantra used to justify shuttle in the 80's and early 90's before there was an ISS.) From everything I've read, the current plan is to keep ISS flying until at least 2020, so that's 8 years away... and it's quite likely that it will continue well past that. Mir was kept aloft for nearly a decade past it's 'replacement date'. Thing is, despite his faults, Griffin was right that we cannot afford to go anywhere else so long as we're spending money on ISS. Frankly, it's a shame that Space Station Freedom (which morphed into ISS after the Soviet collapse in 1991) didn't get canceled... because the main thing we've learned from it is how NOT to build a space station (mega-structure constructed from 20 ton modules brought up by dozens and dozens of flights of an expensive manned spaceplane). We could have done a lot more with the money that was wasted on ISS... but that's water under the bridge...

Missions to a near-Earth Asteroid? REALLY? For a "shakedown test flight" (Apollo-9 or 10 style) of a spacecraft truly designed to go to Mars, for real, yeah. But for any other reason, a spacecraft design that would not be sent to Mars, with some other design supposedly to be built years later for Mars, no.

Not sure what you're trying to say here. The only mission even manifested so far is a "loop round the moon" ala Apollo 8... not even sure they can drop into orbit or just loop around the moon like a Zond did in the late 60's (unmanned). I don't see that an asteroid mission would be particularly useful, honestly... an unmanned probe could land and conduct several "hops" to collect samples for return to Earth in a REAL laboratory capable of MUCH more in-depth study than possible in a spacecraft for a FRACTION of the cost of a manned mission. About the only thing of any "use" from the mission as far as "Mars precursor" operations might be long-term storage of cryogenic propellants (which IIRC isn't baselined) and experience with a deep-space hab they'd need for the trip (WAY too long to ride all the way out in Orion... it doesn't even have a toilet anymore!) Other than that, there's really NOTHING to be gained from an asteroid mission-- maybe communications and operations at long distances and deep space navigation... (but we've already got TONS of experience with that from the unmanned program). Long term life support should have to be proven out completely in LEO/L2 before any asteroid mission is contemplated... because if the ECLSS doesn't work, they're dead at those distances, period...

Some paranoid rabble-rousers might jump out of their shoes, but I don't see China doing anything space-wise that would cause the U.S. to suddenly jump into a solid, firm "yes we ARE really going to do it" commitment to go to Mars, that would actually truly "yes we DID it" happen.

China is moving forward, no doubt about it... and what they've done is truly impressive, and their plans for the future (if they turn out to be more than vaporware) should be equally impressive. They've managed to do so far what it took the US and Soviet Union dozens of flights over a decade to accomplish (first manned mission, rendezvous, spacewalk, and first space station). Their long-term plans are ambitious, but what it really has to do with us is to be seen... We've had one space race, and it was a dead end. We (foolishly) abandoned nearly the entire system and the vehicles we had developed, and essentially started from scratch with the shuttle, and we got a fragile, expensive system less capable than the one we had, and we've been stuck with it for 30 years. We certainly don't need another "space race" that leads to this sort of outcome...

I remember in the 1970s when we were 10 year from going to Mars. Then in the 1980's 15 years to Mars. And so on, every decade, we are another additional 5 years away from Mars.

Yep, Mars is always at least 20-30 years away. Despite all the talk, a manned Mars mission is no closer now than it was in 1972, 82, 92, 02, 12, or will be in 2022.

And by that I do not count the half-baked Project "Constellation", which might as well have been named Project "Constipation". Especially since it was sort of awkwardly announced in a low-key manner about 2 weeks before the State of the Union message and was not mentioned at all in the State of the Union message (that showed the level of non-support it actually had). Also the twisted logic of going to Mars, by NOT going to Mars, but going to be Moon for 10-15 (20? 25?) years first, with hardware that was not going to be useable for Mars, made no sense to me at all. If you want to go to Mars.... then by #%$ go to MARS, don't waste time and $ on anything beyond what is needed to safely achieve that goal.

Mars is an order of magnitude (or more) harder than any lunar mission. Basically we've got a LOT to learn about deep space manned operations, and frankly, the moon is the place to do it. We need experience building spacesuits that aren't falling apart after a day's work (on the moon, or at Mars), building and maintaining and repairing if needed spacecraft, systems, and equipment in deep space, on the lunar surface. If we can't repair stuff or keep it operating on the lunar surface, NO WAY will be able to keep it going at Mars. Yes, the landers used at Mars would be completely different than those used on the moon, but most of the SYSTEMS (life support, EVA, surface power, etc) would all be virtually identical to their lunar counterparts... only requiring integration in a Mars-capable lander. Plus, the moon is only 3 days away... Mars is a year away. I'm NOT saying we need a huge lunar base or even a permanent presence, but the moon is a valuable training ground that would be absolutely necessary to perfect the systems and verify their operation before sending them to Mars... Plus, we could accomplish a lot of good exploration work at the same time-- Apollo basically just scratched the surface, literally. When one is going to play in the superbowl, it's advisable to practice on their own field next door first. Besides, if we cannot afford lunar missions which will be an order of magnitude cheaper than ANY Mars mission, we cannot hope to afford a Mars mission which will doubtlessly cost many times more... In fact, the sheer COST of a Mars mission basically rules it out for the foreseeable future. NASA's "official" plans, the Design Reference Mission, which describes how NASA would conduct a Mars mission, currently would have about 8 or more SLS launches just to assemble the Mars-bound ship... This from a rocket that is projected to cost well over a billion per flight and only be launched about every other year... certainly doesn't inspire confidence... and seriously lacks reality... IMHO...

Heck, if Apollo had been scheduled to take 20-25 years, a long and slow approach like all the Mars plans of the last several years, it probably would have been cancelled half-way thru. Nixon cancelled Apollo with Saturn-V's and completed spacecraft left to be flown.

This is perhaps a valid assumption... it is an established fact that the longer you stretch out a program, the costlier it is on a per-mission basis, simply due to overhead. That's why SLS is on schedule to be the single most expensive space launch vehicle ever conceived... it won't fly often enough to justify the overhead needed to support it... (it'd be about like keeping a factory tooled up and staffed to build Corvettes, but only produce one every other year-- the cost per car would be absolutely staggering!) NASA, despite 50 years of experience and knowledge and computer tools and new materials and capabilities undreamed of during Apollo and Saturn development and operations, seems incapable of doing ANYTHING in less than a decade or more and spending many dozens of billions in the process... which is the MAIN reason that they're faltering...

On the other hand, we did a "crash" program to develop a lunar landing capability in the 60's, in less than a decade, and succeeded, but we created a system deemed "too expensive" (which turned out to be cheaper than shuttle, but that's in hindsight) to continue to operate, and we abandoned it and started over... So does it really matter that we succeeded, if it was a dead end?? (Not that it HAD to be... in fact, had Saturn flown enough to get some economies of scale, and if the improvements developed for the next series of Saturn vehicles been implemented (from among the many proposed evolutions of the Saturn vehicles, the F-1A engines and J-2S engines which were to be used on any second production run, which never happened) it's entirely possible we'd still be flying evolved versions of the basic Saturn hardware that got its start in the 60's, much as the Russians still fly evolved R-7 boosters and Soyuz capsules...

So pretty much any plan to go to Mars in the last 20-25 years, I think of the old Rocky & Bullwinkle cartoon where Bullwinkle tries to pull a rabbit out of his hat...... Again? That trick never works.

I gave up years ago expecting to live to see us land a crew on Mars, even if I have great health and live a long time.

I'd love to see that I'm wrong.....and see it happen. :)

- George Gassaway

I think you're right... We've tried crash programs (Apollo) and ended up abandoning it all as "too expensive"... (which was a mistake, but it can't be "undone" as it were). We've tried "cheap, routine access to space" via the shuttle (which was never cheap or routine, nor was it ever going to be... it was too compromised a design due to unrealistic demands and unrealistic expectations, combined with WILDLY optimistic self-delusional projections of operations costs, turnaround times, flight rates, and cargoes just "magically appearing" for it, which of course never materialized). Basically shuttle was known to be a dead end when Challenger was lost, but nobody could or would admit it (or allowed it to be admitted). So, instead, we "soldiered on" with a flawed and brittle and very expensive system, built around missions and presumptions and payloads that never happened. Then, to give it a reason to exist, we tried shoehorning experimentation, science, and "research" into it, despite it's very limited capability to remain on-orbit long enough to accomplish anything substantial. Then we tried to sell "research and orbital manufacturing" to the industrial world as a reason for shuttle to exist... nobody would bite and shuttle was left flying missions to see how cockroaches reacted to zero gee and taking blood samples and such trying to justify manned space missions and the shuttle itself. Finally, we created the reason to keep shuttle alive, by designing a space station to be constructed by it, basically the ONLY remaining reason that shuttle had been sold on originally that hadn't been tried... (commercial satellite launch and retrieval was a failure, because it was WAY more expensive to design satellites with the necessary safety margins for launch in a manned vehicle, and the operations costs were much higher for a manned vehicle, and therefore launch costs... and nobody really wanted their satellites back; by the time they broke down they were obsolete anyway-- the main takers for satellite retrieval/repairs were satellites stuck in useless orbits due to launch vehicle failures... but of course shuttle launch/ops costs were SO high that it was never a paying proposition... better to just launch a new satellite... heck even shuttle's "shining star", Hubble repair, was SO expensive to conduct that duplicates of Hubble could have been launched for what it cost to repair the original... nevermind the opportunity cost of Hubble being stuck in LEO so shuttle could launch/service it... which is about the worst orbit possible for astronomical observations. The DOD/AF grand plans for blue-suit spaceflight, launching spysats or flying special observation platforms into polar orbits from California over the poles and landing back in California after a single orbit, or futzing around with Russian satellites in space and all the other claptrap that the military used to justify getting their own shuttle (originally Discovery was to be the "air force shuttle" and was due to be transferred to Vandenberg and launched on the first all-Air Force shuttle mission into polar orbit not long after Challenger... which of course torpedoed all those plans-- no shuttle ever flew from California into space or into polar orbit period. Supposed research and manufacturing that industry would be knocking the doors down at NASA to get aboard shuttle or a space station to do simply never materialized... just as it hasn't for ISS). IMHO, we should have retired shuttle after Challenger and simply developed a "shuttle derived" launcher then, as the National Launch System and Advanced Launch System studies proposed doing... and replaced shuttle with a smaller, more robust space taxi (capsule or small Dreamchaser/HL-20 like spaceplane). In fact, this was proposed back when the shuttle was first being explored as a proposal-- a small reusable spaceplane on an expendable booster designed for minimum costs. But "reusability" was the "holy grail" of spaceflight at the time, and anything not fully or almost fully reusable simply was blown off... of course now we know, as shuttle manager John Shannon told the Augustine Committee, that "reusability is a myth" and cost just as much to refurbish, inspect, test and reuse the SSME's and SRB's as it would have to simply replace them with all-new parts every time (expend them).

During most of the shuttle era, we've tried SSTO and Aero-Space Plane runway-to-orbit-and-back-again type vehicles, all of which have failed miserably and been canceled long before anything actually flew... the cost to develop then were horrendous and the operations costs, if indeed they ever became operational, would have been questionable as to whether they'd ever be profitable, or indeed as cost-saving as projected.

SO what does that leave us?? The only path that been proposed that has never really been tried is the "cheap, SIMPLY launch"... developing a launch system designed not around high performance, cutting edge materials and machinery, not designed for absolute maximum performance, but designed to be as simple and cheap as possible and still deliver a cargo to orbit... IOW, systems like the Sea Dragon (or more realistically it's smaller cousins that have been proposed), Big Dumb Booster, Low Cost Launch Vehicles, and other such proposals. They've been STUDIED, but never really and truly designed and tested... Personally I think this is the way we should go.

Later! OL JR :)
 
I am afraid you may be right..I think we may need another Sputnik moment.
have you had a chance to fly some of your custom builds like the P-61? those builds were really great!

All the war bird builds have successfully and safely flown multiple times except for the P-61 - waiting for the right conditions for the first flight and a Pad Fuehrer blessing. I showed the Pad Fuehrer the plans for the next war bird that makes the P-61 look like a nice sane 3FNC. With all the non standard applications and weird rocket science it might just get me put on the 2013 naughty list.
 
I think the MR 171 is powered by some 1960's quick burn SRB's, using the propellants they were developing for the ABM system. Rumor has it that there is also a nuclear rocket motor included that was also canceled in the 60's - one from that test site you have to get special permission to visit. But nothing beats a MIGHTY D12 and some D11P's to get the fantasy ripping. . . or moving. . . or slowly lifting off the pad.
 
NERVA was the nuclear rocket that was developed and tested back in the late ‘60s early ‘70s and from what I read about it NERVA could have propelled a six manned vehicle to Mars in a matter of weeks keeping the crew under a constant 1/10th G for the duration.

The signing of the “No nukes in space” treaty by President Carter put an end to the NERVA program.

Or maybe NERVA was all hype and no thrust and the treaty was just a good excuse to cancel a program that was going nowhere fast.

Be that as it may; manned missions to Mars and beyond will never be anything but a pipedream until we do develop some propulsion/drive system that can deliver people to these regions in a time span less than months or years.

But this truly begs the question; why bother?

I’m as big a Sci-Fi nerd as the next guy but the problem with science fiction is the writers always assume there is an answer; and reality, unfortunately, might prove otherwise.

As long as we have to “Blast” our payloads into orbit and utilize aero-breaking to recover them; even near Earth space becomes so costly to exploit there isn’t anything to be gained by doing it. I’m all for knowledge and exploration for its own sake but damn!!

Beyond NES we need that constant thrust propulsion system and to the best of my knowledge the ISS hasn’t spent one second experimenting along those lines.
 
With so many NASA programs going nowhere fast at least my fantasy scrap rockets are going somewhere fast, well maybe not fast and I really don't know where they are going, but at least they are going. I just hope the Euros can get the telescope that ate astronomy off the planet by the end of the decade. Until then we can all pee in jars and look at stars. Where has the magic gone?
 
NERVA was the nuclear rocket that was developed and tested back in the late ‘60s early ‘70s and from what I read about it NERVA could have propelled a six manned vehicle to Mars in a matter of weeks keeping the crew under a constant 1/10th G for the duration.

The signing of the “No nukes in space” treaty by President Carter put an end to the NERVA program.

Or maybe NERVA was all hype and no thrust and the treaty was just a good excuse to cancel a program that was going nowhere fast.

Be that as it may; manned missions to Mars and beyond will never be anything but a pipedream until we do develop some propulsion/drive system that can deliver people to these regions in a time span less than months or years.

But this truly begs the question; why bother?

I’m as big a Sci-Fi nerd as the next guy but the problem with science fiction is the writers always assume there is an answer; and reality, unfortunately, might prove otherwise.

As long as we have to “Blast” our payloads into orbit and utilize aero-breaking to recover them; even near Earth space becomes so costly to exploit there isn’t anything to be gained by doing it. I’m all for knowledge and exploration for its own sake but damn!!

Beyond NES we need that constant thrust propulsion system and to the best of my knowledge the ISS hasn’t spent one second experimenting along those lines.

Pretty much spot on, but NERVA was canceled long before Carter... NERVA was test fired several times, and it worked. You're right that it was treaty obligations that torpedoed it, but it wasn't just that... it was going to be expensive to develop, and then the question was "use it for what?" NERVA was originally proposed and work started on it during the late 50's when "all things nuclear" seemed possible and the answer to every big problem. Remember this was at the same time that the gov't was working on using nuclear weapons as a spacecraft propulsion means (Project Orion), so a nuclear reactor using its heat to create hot gas ejected through a nozzle for propulsion seemed absolutely tame by comparison. In priciple it is, but it requires some rather exotic materials and fine engineering to keep the reactor in one piece. NERVA was proposed for everything including second and third stages for Saturn IB's and Saturn V, in-space propulsion, "lunar shuttles", you name it. Obviously by the 1960's, the idea of spewing tons of radioactive exhaust gases into the atmosphere willy-nilly was becoming highly unpopular, and the problems related to it were becoming better and more widely known. The signing of the Limited Test Ban Treaty in 1963 proves this point. By 1966, as NASA was looking forward to a starry future of lunar missions followed by moonbases and Earth orbital space stations, and eventually Mars trips, the government was looking at the budget problems caused by Vietnam and the "Great Society" social programs that LBJ had started... and looking for a downsized space program, not an expanded one. Saturn V production ceased with 15 vehicles produced in the late 60's and was never restarted. Apollo Applications was downscaled from moonbases and a series of large Skylab sized space stations with dozens of crews being launched to them over the course of the program, to a single Saturn V launched dry lab visited by three successive crews flying leftover Saturn IB's and Apollo spacecraft. There was simply no need for NERVA in such a reduced program. NASA went looking for a new mission, and suggested a space shuttle used to build a large space station, and keep it supplied and transport crews, as well as providing satellite launch, repair, and retrieval services for commercial customers, and reusable launch capabilities for the commercial satellite market, DOD, and NASA itself, eliminating the need for expendable rockets, and supposedly saving a ton of money in the process. Of course we now know just how incorrect this was, but that's another issue. At any rate, the Nixon Administration, looking to cut costs, certainly wasn't going to reinstate the cuts that had already been made to NASA by LBJ, like the cancelling of Apollo 20, followed by the cancellation of Apollos 18 and 19, and the downsizing of Apollo Applications. Despite the conclusions of the Townsend Report that called for a more robust space program, Nixon followed the lead of the Congressional budget cutters and approved a space shuttle, but no space station. NASA figured that the station would come later, not imagining that it would be 26 years before the first station components even achieved orbit, and that on a Russian Proton launcher!

When Bush II presented the VSE, NASA soon revived the idea of the nuclear in-space propulsion element. Project Prometheus was going to design and produce a nuclear thermal propulsion engine for use in deep space. It was one of the first things cut by the Constellation Program. Also soon canceled were methane engines for the SPS on the Orion service module (for Mars ISRU produced-propellant), Orion land landings, Orion reusability, the Altair lunar module, and soon the entire joke that the Constellation Program had become.

I think you're right. Unless we have some form of propulsion that can shorten the trip time to Mars, and equally important, make the mission more reusable and less expendable, and lower the huge mass of mostly propellants needed to be delivered into orbit for an all-chemical propelled mission which would take months/years. A nuclear engine would be expensive to develop, like any new rocket engine, but it would solve a lot of problems and open a lot of doors. Nuclear Thermal Propulsion (NTP) like NERVA is the best way forward, and in fact most of the energy produced by a nuclear reaction is thermal energy, so this would be the most efficient type. Nuclear Electric Propulsion (NEP) would have MUCH MUCH less power for a given reactor size due to inefficiencies in transforming thermal energy into electrical energy, and the low thrust capabilities of ion thrusters or Hall Effect thrusters. Electrical power WILL be necessary, for ship operations and for surface ops as well, but it should NOT be used for primary propulsion due to inefficiency. Dual use engine designs exist which can produce all thrust, a combination of thrust and electricity, or all electricity, depending on the needs and phase of flight. NASA's Design Reference Missions (DRM's), which are basically the "outline" that guides all mission planning and stipulates the equipment needed for the mission and how it will be conducted, are all chemically based missions... which require hundreds of tons of IMLEO (Inserted Mass in Low Earth Orbit), meaning at least 6-8 HLV launches PER MISSION. The launch costs alone will run into the BILLIONS... Other methods like Solar Electric Propulsion (SEP), while having the luxury of "free" electricity via sunlight energizing solar panels, really combines the worst of both systems-- it requires MASSIVE solar arrays to generate the necessary electricity for the propulsion system, as well as using electrical thrusters capable of only miniscule thrust levels, which operating continuously for months CAN produce large delta-V's, it also requires large delta-T's... (large amount of time-- essentially it has to "spiral" cargoes out to the moon, over a period of weeks or months... a far cry from the three days of Apollo for the translunar coast... which requires multiple passes through the Van Allen radiation belts, thus making SEP completely unsuitable for manned deep space propulsion originating in LEO.)

Thing is, there's really no alternative to chemical propulsion from Earth's surface to orbit for the foreseeable future. The thing is, there are smart ways to do this and dumb ways. While at first heavy lift rockets that can launch the needed mass of equipment and propellant into orbit for missions in the least number of launches seems attractive, in truth HLV's are going to be ENORMOUSLY expensive to design, manufacture, transport, test, support, and launch. They share little/no common parts with smaller launchers used for commercial satellites and military payloads, so there is little or no cost sharing between programs. In addition, their flight rates will be quite low, meaning that the system never achieves any economies of scale that make the best use of personnel, infrastructure, or manufacturing, and hence remain exceedingly costly. Essentially, this is what "got" Saturn V and IB-- billions of development effort to build a handful of vehicles flown about twice a year (in the case of Saturn V, even less with Saturn IB except for the brief trio of Skylab missions), and no second production run, the vehicles were simply phased out and abandoned as soon as the capability existed to produce them. Shame too, because had the improvements envisioned and developed for a second run of Saturn vehicles been implemented, and a modest but rigorous study and redesign effort been implemented to shave costs and simplify and streamline the Saturn vehicles and their production, we would likely still be flying some evolved Saturn vehicle to this day, much as the Russians are still flying evolved R-7's that first flew in 1957 and evolved Soyuz's that first flew in 1967. Smaller vehicles fly more often, thus achieving higher flight rates and greater economies of scale in production, infrastructure, and use of personnel. Too small and the flight rates get TOO high, however... and more flights does increase the risks, at least statistically, of a malfunction causing a launch failure that would impact the program... but it's arguable if a very-low flightrate HLV that did not keep its support personnel well experienced at preparing and launching multiple vehicles...) The key is finding the balance between flight rates, IMLEO necessary to achieve the missions, and the existing or planned support infrastructure, personnel, and associated costs. At any rate, nuclear propulsion isn't an option in Earth's atmosphere (or apparently out of it either). While Skylon attempts designing an SSTO HTHL vehicle, which NASA has REPEATEDLY tried and failed (the Russians as well with their Spiral program). The odds aren't good... I'll believe it when I see it. SpaceX is planning to try recovery and reuse, which again, NASA and the Russians both have tried with at best limited success (depending on one's metric of success, both efforts could be seen as a complete failure, not having delivered on the promises made for it). The main effort that has been proposed but never implemented is MINIMUM-COST DESIGN... it's been proposed MULTIPLE times but never gone beyond the study phase. Perhaps if the billions wasted on false starts for SSTO super-spaceplanes and such had been spent on minimum cost design, we wouldn't be in this position...

Similarly, "aero-braking" back into Earth's atmosphere is the single least costliest method of returning back into Earth's deep gravity well... retropropulsion into LEO from deep space is THE most expensive way to return to the vacinity of Earth there is... even with a nuclear shuttle propulsion unit to push cargo and crews to the moon or other deep space destinations, returning the entire vehicle to LEO at the end of every mission DOUBLES the propulsion requirements necessary to boost them away from Earth in the first place (ignoring expended cargo/propellants/spacecraft modules left behind not on the return trip). Again, there is a better way... travelling to the Lagrangian points of the Earth/Moon system is the most propulsion efficient way to conduct operations in the deep space of the Earth/Moon system. It's also the best place to depart the Earth for Mars or anywhere else beyond, requiring the least propulsion delta-V. Return to Earth is still fairly energy-intense, but there's nothing wrong with a crew vehicle doing a direct return and entry to Earth's surface as was done in Apollo, or, if LEO IS the ultimate destination for whatever reason, true "aero-braking" (utilizing the atmosphere to bleed off velocity by turning it into frictional heating via repeated shallow dips into the atmosphere, perhaps augmented partially by propulsional retrofire to assist the aerobraking and minimize trips through the Van Allen radiation belts, which are hazardous to man and machine both, using a minimalist crew return vehicle, might be possible.

So, ultimately, if we're going to do ANYTHING in space in an affordable and sustainable manner, we're going to have to embrace more reusability of in-space vehicles, which is probably easier than vehicles having to launch and land on Earth's surface and traverse its atmosphere... We need decent size (not super-duper uber-boosters, nor little launchers that would require dozens of launches per mission) CHEAP launch vehicles sending cargo to LEO, then highly efficient in-space propulsion probably via nuclear EDS stages that can repeatedly make take cargoes to the L2 destination for descent to the lunar surface, or return cargoes back to LEO (it should be equipped with a heat shield and sufficient guidance to allow its return to LEO without having to make a propulsive braking manuever... only using aerobraking to minimize propellant requirements and therefore efficiency). Our Mars vessel needs to have a good balance of reusability of the main modules (propulsion and habitat) and expendability where that is most appropriate (landers, descent stages, ascent stages, etc).

Later! OL JR :)
 
SO what does that leave us?? The only path that been proposed that has never really been tried is the "cheap, SIMPLY launch"... developing a launch system designed not around high performance, cutting edge materials and machinery, not designed for absolute maximum performance, but designed to be as simple and cheap as possible and still deliver a cargo to orbit... IOW, systems like the Sea Dragon (or more realistically it's smaller cousins that have been proposed), Big Dumb Booster, Low Cost Launch Vehicles, and other such proposals. They've been STUDIED, but never really and truly designed and tested... Personally I think this is the way we should go.

Later! OL JR :)

So what you are really saying is I should aspire to building model rockets from scrap and reject parts from trash bins, using Elmer's glue and powered by simple black powder motors that were cool only for a brief time back in the 70's? Dashing my dreams of Rolls Royce aluminum welded fin cans, VMAX propellants, carbon fiber body tubes, metal tipped nose cones, computer design, advanced electronic deployment, tracking and video. Such is counter to the Ego of the true American Rocket Scientist, Agency Administrator, Politician and High Power Certified Rocket Flier. If you can't afford the best then it is better to not fly at all. What then is all that high end education and engineering for? All we can do is just set back, do some more studies and keep paper tiger projects alive to bring in as much funding as possible so we can keep our hard fought for jobs until retirement. I cannot bear to see the poor Liberal Arts major have the last laugh, constantly flying with his cheap, silly LPR black powder motors and thin paper tubes. If it ain't rippin' off the pad on a motor labeled from the last half of the alphabet, it just ain't true rocket science. I want to be cool when talkin' with the fellers so I don't use words like SIMPLE, CHEAP, LOW PERFORMANCE, COMMON MATERIALS, BIG DUMB BOOSTER, and LOW COST. I want to show off to everyone the machine that goes “PING.” I want exotic materials and to be on the cutting edge, that is the NASA way. Any broader view of Rocketry Force is unnatural and will lead to the Dark Side, and that is the FINAL word from Yoda and the Jedi counsel.:)
 
If you can't afford the best then it is better to not fly at all.

Pretty much sums up NASA's attitude... which is why we're in the quandary we are in and have squandered the last 8 years since the retirement of the shuttle was announced and work on the Constellation Project started...

What then is all that high end education and engineering for? All we can do is just set back, do some more studies and keep paper tiger projects alive to bring in as much funding as possible so we can keep our hard fought for jobs until retirement.

Very prescient... pretty much exactly what NASA is content to do... so long as they have some contracts to let to the big aerospace contractors, giving them billions to work on studies and hardware, that will be canceled before it ever flies... Just as NASA did for the entire history of the Shuttle Program...

Later! OL JR :)
 
Aero-breaking might be the cheapest and easiest means to bring stuff back from space but you just know that if we began doing it on a large scale that Al Gore, or one of his ideological descendent, would decry all the heat being pumped into the atmosphere as one more outrageous misuse of Earth’s ecosphere and another source of AGW.

Three things you should never go cheap with; submarines, satellites and sushi.
 
Aero-breaking might be the cheapest and easiest means to bring stuff back from space but you just know that if we began doing it on a large scale that Al Gore, or one of his ideological descendent, would decry all the heat being pumped into the atmosphere as one more outrageous misuse of Earth’s ecosphere and another source of AGW.

Three things you should never go cheap with; submarines, satellites and sushi.

Totally different problem, and totally unrelated. The amount of heat is completely negligible in the grand scheme of things... Earth gets about 7 watts of solar heat on every square meter of surface area facing the sun, all day, every day, and has for billions of years, and will for billions of years more (presumably). Think of how much waste heat is generated via the burning of gasoline every single day... How many million barrels a day of gasoline are burned just in the United States daily?? All of that energy is ultimately turned into waste heat-- over 70% of it is waste heat right out the engine cooling system and tailpipe. Most of the rest is waste heat dumped by the brake rotors being heated when the brakes are applied, and through atmospheric drag on the vehicle itself. Only a small portion of that energy is expended in actually moving the mass of the vehicle and cargo to its desired destination. Then figure in all the waste heat produced by power plants of all types, which can be substantial... how many tons of coal are burned per day?? How many mcf of natural gas burned every day in power production?? How many megawatts of nuclear fission power is produced?? All these produce prodigious amounts of waste heat, and it's all dumped into the environment, either into cooling ponds, cooling water drawn in from rivers or reservoirs and dumped back into them after absorbing the waste heat, and waste heat dumped directly into the atmosphere via cooling towers. Then there's the waste heat generated from the transmission of electricity, which is a pretty decent amount. Ultimately most of the electrical energy that is distributed goes out into the environment as waste heat. It all adds up. Then there's the frictional heat from the several TONS of space dust, micrometeorites, and meteors/meteorites that collide with Earth's atmosphere every single day, decelerating via aerobraking (not aero BREAKING) which usually generates sufficient energy to vaporize most of them! So the energy dissipation into Earth's atmosphere is quickly radiated out into space. It's a TOTAL non-issue.

Now, I was reading an analysis of the growth in power use rates worldwide, and projections of where this would go if these rates remained constant, over thousands of years... Eventually there would be SO MUCH waste heat from the energy generation and use that it would be sufficient to liquify the surface of the planet-- but it would take THOUSANDS to MILLIONS of years of steady, unbroken energy use rates to get the waste heat levels that high. Then there's the tiny issue of how do you generate that much power, and for what, if you've liquified the surface of the planet?? Clearly it's a non-issue.

Just sayin'... Later! OL JR :)
 
And you think your logic and scientific facts will dissuade the acolytes of AGW?
 
And you think your logic and scientific facts will dissuade the acolytes of AGW?

No, of course not... I don't even care to talk about AGW... it's totally beside the point, the topic of discussion, that being the heat load dissipated into the atmosphere by aerobraking of spacecraft.

Later! OL JR :)
 
First, awesome job and great looking rocket.

This reminds me of HBO's miniseries From the Earth to the Moon. In the first episode a few unnamed NASA officials are trying to figure out how to get a man to the moon quickly and they propose to just send him there and continue to send supplies until they can figure out a way to get him back safely. I'm not knocking your design, but it seems that this would fit those parameters nicely. There is nothing wrong with a sleek little capsule on a huge rocket.
Very cool! This concept of a single astronaut was also the plot of a novel called "The Pilgrim Project", which was ultimately turned into Robert Altman's Countdown.
 
The MR 171 flew again yesterday on 2 D11-Ps and an E9-4. Perfect flight and recovered with no damage at all. The capsule section came down perfect on the "Pretty in Pink" nylon parachute Stardust lent me to impress the on looking ladies. As the D-11s burned out the big MR 171 shifted gears down as the E9 burned on but kept heading up.
 
Here's some pics I came across of the NAVAHO booster rockets strapped onto "something" to make a "HLV" ala about 1958... guess this might pass muster for "beatin' dem Russkies"... LOL:)
19571127 PM1140 Jupiter_Navaho booster (2).jpgLV concept unknown (2).jpg
Later! OL JR :)
 
Flew the MR171 at NSL Monday morning. After a hard weekend of flying a CRASH member posted this on the club forum...Thanks!


We all know Dave had some hard landings this weekend and feel his pain. He took it in stride and was pleased with the over all flight performance of his warplanes from a bye gone era. Cudos to you Dave for stepping out of the mold. I wanted to share Dave did have a very interesting landing the last morning regarding his MR171 Capsule. As if Mother Earth reached up and cradled the recovery, saying, “you experienced some hard landings, let me cushion this one..”

MR171 landing.jpg

No damage to delicate escape tower landing perfectly in the dead bush.
 
Love it !

That is a nice "grab" by the bush !

I also loved those launch pics ,as this is the first time I saw them.And as i mentioned early after you posted ,a beautiful build !

But....I think I may have something that will get the lads to planet Mars :wink: I will reveal more info and pics very soon.


Yessir Mr.Daddy ,we seem to think alike :cheers:

Cheers


Paul T

View attachment 131073

No damage to delicate escape tower landing perfectly in the dead bush.[/QUOTE]
 
Love it !

That is a nice "grab" by the bush !

I also loved those launch pics ,as this is the first time I saw them.And as i mentioned early after you posted ,a beautiful build !

But....I think I may have something that will get the lads to planet Mars :wink: I will reveal more info and pics very soon.


Yessir Mr.Daddy ,we seem to think alike :cheers:

Cheers


Paul T

View attachment 131073

No damage to delicate escape tower landing perfectly in the dead bush.
[/QUOTE]

Can't wait!
 
How come you always have a scowl on your face?
You come across as such a jovial fellow.
:confused2:

I usually smile for the posed shots - they must be catching my unphotogenic side with the unposed shots. Or maybe my shoes are too tight, or my head is not screwed on right. No, it is none of this all, it is just that my motors are two sizes too small:sad:
 
Well it finally happened. I think this was the sixth time the MR171 has flown and for the first time all three motors did not light. Just the center E9-4 and one side D11P. She went up slow and arced over and I readied myself for the crash, but then then outboard D burned out and the remaining thrust from the mighty E9 twisted and straightened her out enough to go up a bit further. As she went over the ejection charge went off and all was fine. No damage. The igniter did burn in the third motor and left residue in the nozzle but was just short of igniting the BP. So it will fly if one outboard doesn't lite. I would like to say avoiding the crash was do to good rocket science, plenty of prebuild computer simulation and flight testing under controlled conditions, but it really was just the invisible hand of a rocket god that saved the day.
 
That is a thing of beauty !!

Great launch picture of a great looking rocket !


Paul T
 
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