Attempting to Fulfill the Plan MNKh Edition

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On costs you're quoting for the RLA I'm not sure what millions of rouble would translate to in modern money.

In OTL's 1974, the rouble in January of that year was worth 1/3rd of a USD when buying Swedish goods and services. I had thought that the Soviet Union kept the value of the rouble above the USD for bragging rights and assumed that would be the same in TTL as well, so my estimate of "a couple million roubles" for a RLA first stage was off.

If the Americans were manufacturing the RLA cores, I would expect their price to be in the ballpark of what they could make Saturn 1B stages for. The Bellcomm memorandum "Near Term Intermediate Vehicle: Low Cost SIVB Stages" from March 18, 1969 puts the price on the S-1B stage as 3.71-4.33 million 1969 USD depending on number ordered. In 2024 dollars that would be 31.8-37.11 million USD. Note that the first stage was the cheapest part of the rocket (as is usual for rockets) and the total cost of a Saturn IB was given as 15.88-18 million 1969USD, which would be 136.1-154.27 million 2024USD. Comparing that to the Falcon 9, which has a similar payload, in 2018 NASA was paying 140 million 2018USD (175.37 2024USD) and in 2022 the list price of getting a Falcon 9 (which is never what SpaceX actually charges, but list prices never include all the custom work that needs to be done adapting a rocket to a specific payload so they are quite normal in this respect) was 97 million 2022USD (104.25 million 2024USD).

Note that all of these numbers come with a host of caveats and disclaimers - for example, the Bellcomm numbers are assuming production lots of 30 vehicles at 6/year or 95 vehicles at 15/year. The actual Saturn IB had 14 examples made, total, meaning its actual cost was higher than the theoretical costs that could be achieved with the longer production runs that Bellcomm was assuming. Also, I calculated the 2024 prices using general inflation statistics, these are an average of the inflation and deflation across a basket of products weighted by importance. Since most people do not buy things like rockets or other high end aerospace products often, aerospace sector price inflation has a low weight when calculating national inflation numbers. Finally, rocket prices are never apples to apples. As I hinted above, launch providers often list misleading prices. For example, when the USAF was trying to drive NASA out of the launch business, they would routinely report misleading prices for their launch vehicles, and today SpaceX has for years made misleading claims about the prices of the Falcon 9.

These aren't lies as such, but rather, reflections that the cost of a piece of a rocket when it rolls off of an assembly line, and the cost of that same piece of rocket after it has been transported, stored, validated, assembled and rolled out to the launch pad are very different and there is not standard part of a component's life cycle at which to assess its price for comparative terms, and some costs may be charged for at different points of the life-cycle by different companies (for example, because SpaceX does more in-house, the profit for the people who who made the engines comes when a launch is bought from the company, whereas with most rockets, the people who made the engines are usually a sub-contractor whose profit comes when the component is delivered to the company who assembles the rocket).

Now that we have some grounding in rocket costs... I would expect that the cost for us to manufacture RLA first stages is less than what the Americans could make the same stage for, there's two major reasons for this: firstly, we invested heavily early on in the RLA program in making a large factory for RLA production and we are reportedly producing them as fast as we can (we've been told several times that we are making them pretty much flat out) so we have economies of scale that are being fully used and are racking up considerable worker experience in producing these things. Secondly, our wages are lower than American wages, and most of the cost of rockets is labour costs.

I would not be surprised if we were making RLAs for 40-60% of the cost of a Saturn 1B stage.

In any case, I'm dubious flying even a very large supersonic plane once would cost tens of millions a flight, millions I could certainly easily see though maybe even ten million. But that would as such in my opinion be competitive against the likes of the RLA for sure by quite the margin.

10 million USD in 2024 dollars?

Regards,

fasquardon
 
Now that we have some grounding in rocket costs... I would expect that the cost for us to manufacture RLA first stages is less than what the Americans could make the same stage for, there's two major reasons for this: firstly, we invested heavily early on in the RLA program in making a large factory for RLA production and we are reportedly producing them as fast as we can (we've been told several times that we are making them pretty much flat out) so we have economies of scale that are being fully used and are racking up considerable worker experience in producing these things. Secondly, our wages are lower than American wages, and most of the cost of rockets is labour costs.
If I recall correctly the RLA factory had a capacity of about 50 a year. So presumably that's the rate they're being made at then. Hopefully that can be kept up and the factory be made full use of for a good time to come.

Still based on your other figures that should be plenty for some economies of scale and then some then. And I think it would match up with some I know of from SpaceX in the matter as well I guess. Though it is hard to get the real costs for SpaceX, as they're selling in to a relatively noncompetitive market and have a very large rocket development to finance. But it's been suspected the price they pay internally for their Starlink launches is probably under 50 million, possibly a fair bit under even like 30 million. Admittedly Starlink isn't the most challenging launch profile, but they repeat it a lot so they have plenty of experience with that config I guess. Still if those figures are some what accurate it actually some what lines up with your estimated mass production numbers. Which is an interesting perspective on thinking about how SpaceX got the cost of Falcon 9 production so low I guess, a rocket that at current is launching at a rate of over 100 a year.
10 million USD in 2024 dollars?
Yeah, I used current number estimates for everything. Mixing different values would only cause confusion after all.

Still that is just a personal guess by me on the matter. I can't claim it's anything like rigorously researched or based on any solid fact. Just a feeling from general aviation operations. Though just to make sure I now looked up some figures which hopefully are some what current. Still based on those for instance mil jets like the B2 have a cost of around 150k per hour, and the stealth coating on that make it a particularly large maintenance hog. A B-1b as a low supersonic bomber is around 60k I believe for comparison. Or for a very fast plane like the SR-71 about 200k per hour. So even assuming flight hours are far more expensive for this vehicle and you need a fair few hours of flight per launch on it, it's rather hard I think to get all to excessively high costs per launch in my opinion. Well so long as we don't incorporate the potentially quite high R&D costs in to it all, which I think one shouldn't really. As the goal is to get a feeling for the base prices of each solution.

As such, I don't think my guess is actually all that unreasonable. And it would actually probably be able to undercut the RLA first stage cost by a fair bit if one was willing to eat the immense R&D costs for it.

Though well... that even assumes any of the Soviet scientists ever dare propose it though. Maybe they would if we completed the reusable air launcher or maybe they wouldn't.
 
If I recall correctly the RLA factory had a capacity of about 50 a year.

Yow! 50? Even if each RLA-3 counts as 3 units of production capacity I'd imagine we were launching RLAs of some kind around 40 times a year (but probably we are launching those at most once a year, not 4 times a year). And likely at least as many, if not twice as many light rockets launched. That's an impressive amount of stuff going up.

Our economies of scale might be better than I thought then.

Still that is just a personal guess by me on the matter. I can't claim it's anything like rigorously researched or based on any solid fact. Just a feeling from general aviation operations. Though just to make sure I now looked up some figures which hopefully are some what current. Still based on those for instance mil jets like the B2 have a cost of around 150k per hour, and the stealth coating on that make it a particularly large maintenance hog. A B-1b as a low supersonic bomber is around 60k I believe for comparison. Or for a very fast plane like the SR-71 about 200k per hour. So even assuming flight hours are far more expensive for this vehicle and you need a fair few hours of flight per launch on it, it's rather hard I think to get all to excessively high costs per launch in my opinion. Well so long as we don't incorporate the potentially quite high R&D costs in to it all, which I think one shouldn't really. As the goal is to get a feeling for the base prices of each solution.

To what extent do those hourly costs reflect the costs of the aircraft in the hanger? And the cost of take-off and landing? A single launch could involve the aircraft flying for mere minutes, but those minutes would involve both take-off and landing and all the stresses and strains of such, and for much of the time, a carrier aircraft would be sitting in a hanger or be spread out in pieces undergoing maintenance.

Also, IMO launch costs should include defraying the initial R&D cost.

If we develop supersonic giants and use them extensively, that's quite different to developing supersonic giants we rarely use.

Regards,

fasquardon
 
Well so long as we don't incorporate the potentially quite high R&D costs in to it all, which I think one shouldn't really. As the goal is to get a feeling for the base prices of each solution.

I dont see how comparing base price without the R&D cost would be useful to form a judgement.

If we fly 50 flights each year of the new bomber for 30 years and each flight saves 50 mil compared to the RLA, that means that the R&D and start-up may cost 75 billion at most before it is still more expensive despite substantial base cost savings.

Unless you think that the development itself would be a great way to advance our scientific knowledge?
 
To what extent do those hourly costs reflect the costs of the aircraft in the hanger? And the cost of take-off and landing? A single launch could involve the aircraft flying for mere minutes, but those minutes would involve both take-off and landing and all the stresses and strains of such, and for much of the time, a carrier aircraft would be sitting in a hanger or be spread out in pieces undergoing maintenance.
So far I understand hourly rates for flying, I think they indicate how much you have to pay in total, maintenance etc, to get 1 hour effective flight time out of the craft. Thus the cost to keep it flying. So things like storage I think would be included in this. Obviously one could create situations where it doesn't work out, but it's probably fair enough. I kind of figure the metric came in to being, because to an extent aircraft users care more about how much they effectively have to pay for the thing they really want, flying, on the ground does them no good after all.

Also, IMO launch costs should include defraying the initial R&D cost.

If we develop supersonic giants and use them extensively, that's quite different to developing supersonic giants we rarely use.
While there is a truth to this, if one only views it in that form it can give a pretty warped view of how much it actually costs to run the assets one has once they've already been developed. So I tend to personally like to keep it some what separate, a figure to take in separately from the running cost, thought of course one certainly shouldn't forget R&D, you did pay it after all.

Though considering we're managing to launch so many RLA, fair chance you could keep a few of them running at a reasonable rate though. Especially as you might be able to pick up some of the light launches as well because your first stage was effectively on the cheaper side. It's a bit of a so-so question on if its worth the economics I guess. Though now that I think about it, it certainly would give the Soviets more options on launch inclinations. So that's a small side benefit for what ever that is worth.

On a side note, now that I'm thinking about it... I guess if a supersonic aircraft of that scale existed, the military would probably occasionally want to lend them to test their various new aircraft and missile prototypes. Getting some real world flight data at relevant operational speeds tends to be pretty valuable to them. It's not a good enough reason to develop them of course, else the USA would have long done so, but I guess it's something that would give them some more use.
Unless you think that the development itself would be a great way to advance our scientific knowledge?
I actually do think just being able to move the bar on ones scientific and technical capabilities has some value in and of itself, yeah. It tends to change what kind of projects get proposed and done, because it becomes a well understood field then where the fores and against and actual costs are now known.

Though another reason to keep things some what separate at times is because at times when you say for instance halve the costs of things an unknown larger amount of it could be used. This is something we saw in modern launch costs as well, the launch costs passed a certain threshold and apparently this made certain types of mega constellations viable. So I can be useful to get a sense of how low the launch costs could actually be pushed and if that might help start an expansion of launches.

It's things like that which make me want to keep R&D as a separate item, so I can see what the actual capability and cost could be once one actually has the item.



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Still regardless of that, I think this discussion has been pretty fruitful. It gave me some extra perspectives on how to think about the Reusable Launcher project. And I now think it is probably actually a good choice to take. I can think of a few reasons why.

- One it keeps the designers busy and in practise with a new project now that the RLA upgrade has completed.
- It gives a signal to the designers we are interested in reusable proposals
- A very large subsonic cargo plane will always have its uses. Certainly the Antonov-225 always could find continued work moving around overly large/cumbersome or overly heavy objects by air. So the air frame will continue to get used till its End Of Life, helping defray it's design costs some what and giving a some what useful asset even if it is no longer used in launches.
- I believe the original project intended to design a staged combustion hydrogen second stage. This is a useful improvement in our hydrogen engine technology and could probably be put to use as is or in a redesign for the RLA interplanetary stage in a future upgrade.
- If the project works we can get rid of a small launcher that runs on rather toxic fuels. While its real world hazard level is some what relative, it's still a bit annoying and could occasionally cause some extra problems. So it would probably be better to phase it out in time.
- If the project works very well, we'll get a new small launcher that runs cheaper then our current small launcher.
- Being plane launched it could access more orbital inclinations easily then our current main launch site allows.
- The project is on the cheaper side to fund
- Having the worlds largest aircraft has some minor prestige attached to it, so the politicians could see it some what positively as something to occasionally brag about


Over all as such one way or the other the project will probably benefit us, even if it under performs it will probably still be an ok enough outcome for our future goals in space.
 
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Or we could just use an RLA which costs no additional R&D funding and has massive pre-existing stocks of physical and human capital tuned to it already. Gotta find something to keep the Stalingrad factory in business long term, Intercosmos helps but eventually the Germans/Indians/Chinese are going to run out of cheap and easy satellite business too. Spending 4 RLA cores every time we need to rebuild and recrew a station - remember our station program throws away the entire station and launches a new one every 3 months for each new crew - is likely still cheaper than developing MKAS even if MKAS works which again I doubt it actually would.
 
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Found a real Soviet project similar to DynaSoar

View: https://youtu.be/Cz8CB2G4atQ?si=FHk4tvW5REmaj151

The LKS (Russian: Лёгкий Космический Самолёт, "Light Cosmos Plane") was a Soviet Union spaceplane project led by Vladimir Chelomey in response to the United States Space Shuttle. The LKS was smaller and cheaper than its American counterpart, but was ultimately discarded in favor of the larger Buran. Claiming that the Buran project was too big, heavy, and expensive for Russia to complete, Chelomey designed the LKS in 1979. He ordered the construction of a full-scale mock-up, as a way to further stimulate interest. The project was never fully sanctioned however, and in 1982, Chelomey was officially ordered by the Soviet government to stop any further development. In March 1983, Chelomey made yet another attempt to obtain permission to build the LKS to repel US Intercontinental ballistic missiles. This too proved futile. In 1991 the mock-up was destroyed, possibly by sabotage.

Mission Steps

  • Start
    • 1. Launch by a Proton rocket (T = 00:00)
    • 2. First Stage Separation (T = 02:06)
    • 3. Second Stage Separation (T = 05:34)
    • 4. Third Stage Separation (T = 09:49)
    • 5. LKS OMS Ignition (T = 10:00)
    • 6. LKS in LEO (T = 13:20)
  • Orbit
    • 1. LKS gain the correct asset for burn
    • 2. LKS OMS ignition & de-orbit burn
    • 3. Braking maneuverings
    • 4. LKS re-entry into atmosphere
  • Landing
    • 1. LKS is back into the atmosphere
    • 2. Braking maneuvering
    • 3. LKS gain the landing alley
    • 4. LKS assume a steep descent angle
    • 5. LKS turns to Baikonur Cosmodrome runaway
    • 6. LKS lands and open the brake chute
 
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Our current light launcher is still pretty new, a new light launcher strikes me as chasing efficiency for the sake of chasing it since if we want technological advancements we have pretty much every other project available to push our boundaries. Maybe when we're well into the 80s we can upgrade the light rocket but for now I just don't really see the point
 
Especially since the PKA doesn't work either. Due to a very weird combination of rolls the PKA ended up being our only spaceflight vehicle for a few years during the early crewed program because the RLA + capsule wasn't ready yet, but without that very weird streak of luck getting it into the history books it would be widely considered a failure I think. When we actually did fly it for a few years on account of having nothing else, we discovered that it was effectively a single use craft after the damage associated with reentry and landing.

So not only would a revived MKAS program have to get over the hurdle of the carrier aircraft that killed it last time, as well as the big weird hydrogen launcher stage which would have probably killed it if the aircraft didn't, but even the PKA orbiter isn't actually reusable so it would need to design a new orbiter as well. Too many potential points for the program to fail when it couldn't even clear the first checkpoint last time we tried, if we can't use the PKA and we can't use a giant pre-existing cargo plane then we're just developing a worse spacecraft from scratch to maybe theoretically be a little cheaper than the tested and reliable RLA if you ignore R&D costs and assume it flies for decades if it all works perfectly. And if anything doesn't work perfectly we just wasted all the money for however long the program ran before getting canceled again.
 
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A station powered by a reactor capable of generating up to 100kW can undertake scientific experiments previously unheard of for solar-powered systems.
What kind of experiments require that much power?
The ISS solar arrays can produce at peak 240kW
Can we have ion engine for station keeping?
How do we deal with shielding?

Here's a 1974 Soviet proposal for a space station with nuclear power:

MKBS

MKBS
falsesteps.wordpress.com

MKBS: Mir’s Giant Ancestor

What it was: A large nuclear-powered space station, in the 220-250 tonne range, that would be the main part of a “cloud station”—a set of orbital installations that would define the USSR’s presence…

The MKBS consisted of two large core modules of 80 and 88 metric tons each, launched by the N1. These were powered by a 200 kW nuclear power plant derived from OKB-1's work on nuclear electric propulsion. Solar arrays totaling 140 square meters of area provided 14 kW of backup power. Two Proton-launched modules were connected to large arms which spun to provide artificial gravity for crew conditioning and experiments. Additional Soyuz and TKS-derived modules could be attached and detached to conduct special studies. Total mass of the station was to be up to 250 metric tons, with a basic core diameter of 6 m and a length of 100 m. The operational MKBS would be placed in a sun synchronous orbit of 400 to 450 km altitude at an inclination of 97.5 degrees. A basic crew of six, with a maximum of ten, would inhabit the station throughout its ten year life. Crews would serve two to three month tours, with overlapping crew member replacements four times a year. The station was to be equipped with a total of eight motor clusters consisting of orbital correction motors of 300 to 1,000 kgf, coarse orientation motors of 10 to 40 kgf, and ion engines for fine orientation and orbital altitude maintenance with a thrust of 100 to 300 grams.

The primary overall requirement was to define a MOK system which could perform a broad range of tasks while minimizing expenditures in the creation of the system and its subsequent use. These requirements were met by the following technical decisions:



  • It was desirable to minimize the quantity, cost, and crew size of orbital spacecraft while not making any single spacecraft too complex. This was solved by always considering that a particular part of a task might better be accomplished by another spacecraft, rather than having a single spacecraft accomplish everything.

  • Communications and earth surveillance requirements of the base MOK would best be met by a sun-synchronous orbit of 97.5 degrees inclination

  • The active life of the MOK would be for 7 to 10 years utilizing continual replenishment of the spacecraft and in-flight repairs

  • Consumption of fuel in moving from earth to orbit and from orbit to orbit would be reduced by having fuel dumps in a supporting orbit and using ion engines for spacecraft orientation

  • Landing capsules would at first be used for imagery recovery, but digital downlink would be developed quickly to eliminate this consumable item

  • A special modification of the existing Soyuz 7K with manipulators would be used for inter-orbital ferry and regular repair service of autonomous spacecraft while being based at the MKBS

  • The development cost would be minimized by use of existing or in-development systems:
    • Soyuz 7K-T spacecraft and Soyuz launch vehicle as the basic transport craft

    • Development of unpiloted modifications of Soyuz for use as MKBS visiting modules

    • Development of the basic modules from the existing Salyut space station 17K, launched by the Proton booster

    • Use of the N1 for launch of the MKBS core spacecraft

    • Use of the N1 with the Block Sr upper stage for delivery of special modules to geostationary orbit

    • Maximum use of existing and in-development facilities for support of MOK, such as launch complexes, command and control centers, etc.

    • Reduction of the cost of transportation to and within the system, by putting all future satellites as much as possible in the same orbital plane of 97.5 degrees, and by development of new economical reusable transport systems
It was planned that ultimately the MOK would be supported by a reusable launch vehicle, which was to be a modification of the N1 Block A. This would use a combination of air-breathing LACE (Liquid Air Cycle Engines) booster engines and liquid hydrogen/oxygen propellants sustainer engines on the core.
The development of the MOK would been undertaken in two phases: An experimental phase (near earth orbit around 51.5 degrees) and an operational phase (sun-synchronous orbit of 97.5 degrees). In May 1974 the N1 was cancelled, and with it, the MOK.

Technical development of the MOK was the first large-scale space technology study which used combined , earth resources studies, economic analysis to determine the best engineering solutions. Various technical results obtained in the process of this work were used for a long time after. In particular the development of the Progress replenishment spacecraft, Soyuz space station ferries, and special-purpose modules of the Mir spacecraft could be traced directly to the concepts and designs for the MOK. Leading participants in the project were I N Sadovskiy, V V Simakin, B E Chertok, V S Ovchinnikov,, M V Melnikov, A P Abramov, V D Vachnadze, V K Bezverbiy, A A Ryzhanov, I E Yurasov, V Z Ilin, G A Dolgopolov, N P Bersenev, K B Ivanov, V C Anfyrev, B G Sypryn , V P Zaitsev, E A Shtarkov, I V Gordeev, B V Korolev, V G Osipov, V N Lakeyev, V P Byrdakov, A A Kochkin.

It was interesting to note that American propulsion engineer Peter James described the MOK in considerable and accurate detail in his 1974 book Soviet Conquest from Space. The book was dismissed by many authorities because the systems described in it never appeared. Only in the last two years has it become apparent that the system described to Mr James was in development, but was cancelled at just about the same time his book appeared.

Also, which path are we aiming at? LEO space station, Lunar Surface/orbit base, or Mars?
 
than we're just developing a worse spacecraft from scratch to maybe theoretically be a little cheaper than the tested and reliable RLA
It's not an RLA competitor, it doesn't have the throw weight for that. It's the small launcher competitor and it says that as well in the brief for it. And the small launcher runs on very toxic fuels and while admittedly this usually doesn't matter to much, I can't say that fills me with enthusiasm either. It's just kind of a fuel tech branch that I kind of want to die, especially as performance wise the fuel doesn't even give any kind of advantage beyond that you could have a rocket fueled up with it for a long time... which you don't care about in commercial space flight. Also the brief for this particular iteration says nothing about a reusable second stage like the PKA, it seems to just be a plane dropped hydrogen rocket stage. So the only real major challenge here is getting liquid hydrogen to keep long enough till it launches, I guess if one let some of it boil off this might be possible.

'[]Reusable Launchers: The initial MKAS program following the PKA was dismissed by Glushko as an impossible engineering nightmare but it can still be resumed for the sake of providing a lighter launch vehicle. Using long-burning hydrogen engines along with a reusable launcher attached to a drop tank will improve launch capacity and especially if paired with a carrier aircraft reduce costs. The technologies for the project itself are available today with the only issue being the degree of complicated engineering work. It is believed to be possible that some form of the MKAS concept could be launched in the decade allowing space to be opened to low-cost space launch. (-10 RpY Expected)'

As one can see the expected cost is also actually rather modest, possibly because the actual goals aren't actually that huge. And since the projects original run we've already developed hydrogen engine and fuel tanks, so we'd just be iterating on those. The carrier plane may or may not exist already as well, we never did find out if the military maybe completed a prototype large plane in the end after all. But even if it didn't, making one or two An-225 or somewhat large planes would be well with in current aerospace ability, and while not cheap, it shouldn't be all to excessively expensive either I'd think for just a pair as it's basically thus the same as making a prototype plane rather then something intended to built in numbers.


Of course their estimates could be wrong of course, I'll grant you that it could also not work out as well as hoped. But the brief talks about it as if a large part of the problem is already just a derivative of existing technologies, so it shouldn't be some kind of wild guess either.

Our current light launcher is still pretty new, a new light launcher strikes me as chasing efficiency for the sake of chasing it since if we want technological advancements we have pretty much every other project available to push our boundaries. Maybe when we're well into the 80s we can upgrade the light rocket but for now I just don't really see the point
Sure, but I just don't like out small launcher in the end due to its toxic fuel. Though another way of looking at this is that in the rocket business, like in any other field, if you just rest on your laurels and do nothing... well you're certainly not going to be advancing. And iterating on relatively small budgets and seeing what comes out of it isn't the worst thing ever to do. That iteration matters can also be seen in the current rocket business, where the commercial companies if they have the money for it tend to be looking at the next system they can develop, or the next improvement they can make to their rockets. In that sense now that the RLA upgrade is done, we're currently doing nothing.
 
Speaking of the space station... What if we try to build one of those modules to create artificial gravity using centrifugal forces to increase the health of the crew?

Yeah it's a bit of a waste of money and a stupid idea considering that space stations specifically exist to study the properties of weightlessness. But I think the cosmonauts would love the opportunity to feel the weight again, it would really improve their quality of life. At least a habitation module?



Plus it looks epic and will make Americans envious.
 
How is it a 'resuable' launcher if there's no orbiter to re-use? It's pretty explicitly reviving the MKAS program, I expect it to look like our previous MKAS program. Doing the project that says it will revive MKAS and expecting it to do something that isn't MKAS (like a rocket-launched PKA or an airplane-launched disposable rocket) seems even less realistic than expecting it to be MKAS but it works this time.
 
How is it a 'resuable' launcher if there's no orbiter to re-use? It's pretty explicitly reviving the MKAS program, I expect it to look like our previous MKAS program. Doing the project that says it will revive MKAS and expecting it to do something that isn't MKAS (like a rocket-launched PKA or an airplane-launched disposable rocket) seems even less realistic than expecting it to be MKAS but it works this time.
I presume that is based on this original brief of it.

'The PKA program as a rocket-launched space plane has gone fairly well, with only a few issues occurring in its further development. The five-and-a-half-ton unit is expected to have a small propulsive stage for manual de-orbit capability while carrying up a single pilot to orbit. Several ambitious technicians have, however taken the funding and pushed towards a heavy air-launched concept closer to that of the original space plane program, just one that is orbital capable with a dropable propellant tank. To maintain the 1.5-stage theoretical capability of the vehicle, the expander cycle hydrolox engine has been selected, with the expendable tank expected to contain almost all of the fuel of the orbiter. The almost twenty-ton empty vehicle is expected to have two crew and a payload capability to orbit of almost five tons, in theory. The airforce has also started to contribute, with approval granted for Antonov to design a new super-heavy transport plane for both armored transport and for the orbital program.'

Which I guess is a fair enough criticism on it then. It was awhile since I'd properly read up on the entire thing and I guess I'd forgotten an important detail on it.

Well fair enough, I guess that does make it a lot less interesting then just an air launched system. I guess it's the curse with a fair few of these designs, the designers immediately want to aim for to much, rather then getting there step by step.
 
So far I understand hourly rates for flying, I think they indicate how much you have to pay in total, maintenance etc, to get 1 hour effective flight time out of the craft. Thus the cost to keep it flying. So things like storage I think would be included in this. Obviously one could create situations where it doesn't work out, but it's probably fair enough. I kind of figure the metric came in to being, because to an extent aircraft users care more about how much they effectively have to pay for the thing they really want, flying, on the ground does them no good after all.

Hm, OK.

That said, a supersonic carrier aircraft would be doing such a different mission, that even comparing it to the SR-71 doesn't work IMO.

And even if it cost the equivalent of 10 million USD per flight hour, if it is only flying for 10 minutes per launch, that's still 1.66 million USD per launch, which could be quite competitive.

Anyway, this kind of project is probably not going to come up until the 90s.

While there is a truth to this, if one only views it in that form it can give a pretty warped view of how much it actually costs to run the assets one has once they've already been developed. So I tend to personally like to keep it some what separate, a figure to take in separately from the running cost, thought of course one certainly shouldn't forget R&D, you did pay it after all.

Well, it is true that sometimes things have broad applications that you can't really think of all the ways it could be used, like pretty much all blue-sky research.

I don't think giant supersonic aircraft have such broad applications though.

- If the project works we can get rid of a small launcher that runs on rather toxic fuels. While its real world hazard level is some what relative, it's still a bit annoying and could occasionally cause some extra problems. So it would probably be better to phase it out in time.

You know, I had missed that this was aiming to replace the small launcher. That actually makes me alot more interested in this project. Not because I think it will replace the small launcher completely - the small launcher program is using recycled ICBMs and spare ICBM production, which I expect will mean it sees some sort of use into the 21st Century as at some point (which may already have happened) the missiles will start to be retired and hundreds, if not thousands of reconditioned missiles will then be available for launch use.

And burning their toxic propellants while launching things is actually one of the more environmentally friendly ways to dispose of them all.

But such a small launcher sounds much less ambitious (and thus has less technical risk), while still involving interesting work that will push forward our capabilities.

And I am in agreement with your other points.

And the small launcher runs on very toxic fuels and while admittedly this usually doesn't matter to much, I can't say that fills me with enthusiasm either. It's just kind of a fuel tech branch that I kind of want to die, especially as performance wise the fuel doesn't even give any kind of advantage beyond that you could have a rocket fueled up with it for a long time...

Hypergolics have advantages in terms of reliability (so launches are easier and require less checks before count-down starts) and density, so for a given amount of propellant you need less mass wasted on tanks and your turbopumps can be less powerful. (Indeed, hypergolics can be made without turbopumps at all and still be OK.) They are good for achieving high thrust too.

They have their place.

Gotta find something to keep the Stalingrad factory in business long term, Intercosmos helps but eventually the Germans/Indians/Chinese are going to run out of cheap and easy satellite business too.

Considering that our electronics are in broad terms competitive with the Americans and we may actually be ahead in terms of vacuum adapted electronics with all of our probe programs, our satellites are probably have fairly long service lives.

Which means that if we are running the Stalingrad factory flat out now, demand is only going to rise as our allies programs grow and as we give our manned program more than mere crumbs.

even if MKAS works which again I doubt it actually would.

I don't see any reason why it wouldn't. The thing is realistically scaled. Indeed, I'd missed that this project was specifically aiming to replace the small launchers, which I believe are lofting payloads of 1 tonne and under to LEO. That means the proposal is probably more like the Northrop Grumman Pegasus than it is the MAKS or LKS. We should be able to use modified airliners or military transports for this program.

In any case, even if the design does end up as large as the OTL MAKS proposal, the issue is not whether it will work, but whether other things are more useful investments.

So not only would a revived MKAS program have to get over the hurdle of the carrier aircraft that killed it last time

Critically, the current proposal is open to the idea of launching the new vehicle on top of a normal rocket.

If the proposal was only to try for aircraft launch, I would be against it. But since they're open to better ideas, it is fine.

If they roll well on the plane design, that's OK, if they don't get lucky and instead go for a more conventional LKS-type approach, that's fine too.

Though another way of looking at this is that in the rocket business, like in any other field, if you just rest on your laurels and do nothing... well you're certainly not going to be advancing. And iterating on relatively small budgets and seeing what comes out of it isn't the worst thing ever to do. That iteration matters can also be seen in the current rocket business, where the commercial companies if they have the money for it tend to be looking at the next system they can develop, or the next improvement they can make to their rockets. In that sense now that the RLA upgrade is done, we're currently doing nothing.

This is absolutely spot on.

IMO we need to do the bulk launch program, the hydrogen launcher program, or the re-useable launcher program purely so the engineers who designed the RLA can teach their younger colleagues how to build rockets before they retire. Skills survive best in living people. No amount of documentation can ever be as good as working with someone who knows what they are doing on a real project.

At this point, now we are less funding constrained, there are arguments for all three options here. But picking the fourth option of "none of the above" is in my view, a waste of valuable experience.

This discussion has made me more interested in the re-useable launcher project, so I lean towards that being the best bang for buck.

But the other two options have their arguments as well.

I admit I am probably least interested in the all LH2/LOX rocket, just because that is such an American idea... (Though the Soviets did have some quite interesting ideas for all LH2/LOX rockets in OTL like the Deuteron proposal.)

Maybe when we're well into the 80s we can upgrade the light rocket but for now I just don't really see the point

I would note that from the sound of it, the re-useable program is aiming for having something that would fly in the 80s. See:

"It is believed to be possible that some form of the MKAS concept could be launched in the decade allowing space to be opened to low-cost space launch."

Also, which path are we aiming at? LEO space station, Lunar Surface/orbit base, or Mars?

IMO the political need for a space station means that is the immediate priority. We are also in desperate need of bringing our manned program up to scratch after the neglect post Lunar program abandonment. Intercosmos will include plenty of unmanned satellites, but the real propaganda value is men and women from across the CMEA working together to advance the human conquest of space. And we need good hardware to impress our allies.

I do want to do things like a series of short-duration (no more than 3 month) Lunar bases and a Mars sample return, but I don't think those are priorities as yet, they're just long term aspirations that I keep in mind when I look at the ideas our designers try to get us to fund.

Yeah it's a bit of a waste of money and a stupid idea considering that space stations specifically exist to study the properties of weightlessness. But I think the cosmonauts would love the opportunity to feel the weight again, it would really improve their quality of life. At least a habitation module?

A rotating station would let us study the impact of long term exposure to things like Lunar gravity and Martian gravity. And biological, chemical and industrial processes in the different conditions.

Would be extremely valuable, particularly since evacuating someone from a station in LEO is way easier than getting someone back from Mars.

Regards,

fasquardon
 
This space debate is going over my head now... still, cool to see everyone's arguments! Whatever way we go, we'll do great things in space I'm sure.

EDIT: Also in terms of a small launch reusable system, we literally completed a small launcher program two years ago. We really don't need another one right now.
Good point, thanks for reminding us. Would

Some raw economic data i gleamed from the thread, it covers the eight and ninth five year plans with Turns 75-79 being plan VIII and 81-85 being plan IX
Oooh yeah I love data, thanks for this compilation. Man, it's shocking to learn that the GreatGork bankruptcy wiped out 13 percent of the USSR's GNP. Surprised the impact we saw on the price indicators was not larger from that! Outright cost us a whole plan of economic growth, that stings!
Labor data is interesting. Percentage wise the USSR is gradually catching up with global labor costs, though that slowed this automation-focused plan. Meanwhile CMEA labor prices fluctuate but mostly remain a similar percentage of the Soviet ones, especially General labor.
 
That said, a supersonic carrier aircraft would be doing such a different mission, that even comparing it to the SR-71 doesn't work IMO.
Well for obvious reasons we don't really have an exact comparison, so I just tried to find a few different planes that might cover some aspects of it at least. If you'd ask me what the real cost would be, well probably higher then the SR-71, yeah. There would be the slight mitigating factor the SR-71 is also 60s tech, and presumably a next gen more mature supersonic aircraft design would be at least a little more efficient then it. But it's a pretty big plane, though things like the B-2 and B-1 show that size is perhaps less impactful then speed... So it's conceivable that you could have such a plane fly for half a million an hour in modern money I guess? Though that's obviously a really rough guess.

Well anyway, the supersonic first stage was just me trying to note that if need be we could develop reusability over an alternate path, that if the developers for some reason didn't throw up propulsive landing as an option there was still another war. Though air breathing engines do have some possible benefits if one can get over their high R&D costs I guess.


But we'll see what the designers bring up I guess. We can only work with what is ultimately given after all.



PS, you might be right that we should just give the designers a chance to do something like the bulk launcher option. It would at least let them think outside the standard box for once and they might even just think up some variants of current rockets one wouldn't as easily get otherwise.
 
A bit of change of pace from the discordbureu
This talk of formats reminds me of how rectangular "sound postcards" made out of cardboard were a huge way of listening to music in 1960s and 1970s Poland
Not to mention the Soviet Union having a black market for vinyl recording made out of discarded x-ray scans
Brought to you by @TaxHarbinger
OTL 60s-70s Soviet music industry before rapidly changing to the new cassette tape format in the late 70s

View: https://youtu.be/shisgymvKZ8?si=eW14_0ccujiZhVkU

Are you guys ready for the Format Wars?
 
On the topic of power:
Anyways, 1 units is 38 Megawatts, so 320 GWe is cumulative 8421 units of power. to meet the USSR's OTL capacity. Well, we'll definitely have that breached by TTL 1990, though not sure by how much. Power numbers are fuzzy before 1955.
Y.N. Rudenko, 1991, claims in a soviet publication you can read above that their power grid reached 329gwe capacity in 1990 - I can tell by context that's total capacity, not considering CF, because the previous page states a total production of 1,728twh in that year, compared to the 2,882twh you'd produce running a 329gwe grid for a full year at a CF of 100%. So in other words, their overall CF as claimed in this internal publication was 61.7%.
I did my tally and I'm going to do an omake-worthy writeup Soon^TM, but my preliminary results were awesome enough I had to double check: We installed 1562 power units in the 7th plan, 1620 in the 8th plan, and with this turn a mind-boggling 3625 in the 9th. More power installed in the last 5 years than the preceding twelve. 6804 total. That total over three plans converts to 2268 Terawatthours/year. And that is not including the hydropower that gets directly funneled into metallurgy without seeing the grid, and not including power installed post-war under Malenkov. So unless someone's doing math wrong, we have already solidly exceeded the USSR's 1990 power generation capacity, and next plan will exceed their theoretical 100% CF capacity. Wow.

Sadly 46.5% of that power comes from burning coal, such is the power of the supercritical steam cycle, and 85.3% of it is coal and gas combined. And we're only going to build more. Global warming is going to hit early in TTL.

I wonder how many autodice of gas power we'll be able to build in the 10th plan. This turn and the last we put 3 dice on manual builds along with the two autodice we've effectively invested 5 dice a turn on gas two turns in a row. We'll need it with the coal running out.

Also @Blackstar during my tallies, this turn says we have +671 power from plan programs, but adding up all the Plan Effects comes out to 691. I've used the latter number for this calc.
 
Incidentally, at an 85% CF, 12 VVER-1000s per year should amount to ~89.35twh per year, so if we go max nuclear this coming plan we should be able to install 446.75twh/yr of nuclear power. Assuming our total added electrical generation over the course of the plan is 800twh, we'd be rocketing up to nearly 15% nuclear power in just five years.
 
Just a question, but with us going max on nuclear power, would this affect too much the Oil price ?

Because then we would have a growing reserve, unless we go crazy on developing even more the petrochemical industries to support that unused production for it to not be just being wasted there, did we already decided to build pipelines to the CNE countries for us to supply their energy needs ?

For me i'm already seeing us going more and more on the nuclear power, and well we still have massive reserves of oil and gas just waiting there so idk if this is a problem or i'm just seeing things.
 
@Ryzer it's only a problem if we are still a red petro-state which the majority of it's revenue come from oil and gas. If we can (or have) transitioned over manufactured and/or industrial goods, then we can safely keep our cheap oil and gas to turn them into plastic and petroleum products with additional value (since the cheaper oil would give us a better margin on them)
 
@Ryzer it's only a problem if we are still a red petro-state which the majority of it's revenue come from oil and gas. If we can (or have) transitioned over manufactured and/or industrial goods, then we can safely keep our cheap oil and gas to turn them into plastic and petroleum products with additional value (since the cheaper oil would give us a better margin on them)

Weren't we, technically, already diversifying exports with all of that steel we are producing?
 
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