A Sound of Thunder: The Rise of the Soviet Superbooster

Kistler had its own issues, SpaceX was the only Commerical Cargo bidder which had hardware built, a big difference from "on paper designs"

And given that Kistler was run by old guys and COULD NOT hit financial milestones, it wouldn't have the same success SpaceX has.
In 2006 and 2007 (actually as early as 1998), Kistler had hardware built and assembly begun, while SpaceX was still three years from being able to say the same, so you are simply factually wrong about that. And saying "they couldn't hit financial milestones, therefore they couldn't have succeeded if NASA had continued paying for the technical milestones" is also at best misleading, especially as NASA had cut them off at the knees in the market because they only issued contracts for two flights in 2007, instead of the initial 10-12 which they were supposed to have and which Kistler's pitch to investors was based around which lead to them only raising like 80-90% of the private matching funds they'd said they could. Though by letter of contract they were in violation and program rules said to cut them off, I think if they'd been able to continue on with NASA funds and the private investment they'd added, they could have made it to flight. They were not fated to be doomed, they just got a combination of unlucky and screwed by combinations of economic market health in general, NASA changes in personnel, and decisions on how milestones were written.

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Ya, the amout of cost bottlenecks SpaceX has reduced is insane, ULA did the same with Vulcan-Centaur to be competitive

Well, not on the engines - they're different for each stage, and they are both outsourced. But it's true that even so, Vulcan-Centaur will be cheaper to build and operate than either Delta IV or Atlas V, let alone both being operated at the same time.

I don't have a way off the top of my head to tie this into the timeline discussion, so I'll bow out now before taking this further off topic!
 
In 2006 and 2007 (actually as early as 1998), Kistler had hardware built and assembly begun, while SpaceX was still three years from being able to say the same, so you are simply factually wrong about that. And saying "they couldn't hit financial milestones, therefore they couldn't have succeeded if NASA had continued paying for the technical milestones" is also at best misleading, especially as NASA had cut them off at the knees in the market because they only issued contracts for two flights in 2007, instead of the initial 10-12 which they were supposed to have and which Kistler's pitch to investors was based around which lead to them only raising like 80-90% of the private matching funds they'd said they could. Though by letter of contract they were in violation and program rules said to cut them off, I think if they'd been able to continue on with NASA funds and the private investment they'd added, they could have made it to flight. They were not fated to be doomed, they just got a combination of unlucky and screwed by combinations of economic market health in general, NASA changes in personnel, and decisions on how milestones were written.

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Did they ever do a static fire or cryogenic fuel tank tests of some sort? Prototype F9 S1 with Merlin already was static firing by the end of 2007.
 
They already have a fine design, if it ain't broke don't fix it, having a different Upper stage would cost more and have a limited life span (Starship is supposed to replace Falcon)

They have a good design but its not as usable as it could be. I doubt a methalox propellant upper stage would be that much of a stretch for SpaceX given they were already paid to develop such. (Considering SpaceX initially planned on a pressure fed Raptor for HLS landing purposes there must have been some work achieved)

Most designs are frozen before a single part is made, while SpaceX is fluid in the design, costs more and gives more issues, but they get a better engine

Not that much 'better' considering how badly it's working at the moment. More so SpaceX used more common practices on the successful Falcon 9, and unlike Starship it actually worked.

They made orbit on raptors a few weeks ago (Starship was within 200m/s from orbit)

With multiple failures and "energetic" issues from the moment they shut down till Starship burned up on reentry. (Including something rather more 'energetic' given the amount of debris that happened at atmospheric interface)

Launch was flawless,

Well except for the clear signs of multiple Raptors on Superheavy not operating nominal as indicated by the dirty exhaust plume.

the relighting had issues, given its the first time it made it far enough for relighting, having issues is expected (Falcon 9 was the same, Falcon Heavy lost its core on first launch)

Again indications were there that multiple engines were failing during the boost back, A reliable engine is a must for a reusable vehicle.

Kistler had its own issues, SpaceX was the only Commercial Cargo bidder which had hardware built, a big difference from "on paper designs"

Not at all as Kistler had hardware already built and mostly tested whereas SpaceX did not having only the Falcon 1 at the time and had not started development of the Falcon 5 (which was their initial pitch) or the Falcon 9.
And given that Kistler was run by old guys and COULD NOT hit financial milestones, it wouldn't have the same success SpaceX has.

Old ex-NASA guys which is why it was the initial favorite front-runner :) And once Griffin came on board that switched to SpaceX who didn't even have working rocket at that time. (Griffin and Musk's words btw)

Delta 4 was too expensive for Commerical competition, even Atlas V was the same to an extent (cheaper to fly elsewhere)
Falcon 9 made both obsolete (far cheaper costs for payloads), and needing a replacement for Russian Engines, plus Russia refusing its engines for US Military payloads) meant ULA needed to change

Other way around the US launch services rejected the idea of depending on Russian engines.

A TL where SpaceX doesn't exist, same with CTOS, would need to change as well, Atlas V would be unviable, so likely a replacement for both would be needed, ULA would likely have a Delta V and Atlas VI (or Vulcan-Centaur) due to the need to have TWO DESIGNS incase one gets grounded

ULA had both the Delta IV and the Atlas V which were designed to meet the DoD requirements so that was likely going to continue without a general "commercial" launcher. COTS was aimed at commercial ISS supply with only a vague requirement of being an actual commercial launcher.

Where Musk is the trailblazer, Bezos is the follower, he would not be willing to take the same risks as Musk, New Glenn is still in design stages, and it was around before Starship and reusable Falcon
BOTH of which have flown, Blue Origin hasn't even made orbit and is basically "helping" in other contracts (lander)

Bezos never made any bones about his initial focus being on the suborbital tourism aspect of space flight. Time isn't really major factor here. Considering the BE4 actually works unlike the Raptor there's a good reason to believe that New Glenn will also likely work from the first flight. (Again unlike Starship)

Him using lawyers to delay and sabotage other contractors would not bode well in a no spaceX TL, US Military would not put up with that bullshit and Blue Origin would be blacklisted due to it. He pissed people off for the HLS contract case, Imagine him doing the same with a launch vehicle when he loses the contract

Hmmm Bezos called into question a dubious contract where and announced dual "winner" contract was suddenly cut down to only a single participant who was allowed to by the grantor to change their bid whereas none of the other participants were given such a chance and then that sole "authority" then "retires" to go work for SpaceX. Nothing fishy about that I'm sure. Had the military/DoD been involved with the procedure (they literally have no interest in the HLS contract) then you could be damn sure it would not be Blue Origins or Bezos who'd be under the microscope at this point. And lest we forget I clearly recall SpaceX suing ULA and the DoD over an already awarded contract so apparently the US Military DOES put with that bullshit after all since SpaceX has not been "blacklisted" yet. (More so it's been the DoD along with NASA who've been pushing ULA to have an alternative to SpaceX for good reasons)

Randy
 
Did they ever do a static fire or cryogenic fuel tank tests of some sort? Prototype F9 S1 with Merlin already was static firing by the end of 2007.
Aerojet Rocketdyne had conducted an extensive sequence of engine qualification tests on the engines in their original configuration in 1995 and the for-Kistler configuration in 1998, and the tanks were proof tested as they were produced. Obviously, as assembly wasn't completed, cryo testing of the completed vehicle or the three-engine cluster were not carried out. The AJR results are in AIAA 98-3361 MODIFICATION AND VERIFICATION TESTING OF A RUSSIAN NK-33 ROCKET ENGINE FOR REUSABLE AND RESTARTABLE APPLICATIONS.
 
Re: Kistler, see
That thread is actually...largely out of date with research it caused me to do and thus now probably as much wrong as right.
 
In 2006 and 2007 (actually as early as 1998), Kistler had hardware built and assembly begun, while SpaceX was still three years from being able to say the same, so you are simply factually wrong about that. And saying "they couldn't hit financial milestones, therefore they couldn't have succeeded if NASA had continued paying for the technical milestones" is also at best misleading, especially as NASA had cut them off at the knees in the market because they only issued contracts for two flights in 2007, instead of the initial 10-12 which they were supposed to have and which Kistler's pitch to investors was based around which lead to them only raising like 80-90% of the private matching funds they'd said they could. Though by letter of contract they were in violation and program rules said to cut them off, I think if they'd been able to continue on with NASA funds and the private investment they'd added, they could have made it to flight. They were not fated to be doomed, they just got a combination of unlucky and screwed by combinations of economic market health in general, NASA changes in personnel, and decisions on how milestones were written.
the milestone of half private half government money was a good call by NASA, to make sure whatever company gets CTOS isn't solely relying on government money
Kistler couldn't raise the funds

There are obviously other issues outside this (Griffen and Musk being friends), but even then there might be classified documents which show other reasons why they are cancelled, we only get a quarter to half the story

They have a good design but its not as usable as it could be. I doubt a methalox propellant upper stage would be that much of a stretch for SpaceX given they were already paid to develop such. (Considering SpaceX initially planned on a pressure fed Raptor for HLS landing purposes there must have been some work achieved)
Again, it would cost EXTRA for little benefit, Falcon Heavy doesn't fly much and the DOD payloads aren't heavy enough to need it, SpaceX uses the same pad and facility for Falcon 9 and Falcon Heavy, so both would need to be changed along with the launch pad infrastruction
Not to mention recerfity Falcon 9 for Crew flights due to the change

The metholox upper stage adds more headaches
Not that much 'better' considering how badly it's working at the moment. More so SpaceX used more common practices on the successful Falcon 9, and unlike Starship it actually worked.
Falcon 9 was also regulated by the US government, Musk spoke on this. The US GOV maintains oversight of ALL rockets built under government contracts for obvious reasons.


Starship is SELF FUNDED by SpaceX so oversight is far less of a thing, so common practice doesn't apply, hardware testing is just as good if not better then computer testing. the US government is just having FAA oversee SpaceX flights and not much else
Starship isn't exactly a conventional design for a rocket either, it would be like if a Areospace Company building commercial jets built their concept ones (the recent O design).
It might work, it might not, there is ONE way to prove it. Like the wright brothers with a fixed wing and tail design over bird like designs
With multiple failures and "energetic" issues from the moment they shut down till Starship burned up on reentry. (Including something rather more 'energetic' given the amount of debris that happened at atmospheric interface)
Starship burned up BY DESIGN, its the first flight which made it to stage sep, we are talking about this on a TL where N1 continues and gets the issues ironed out, a rocket which Starship is DIRECTLY compared to

Its a bare bones shell currently, so it being torn up on reentry isn't unexpected, the flight achieved its goals besides landing the booster in the ocean, Starship burned up over the Indian Ocean as intended

To list a few designs that had issues
STS-1 Columbia had spy satellites image the orbiter to ensure the heat shield was fine, and Young landed the thing with a broken Body Flap (said he would have ditched the Orbiter if he knew about it)
Shuttle also had tile damage on multiple flights, foam loss on every single flight and O-Ring damage on flights, it is still regarded as a good vehicle by the public
Saturn V flew Apollo 8 with all the issues Apollo 6 had to the moon, current NASA would have flew another unmanned mission and wouldn't dare send people to the moon
N1 blew up every time (likely second and third stages had issues as well but never got to show it) but is viewed as a rival to Saturn V

I get you don't like SpaceX, but give them a chance buddy

Starship is being developed with modifications in mind, they are in uncharted territory when it comes to designing a totally reusable rocket, spending 10 years designing it in a computer would still leave you with questions (will it really work?), SpaceX's model of flying a bunch of test models to prove concepts WORK is better

Well except for the clear signs of multiple Raptors on Superheavy not operating nominal as indicated by the dirty exhaust plume.
Still better than the second test flight, major issues only popped up on relight
Again indications were there that multiple engines were failing during the boost back, A reliable engine is a must for a reusable vehicle.
Falcon 9 had the same issues, both with engines not firing and engines cutting to early.

Not at all as Kistler had hardware already built and mostly tested whereas SpaceX did not having only the Falcon 1 at the time and had not started development of the Falcon 5 (which was their initial pitch) or the Falcon 9.
Old ex-NASA guys which is why it was the initial favorite front-runner :) And once Griffin came on board that switched to SpaceX who didn't even have working rocket at that time. (Griffin and Musk's words btw)
To innovate one needs a person who believes fully in the new concept and wants to SEE it to completion, Von Braun did this with rockets.

As I put above, there are likely issues we don't know about in regards to Kistler, and that's outside of the Musk/Griffen stuff
Other way around the US launch services rejected the idea of depending on Russian engines.
Russia threatening to cut of Soyuz flights and engines were what caused the US to change, US lawmakers realized russian engines being cut would ground Atlas. Plus the optics of buying stuff from a hostile Russia would be bad for politicians

ULA had both the Delta IV and the Atlas V which were designed to meet the DoD requirements so that was likely going to continue without a general "commercial" launcher. COTS was aimed at commercial ISS supply with only a vague requirement of being an actual commercial launcher.
What I mean is, without SpaceX the launch market would still be dominated by foreign and European launchers, majority of Delta 4 and Atlas v Payloads are government payloads
Bezos never made any bones about his initial focus being on the suborbital tourism aspect of space flight. Time isn't really major factor here. Considering the BE4 actually works unlike the Raptor there's a good reason to believe that New Glenn will also likely work from the first flight. (Again unlike Starship)
New Glenn is still a decade away (I would be surprised at a launch before 2030), BE-4 had all kinds of delays, delaying Vulcan-Centaur by a year

I'll trust the rocket actually flying right now to fly better, New Glenn might be the same shitshow

Hmmm Bezos called into question a dubious contract where and announced dual "winner" contract was suddenly cut down to only a single participant who was allowed to by the grantor to change their bid whereas none of the other participants were given such a chance and then that sole "authority" then "retires" to go work for SpaceX. Nothing fishy about that I'm sure. Had the military/DoD been involved with the procedure (they literally have no interest in the HLS contract) then you could be damn sure it would not be Blue Origins or Bezos who'd be under the microscope at this point. And lest we forget I clearly recall SpaceX suing ULA and the DoD over an already awarded contract so apparently the US Military DOES put with that bullshit after all since SpaceX has not been "blacklisted" yet. (More so it's been the DoD along with NASA who've been pushing ULA to have an alternative to SpaceX for good reasons)
NASA requested funding for two, Congress mandated two but funded enough for ONE LANDER
NASA then did an audit of landers and found SpaceX to be the cheapest, most downmass and the only one with HARDWARE BUILT for a then expected landing in 2024-2025
Even if Starship can put down a fraction of the 100 tons (20 or 30) its still more then the other two, the dynetics lander had negative downmass and National Team was second choice
NASA did the responsible thing and funded one design fully over two half funded designs, it would be like if NASA funded Saturn V and Saturn-8 side by side and didn't land until 1972 due to funding issues for both rockets

Corruption happens everywhere, it happening for space-related contracts is no surprise
 
Thinking a bit about american commercial space ITTL
NASA Lost its monopoly, but it hasn’t yet been required to procure its launch services commercially (Launch Service Purchase act of 1990) , this bill was definitely not certain to pass, or even be proposed, from an AH perspective, and it may be harder to pass with a less severe mid 80s shuttle failure. It seems this bill did have a some effect, most of the space access commercialisation efforts started in the second half of the 80s (and would coincide with the increased supply of LV that was planned by the DoD since these days anyway) but NASA did sign more contracts after, notably with Orbital Science (Which it was already working with on Pegasus) and Space Services/Conestoga in the wake of the bill, and it did seem that it increased confidence among established LSP to produce larger batches of rockets. So maybe this should be taken into account.

Before that bill in 1986 there was another proposal (that failed), the Commercial Space Incentive Act, that would also make the US federal government subsidies any payload Launched by private LSP to $500/lbs if they were above 10,000 lbs, one of the argument for thay bill was apparently as a way to catch up with the soviet launch capabilities, maybe this would be more impactful ITTL...

There’s OTRAG but it was doomed by politics before it could be doomed by technical issues.
On the American side, there’s Space Services, AMROC, Orbital science, EPAC, which all have deep enough roots in the 80s that they could probably avoid being butterflied away.

EPAC and Taurus are maybe a bit too tied to Peacekeeper and ICBMs that their future is too dependent on the geopolitics to make predictions.

AMROC had some fundamental problems, Hybrids don’t scale well, have bad mass ratio their only way for larger launcher would have been clustering... but they did have a streak of bad luck in timing and the accidental death of their co-founder, (and they did put a Falcon 1-sized rocket on the pad, even if it didn’t leave it upright) more importantly they were one of the few companies of the days to build their own main propulsion, maybe if they do reach orbit this could give more confidence in non-solid private launcher projects in the 90s?

There are the various projects of Gary Hudson between Percheron and Roton, most notably the Liberty 1 air launched rocket that tried to compete with Orbital science for that Military funding, which somehow went up to making a pressure fed S1 prototype - did anyone even try pump fed liquid engines at the time? Pacific American wanted to make a Liberty 2 using Refurbished F1 - seems like they’d be particularly interested in using soviet engines if they are allowed.

Then in the late 80s there’s already Vega and Scout 2 - and whatever Fiat Avio was trying to do to sell their various SRBs, useless until they lobbied the Italian space agency enough that they’d threaten ESA funding to get the French approval, working through ESA and Arianespace is useless at this point, and Europe doesn’t have the necessary VC funding environment yet.
 
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the milestone of half private half government money was a good call by NASA, to make sure whatever company gets CTOS isn't solely relying on government money
Kistler couldn't raise the funds

Not be an nit-picker but it's COTS :)

There are obviously other issues outside this (Griffin and Musk being friends), but even then there might be classified documents which show other reasons why they are cancelled, we only get a quarter to half the story

Both fans of Zubrin's Mars Direct and members of the Mars Society. Griffin and Musk have said that it was Griffin's suggestion he develop his own launch company. This was outside NASA when Griffin was part of In-Q-Tell. He and Musk had just gone to Russia (2001) to try and buy a cheap ICBM ride to get Musk's greenhouse on Mars. Griffin gave Musk NASA money before he even had anything designed let alone built.

Again, it would cost EXTRA for little benefit, Falcon Heavy doesn't fly much and the DOD payloads aren't heavy enough to need it, SpaceX uses the same pad and facility for Falcon 9 and Falcon Heavy, so both would need to be changed along with the launch pad infrastructure
Not to mention recertify Falcon 9 for Crew flights due to the change

The metholox upper stage adds more headaches

It gains significant payload and makes it possible to have a reusable second stage. This is pretty much a win/win IF SpaceX (Musk specifically) was at all interested in actually lowering the cost of launch and maybe building up Cis-Lunar space to allow a much better background for getting to Mars. Musk doesn't want to wait so he's going for Starship. (Toss up that he's trading "not dying on impact" for "dying during launch")

Falcon 9 was also regulated by the US government, Musk spoke on this. The US GOV maintains oversight of ALL rockets built under government contracts for obvious reasons.

Eh the "oversight" is literally ensuring that the company gives the government payloads a certain priority. It's not very close regulation and it respects a companies' "private" information. Your suggesting that it was the government "regulation" that allowed Falcon to be successful and why Starship is failing? That's not at all what's going on.

Starship is SELF FUNDED by SpaceX

No, Starship is fully and openly funded by public funding and private investment. Both of which are running out given the issues of the system. Musk hasn't spend a dime on it nor has SpaceX. (Though he's skimmed money from Tesla quite a number of times)

... so oversight is far less of a thing, so common practice doesn't apply, hardware testing is just as good if not better then computer testing. the US government is just having FAA oversee SpaceX flights and not much else

Yep it's why the DoD has no interest in Starship, (barring a couple million for the point-to-point study that Space Force has advanced to SpaceX, answer it still that P2P doesn't make a lot of sense and isn't cost effective) and why they won't be manifesting any payloads on Starship even if it does work as advertised. There is FAR more than just the FAA looking at SpaceX. So far SpaceX has managed to get on the bad side of the Army Corps of Engineers, State and Federal wildlife services and a ton of environmental groups by sticking to a very bad launch site and screwing up the surroundings. SpaceX is under investigation by the Labor department as well. It's only March and SpaceX has already almost run out of hours they are allowed to shut down the roads and beaches in the area. Something Texas takes VERY seriously. (aka it's actually enshrined in their Constitution)

Starship isn't exactly a conventional design for a rocket either, it would be like if a Aerospace Company building commercial jets built their concept ones (the recent O design).
It might work, it might not, there is ONE way to prove it. Like the wright brothers with a fixed wing and tail design over bird like designs

Oddly the fact that commercial companies DON'T start by crashing their design due to lack of foresight and planning is a major reason most of them are still in business. Note that the Wrights specifically did advanced design and testing BEFORE they every tried to build a flying glider let alone a powered aircraft. Exactly the opposite of what SpaceX did for Falcon 9. The Wright brothers couldn't afford a nonworking design, seems SpaceX can.

Starship burned up BY DESIGN, its the first flight which made it to stage sep, we are talking about this on a TL where N1 continues and gets the issues ironed out, a rocket which Starship is DIRECTLY compared to

Uhm no, exactly the opposite in fact. Starship lost all control shortly after engine shut down and disintegrated due to that same lack of control having in enter backwards and almost upside down. And Starship has made it to stage separation twice now, not once.
IN context to the thead, yes we are discussing a timeline where the N1 works but also in context at no point did the designers set "clearing the tower" as the goal. They designed it to make orbit and that was always the goal. So far we've had one "success" of clearing the tower but the overall flight failing, one reaching staging, (which itself was changed because the first method was stupid) and then failing and now one failing to either "soft land the booster" (first stated goal) and second reentering the upper stage (second stated goal) and a number of "sub-goals" that were skipped due to issues with the design.
Literally the only thing that's "compared" between the N1 and Starship is the number of engines with the main point being that's not a good idea and so far it seems that's correct.

It's a bare bones shell currently, so it being torn up on reentry isn't unexpected, the flight achieved its goals besides landing the booster in the ocean, Starship burned up over the Indian Ocean as intended

Think about that for a second, it's an empty shell that barely made orbit with approximately 90% of a full propellant load that had several issues with its engines and flight controls all of which failed at some point. It has no mass simulators onboard for planned systems and even the door may not have worked as planned.
Let's NOT move the goal posts here shall we? Superheavy was to planned to make a hovering maneuver (long enough for the chopsticks to snatch it) before it splashed down in the Gulf of Mexico. It failed. Starships goal was a successful reentry to a "splashdown" in the Indian Ocean NOT to burn up on reentry because it was out of control. It failed and the TPS is still an unknown, as is how the vehicle will be controlled because evidence says the current RCS is not working. (And top that with the ongoing plumbing and engine issues along with the control issues)

To list a few designs that had issues
STS-1 Columbia had spy satellites image the orbiter to ensure the heat shield was fine, and Young landed the thing with a broken Body Flap (said he would have ditched the Orbiter if he knew about it)

Yet it was a successful mission despite that due to the time and effort put into planning and building the Orbiter. Not helping your case here.

Shuttle also had tile damage on multiple flights, foam loss on every single flight and O-Ring damage on flights, it is still regarded as a good vehicle by the public

Because despite these issues it still worked, again because time and effort were taken to do the job correctly. Starship has literally failed out the gate from the start because this has NOT been done.

Saturn V flew Apollo 8 with all the issues Apollo 6 had to the moon, current NASA would have flew another unmanned mission and wouldn't dare send people to the moon

Apollo was designed around getting people to the Moon, NASA had very little use for automated mission at the time and prefered 'risking' a crew rather than trying to do things with automation. A lot of that was a need to convince Congress that the risks could be managed after the Apollo 1 fire. Similarly today mollify Congress over the ability to reach the Moon requires NASA do things different hence an automated flight followed up by a manned flight.

N1 blew up every time (likely second and third stages had issues as well but never got to show it) but is viewed as a rival to Saturn V

Closer to a Saturn 1B rival but yes it was seen as the Soviet Lunar booster as is envisioned here.

I get you don't like SpaceX, but give them a chance buddy

Not sure where you got that idea from, I actually love what SpaceX has done specifically with the Falcon. I'd like to see them succeed with Starship but frankly the fact that they keep failing and that failing is due to a clear lack of planning and development, again exactly opposite of what we saw with the Falcon development, and watching the time and public money being wasted on a badly planned and designed vehicle is pretty frustrating.

Starship is being developed with modifications in mind, they are in uncharted territory when it comes to designing a totally reusable rocket, spending 10 years designing it in a computer would still leave you with questions (will it really work?), SpaceX's model of flying a bunch of test models to prove concepts WORK is better

And they have failed to prove that this "process" is better than actually taking time and effort to carefully plan and build a working vehicle. This isn't "uncharted territory" it's a very well established and proven methodology to designing and building a working launch vehicle. SpaceX in fact used that exact methodology to design and build the Falcon 9. Instead we've got Musk suggesting that an expandable Starship makes a lot of sense. (It doesn't) What we have instead is a set of arbitrary "points" that Musk has invented that are driving the design and failing badly.
Musk wants "Mars Direct" on steroids', so he's building a super-heavy launch vehicle with public and private (but not his) money that requires a very careful and well planned development program that he essentially doesn't want to do. Instead we keep getting failure after failure. We COULD be sending flights to Mars today if Musk wasn't fixated on his personal "plan" which is unsupported by any evidence or work, (part of the reason Zubrin's been trying to talk him down) and have wasted a lot of time and a lot of money simply so Elon can put on a show rather than an actual development program.

Still better than the second test flight, major issues only popped up on relight

Eh no, there were problems right off the pad. The methalox engines were obviously not running nominally or there wouldn't have been the obvious smoke trail. Engines were showing signs of significant problems in flight with flares and outgassing (greenish exhaust showing they were falling apart) which followed with engines outright failing and looking like several exploded when trying to relight. Starship had engine issues too including an "event" as the engines shut down that was followed by a large uncontrolled leak of (likely) propellant that ended up driving the Starship totally out of control for most of the 'coast' phase and another shortly before atmospheric interface which blew a lot debris out of the engine bay and off the hull itself. This wasn't 'better' it was simply allowing more time for more failures to show up.

Falcon 9 had the same issues, both with engines not firing and engines cutting to early.

And in most cases Falcon 9 had plenty of margin to handle these issues and a well planned and carried out program to fix them. Mostly without loss of mission.

To innovate one needs a person who believes fully in the new concept and wants to SEE it to completion, Von Braun did this with rockets.

So again nothing like we're seeing with Starship since they don't actually HAVE a good plan and are literally just winging it?
Kistler actually DID have a pretty innovative plan, pretty much coming up with most of what SpaceX is doing well before SpaceX even existed. Fully reusable from the start, (unlike Starship) boost back and landing (parachutes but that allowed them to carry more payload to orbit) back at base for rapid reuse.

As I put above, there are likely issues we don't know about in regards to Kistler, and that's outside of the Musk/Griffin stuff

It was a rather open "secret" that Kistler having ex-NASA people working there was the main reason they got a no-bid contract. Boeing and Lockheed were not happy about that and protested which killed that deal and forces Kistler to seek private funding.

Russia threatening to cut of Soyuz flights and engines were what caused the US to change, US lawmakers realized russian engines being cut would ground Atlas. Plus the optics of buying stuff from a hostile Russia would be bad for politicians

Ya the politicians had already cut funding efforts by NASA to build a new domestic engine to replace the Russian ones, and had to scramble to "fix" the optics.

What I mean is, without SpaceX the launch market would still be dominated by foreign and European launchers, majority of Delta 4 and Atlas v Payloads are government payloads

Possibly as the US wasn't without options and frankly NASA was wanting "something" as a program and Congress was getting to the point where they might have been willing to actually fund it.

New Glenn is still a decade away (I would be surprised at a launch before 2030), BE-4 had all kinds of delays, delaying Vulcan-Centaur by a year

Ya it's frustrating when a company takes the time and effort to ensure its engine works rather than wasting a lot of time and money on rushing it into service and it not working. I wouldn't count on New Glenn being that far out considering Bezos is actually putting his own money for it and it's aimed at an actual market.

I'll trust the rocket actually flying right now to fly better, New Glenn might be the same shitshow

You mean the Falcon 9? Because it's the only one "flying right now", so far Starship IS a shitshow. And New Glenn might or it might not but it's highly likely it will at least fly successfully unlike Starship.

NASA requested funding for two, Congress mandated two but funded enough for ONE LANDER

Actually Congress specifically didn't fund ANY lander as they purposefully didn't fund enough for even one of the bids. The finally reversed and gave funding for a second lander when it looked like they might actually get some pushback for publicly short-changing their own "mandate". (And people were already noting they'd done that consistently with SLS. Optics were turning bad for them.

NASA then did an audit of landers and found SpaceX to be the cheapest, most downmass and the only one with HARDWARE BUILT for a then expected landing in 2024-2025

Eh no, ONE person at NASA instigated an "audit" (while informing SpaceX of the new funding limit) and ONE person decided that SpaceX would be awarded the contract after SpaceX changed its bid to fall under the given funding limit. This person then retired from NASA and now works for SpaceX... Rather odd really. And to be clear SpaceX has essentially an empty shell as "hardware" which to this date STILL doesn't have a final design for the HLS nor was it going to be 'ready' for Artemis as NASA itself has pointed out because it also didn't have a booster designed for the mission.

Even if Starship can put down a fraction of the 100 tons (20 or 30) its still more then the other two, the dynetics lander had negative downmass and National Team was second choice
NASA did the responsible thing and funded one design fully over two half funded designs,

And oddly neither Dynetics nor the National Team were even given a chance to reconsider their bids with the actual funding available. As NASA was in fact both mandated and looking for TWO designs, being responsible would have actually been to fund two lander designs as required and go back to Congress for sufficient funding. Instead ONE PERSON decided to fund SpaceX's new bid which oddly was just under the amount Congress had authorized, (almost like they knew what that price was) and ignore the Congressional mandate. (And once a new Administrator had been installed HE went back to Congress and got additional funding for a second bid)

it would be like if NASA funded Saturn V and Saturn-8 side by side and didn't land until 1972 due to funding issues for both rockets

Apples and engine block comparison. NASA had a plan and was hard at work designing and building the Saturn V which was specifically designed to meet the needs of mission and also designed to have plenty of margin to work with. The entire situation let alone the details are not applicable to the current situation.

Randy
 
There are obviously other issues outside this (Griffen and Musk being friends), but even then there might be classified documents which show other reasons why they are cancelled, we only get a quarter to half the story
I've interviewed a fair bit of the design team and senior leadership that's still alive so I think I have a slightly better idea of what was going on than you do, and you inventing "maybe there's classified documents that show they had other stuff wrong beyond the publicly stated reasons they were dropped for not meeting milestones" comes off as you trying to invent reasons you're not wrong when every single fact says you are.
New Glenn is still a decade away (I would be surprised at a launch before 2030), BE-4 had all kinds of delays, delaying Vulcan-Centaur by a year
I think you should prepare to be surprised, and also I would point out Vulcan-Centaur was in the end delayed by Centaur V structural testing, not BE-4s. They had the engines for the maiden launch like a year and a half before the first flight, and the core for the first flight was at the Cape about a year before it finally flew.
 
I wouldn't count on New Glenn being that far out considering Bezos is actually putting his own money for it and it's aimed at an actual market.
And considering they rolled flight tankage to the pad last month, and it's now headed back to the hangar to be reset for static fire...
 
Thinking a bit about American commercial space ITTL
NASA Lost its monopoly, but it hasn’t yet been required to procure its launch services commercially (Launch Service Purchase act of 1990) , this bill was definitely not certain to pass, or even be proposed, from an AH perspective, and it may be harder to pass with a less severe mid 80s shuttle failure. It seems this bill did have a some effect, most of the space access commercialization efforts started in the second half of the 80s (and would coincide with the increased supply of LV that was planned by the DoD since these days anyway) but NASA did sign more contracts after, notably with Orbital Science (Which it was already working with on Pegasus) and Space Services/Conestoga in the wake of the bill, and it did seem that it increased confidence among established LSP to produce larger batches of rockets. So maybe this should be taken into account.

Agree, in context a lot of the "privatization" and "commercialization" of government services was undertaken after the Cold War ended as a political move to shore up waning defense spending and ensure some basic services. Motivations and outcomes are likely to be a bit different in TTL.

Before that bill in 1986 there was another proposal (that failed), the Commercial Space Incentive Act, that would also make the US federal government subsidies any payload Launched by private LSP to $500/lbs if they were above 10,000 lbs, one of the argument for the bill was apparently as a way to catch up with the soviet launch capabilities, maybe this would be more impactful ITTL...

interesting idea, I can see the draw in TTL.

There’s OTRAG but it was doomed by politics before it could be doomed by technical issues.
On the American side, there’s Space Services, AMROC, Orbital science, EPAC, which all have deep enough roots in the 80s that they could probably avoid being butterflied away.

Would love to see the first launch of AMROC made into a success :)
"Scidbladnir" deserved a better shot :)

EPAC and Taurus are maybe a bit too tied to Peacekeeper and ICBMs that their future is too dependent on the geopolitics to make predictions.

Suspect that TTL is still on track to trading away "Peacekeeper" so those boosters will likely still be available. (There were a lot of issues with it's deployment already which are still in place)

AMROC had some fundamental problems, Hybrids don’t scale well, have bad mass ratio their only way for larger launcher would have been clustering... but they did have a streak of bad luck in timing and the accidental death of their co-founder, (and they did put a Falcon 1-sized rocket on the pad, even if it didn’t leave it upright) more importantly they were one of the few companies of the days to build their own main propulsion, maybe if they do reach orbit this could give more confidence in non-solid private launcher projects in the 90s?

Possible, there were quite a few lesser companies that were facing investor confidence issues at the time as well.
(And i recall a plethora of both launch companies being organized and new propulsion companies as well as some interesting R&D efforts. (Hybrids based on candle wax for example, though that was more towards the early 2000s. Interestingly an offshoot of more intense research on how solid combustion worked :) )

There are the various projects of Gary Hudson between Percheron and Roton, most notably the Liberty 1 air launched rocket that tried to compete with Orbital science for that Military funding, which somehow went up to making a pressure fed S1 prototype - did anyone even try pump fed liquid engines at the time?

More background and information here. (Gary is still active on NSF so it's interesting to read his take on things)
Pump fed was always in the background as most efforts were directed towards cheap launch whereas the conventional wisdom is that turbopumps are the exact opposite of "cheap" :) This trend eventually lead to the testing of "VPac" pressure fed designs which itself lead to autogenous self-pressurization concepts. t also lead to some alternative pump systems such as the piston pump concept.
Pacific American wanted to make a Liberty 2 using Refurbished F1 - seems like they’d be particularly interested in using soviet engines if they are allowed.

Maybe? Gary was pretty active towards DoD requirements even when aimed solely at "private" launch :) I'm pretty sure he was aware of how leery they were about using "non-American" engines.

Then in the late 80s there’s already Vega and Scout 2 - and whatever Fiat Avio was trying to do to sell their various SRBs, useless until they lobbied the Italian space agency enough that they’d threaten ESA funding to get the French approval, working through ESA and Arianespace is useless at this point, and Europe doesn’t have the necessary VC funding environment yet.

IIRC there was quite a surge of launch concepts in the mid-to-late 80s, mostly tied up to the then new idea of satellite communication constellations in LEO rather than GEO. I recall being quite surprised by the base BX's I was stationed at actually carrying a wide selection of LSP trade magazines :)

Randy
 
Yep it's why the DoD has no interest in Starship, (barring a couple million for the point-to-point study that Space Force has advanced to SpaceX, answer it still that P2P doesn't make a lot of sense and isn't cost effective) and why they won't be manifesting any payloads on Starship even if it does work as advertised.

@RanulfC clearly you have a massive axe to grind with Starship, but this statement below needs to be updated since the DoD has shown interest with buying and operating a Starship since February 2024.

 
If you actually look at the additional delay from tbe point each recent new rockets went to pad for tanking test to their final launch (H3, Vulcan, A6, Starship), the average is definitely above the year of delay - with only Vulcan being a bit under (May 2023 to January 2024) - In all likelihood New Glenn is still a year away from launch
I'd bet it's a lot closer to a year or less than it is to "won't launch before 2030," which was the assertion.

It’s also not, iirc, Tankage for the first flight, just subsequent ones
I didn't assert it was the first flight's tankage, just that it is flight-intended tankage, and that it will be static fired, and then the first flight vehicle (whether those tanks or others) should be ready soon:

https://aviationweek.com/aerospace/commercial-space/new-glenn-rolls-launchpad-tanking-test
Following the ITT, the first stage will be outfitted with an aft structure and the BE-4 engines, mated with a new upper stage and then returned to the launchpad this summer for a hot fire. Jones expects to be ready to launch the first New Glenn vehicle shortly thereafter. Engines for the hot fire are completing qualification testing at Blue’s West Texas facility.
 
I'd bet it's a lot closer to a year or less than it is to "won't launch before 2030," which was the assertion.


I didn't assert it was the first flight's tankage, just that it is flight-intended tankage, and that it will be static fired, and then the first flight vehicle (whether those tanks or others) should be ready soon:

https://aviationweek.com/aerospace/commercial-space/new-glenn-rolls-launchpad-tanking-test
You are right
Sorry, thought my Post was off topic
 
@RanulfC clearly you have a massive axe to grind with Starship, but this statement below needs to be updated since the DoD has shown interest with buying and operating a Starship since February 2024.


Not a massive axe, just pointing out the reality. No I don't like Starship, I am still wanting to see it succeed and prove me wrong but that's not the direction it's going. Yes the DoD enquired about buying and operating Starship, (the answer is essentially no, Musk doesn't let anyone operate or use SpaceX equipment) as a supposed "fully reusable system from the start" that was a given per the DoD's launch mission. (They investigated the Shuttle in a similar manner, Congress said no to that one) ACTUALLY buying and operating a Starship is not on the table, it's literally just a suggestion, just like the P2P work. Once New Glenn is in advanced testing then that too will be considered for the same reason.
(It does not help that Aviation Week was the ones who broke the story)
Note the article also points out that SpaceX is about five years behind on it's own development track for Starship.

Starship has the main issue in that there is (literally) nothing to it at this point.

Randy
 
It gains significant payload and makes it possible to have a reusable second stage.
Reusable second stage isn't worth the development costs, you would have to recertify crew and bring an object back from LEO or even GEO orbits. Which SPACEX themselves said was too much of a pain in the ass to achieve once, let alone routinely, it would also eat into payload margins due to slowing burns and the landing concept

Not to mention adding two fuel types to the pad infrustructure and requiring changes, which SpaceX wants to avoid

Yep it's why the DoD has no interest in Starship, (barring a couple million for the point-to-point study that Space Force has advanced to SpaceX, answer it still that P2P doesn't make a lot of sense and isn't cost effective) and why they won't be manifesting any payloads on Starship even if it does work as advertised.
When Starship is flying regularly they want to fly it like a cargo business, the US military if it wants can subcontract a variant for their use, SpaceX wants Starship to be theirs first, not a US Government controlled rocket

Oddly the fact that commercial companies DON'T start by crashing their design due to lack of foresight and planning is a major reason most of them are still in business. Note that the Wrights specifically did advanced design and testing BEFORE they every tried to build a flying glider let alone a powered aircraft. Exactly the opposite of what SpaceX did for Falcon 9. The Wright brothers couldn't afford a nonworking design, seems SpaceX can.
A fucking TON of designs worked out on paper for planes didn't work, like the "add more wings" idea, rockets blew up near constantly.
There is a reason why life expectancy of test pilots were short until the 30s and 40s, even into the 50s new designs were made "the proper way" which didn't work that well

Some designs MAY work on paper but NOT in reality, SpaceX wants to prove it works through hardware testing and not spending 5 years on a computer and another 5 building it

Think about that for a second, it's an empty shell that barely made orbit with approximately 90% of a full propellant load that had several issues with its engines and flight controls all of which failed at some point. It has no mass simulators onboard for planned systems and even the door may not have worked as planned.
Let's NOT move the goal posts here shall we? Superheavy was to planned to make a hovering maneuver (long enough for the chopsticks to snatch it) before it splashed down in the Gulf of Mexico. It failed. Starships goal was a successful reentry to a "splashdown" in the Indian Ocean NOT to burn up on reentry because it was out of control. It failed and the TPS is still an unknown, as is how the vehicle will be controlled because evidence says the current RCS is not working. (And top that with the ongoing plumbing and engine issues along with the control issues.
Shuttle TPS was unknown as well, ablators were considered

Its a test model, akin to boilerplates being used on Saturn 1, 1b and V tests, the chief objective is to learn from the data and build a better design
Not sure where you got that idea from, I actually love what SpaceX has done specifically with the Falcon. I'd like to see them succeed with Starship but frankly the fact that they keep failing and that failing is due to a clear lack of planning and development, again exactly opposite of what we saw with the Falcon development, and watching the time and public money being wasted on a badly planned and designed vehicle is pretty frustrating.
You have a massive axe to grind on Starship, and with the second-stage stuff it seems like you hate SpaceX

Raptor is an EXCELLENT engine, if it wasn't it would not be used, the N1 had the same issues with plumbing and engines
It was a rather open "secret" that Kistler having ex-NASA people working there was the main reason they got a no-bid contract. Boeing and Lockheed were not happy about that and protested which killed that deal and forces Kistler to seek private funding.
I am not a big Kistler fan, so having this "favouritism" in contracts is the same as Griffen and Musk
Boeing and Lockheed are right in this situation

This behind the scenes Bullshit happens everywhere, I read Grumman was the best choice to build the shuttle but Rockwell got the bid, the F-35 had a different tail design initially but it was changed to a conventional rudder and elevator design over the integrated rudder/elevator

Kistler needing private funding was a good thing overall, it forces the business to be "invested" and not just gleening government money, the fact they weren't able to reach the goal meant they were cut, it is sad but it happens
Ya it's frustrating when a company takes the time and effort to ensure its engine works rather than wasting a lot of time and money on rushing it into service and it not working. I wouldn't count on New Glenn being that far out considering Bezos is actually putting his own money for it and it's aimed at an actual market.
Raptor works fine, just grouping them together is causing issues, like the N1 engine, the F-1 had to have heat protection covers to make sure the engines on the Saturn V survived to orbit without melting

Eh no, ONE person at NASA instigated an "audit" (while informing SpaceX of the new funding limit) and ONE person decided that SpaceX would be awarded the contract after SpaceX changed its bid to fall under the given funding limit. This person then retired from NASA and now works for SpaceX... Rather odd really. And to be clear SpaceX has essentially an empty shell as "hardware" which to this date STILL doesn't have a final design for the HLS nor was it going to be 'ready' for Artemis as NASA itself has pointed out because it also didn't have a booster designed for the mission.
The Lunar module changed design and weight into 66-67

HLS launches on Starship, not SLS

And oddly neither Dynetics nor the National Team were even given a chance to reconsider their bids with the actual funding available. As NASA was in fact both mandated and looking for TWO designs, being responsible would have actually been to fund two lander designs as required and go back to Congress for sufficient funding. Instead ONE PERSON decided to fund SpaceX's new bid which oddly was just under the amount Congress had authorized, (almost like they knew what that price was) and ignore the Congressional mandate. (And once a new Administrator had been installed HE went back to Congress and got additional funding for a second bid)
I like how you avoid the technical details of the other bids, Dynetic's design was TOO HEAVY and the National Team didn't have much growth options (a part of the audit)

The political climate is different from 2019 and 2020 to now,
Apples and engine block comparison. NASA had a plan and was hard at work designing and building the Saturn V which was specifically designed to meet the needs of mission and also designed to have plenty of margin to work with. The entire situation let alone the details are not applicable to the current situation.
We do not have the actual technical specs of the Starship besides the basic weight and expected mass to orbit. We do not know what "leftover" weight there is for the design to suck up later, worst case they

Comparing the Starship to Saturn V is comparing Apples to Oranges
The Saturn was an unsustainable design designed specifically to shoot people at the moon and land a few times, growth for the rocket was expensive and its mission to land people unpopular with the majority of the public and politicians
The Starship is designed to be Sustainable and designed to act like a "Space Truck" for routine, reusable flights to space at lower costs than competitors and fly a hundred times or more, and be used to expand humans into the solar system

It is literally uncharted territory in spacecraft designs, as designs for sending people beyond LEO are all paper designs (if you don't count Orion and SLS's Mars flyby idea) and designs for this that are FULLY REUSABLE are hard to find outside small studies
 
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