Boldly Going: A History of an American Space Station

It can probably be used for orbital reboost though and as established tech may still keep costs down.
So for reference, an OMS engine has 26.7 kilo-newtons (kN) of thrust. There's 2 on an orbiter, so that's a total of 53.4 kN of thrust.
The two bigger engines on the Zvezda module, which are the on-board option for reboosting the ISS, have 3 kN of thrust each, for a grand total of 6 kN.
And that's for ISS, which is a bigger... well, a probably bigger station that definitely has more drag.
The OMS engines are just waaaaaaaay more than what's needed.
 

marathag

Banned
Columbia in contrast was inevitable as the foam was Russian roulette just with 107 barrels instead of six. Going back to STS-1 the death shot could have come at any time.
Years back, think I came across that the initial painting of the Tank on the early flights may have inhibited that behavior to shed.
Do not know if true
 
Can't answer the rest but as the SSME can't be restarted on orbit they'll pretty much have to use the OMS for that job. Or build a new system that rather defeats the purpose of using a Shuttle in the first place...

The only reason I ask is because the OMS engines are a lot more than is needed for station keeping. A smaller more efficient custom system would seem reasonable if practical.

Which then ties into the other questions. If you don't need and OMS-1 burn, then maybe leaving the OMS engines off altogether and using a smaller system is a good idea. If you do need an OMS-1, then why add another engine when the OMS will do the job.

While the SII proposals called for replacing the OMS engines with a pair of four-engine clusters (500 lbf per unit or 2000lbf per pod)and converting the entire system to monopropellent, what we have here makes neither of these changes. Instead, we've gone with retaining the existing pods, and the hours of life on both RCS jets and OMS AJ10-190 (6000lbf each). This is expected to be enough to support this interim station. The one change that is made is that Enterprise is receiving the "Forward RCS Interconnect System", which is a series of lines that connect the Aft OMS pods with the forward RCS pallet. On the orbiters, this would allow for the movement of RCS prop to help maintain the center of gravity on landing. For Enterprise this is the basis for the connections that also allow for the station to be refueled on orbit over the life of the outpost (as it was in OTL for the US ISS propulsion module). Historically, in 1999 Enterprise was used as the basis for checking clearances on the FRCS system in the space between the crew compartment and the outer skin of the vehicle (Jenkins II-412). Given all of this, reboost might be done by OMS or RCS, depending on the magnitude of the burn (and there are lots of RCS jets that can be fired off individually to wear-level the system), or even by visiting shuttles, which can have their engines looked at on the ground (the initial plans are certainly to use other shuttles for the majority of the reboost).

As for the CoM issues of the orbiter having the tank attached, burning the OMS engines such a situation was used on the STS-51-F Abort-to-Orbit burn, and was programed for almost all aborts (it was referred to as a fuel dump). Here however, at least early on, the shuttle's payload bay is full of stuff and the tanks in the ET are empty which helps reduce off-axis problems for the CoM of the combined stack.


Years back, think I came across that the initial painting of the Tank on the early flights may have inhibited that behavior to shed.
Do not know if true
The painting on the tank was to reduce the exposure of the foam to UV radiation which was thought to degrade it, not for thermal control as I have heard said. Experimentally, it was found that the UV would only penetrate the outermost millimeters of the foam, and this was considered acceptable (the bits that could theoretically come off because of this degradation would be very thin, very unstable, and would break apart before they could impact the shuttle).

To come back to your point, the paint on the ET could itself be shed off, and thus represented further debris that could impact the shuttle, which was why it wasn't considered as an option in the post-Columbia environment.
 
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Image Annex: Space Shuttle Enterprise Cabin Images
So, Just to give an additional perspective on what the orbiter would have looked like when it came back from Paris to be taken apart, we have these images that were taken by Dennis R. Jenkins at some point:








 
Part 4: While Enterprise work proceeds, Shuttle sees successes - but danger lurks
Boldly Going Part 4

The early years of Enterprise’s path to flight proceeded against a backdrop of general success in the Shuttle program. The Spacelab module made its orbital debut in a demo flight in 1983, followed by an operational debut on STS-51-B in 1985. This flight and two more Spacelab missions that same year helped clear the path for the three-segment Spacelab module which would be launched aboard Space Station Enterprise to serve as the station’s initial primary laboratory facilities. However, the nine missions of 1985 were put to shame by the planned schedule for the following year. Shuttle flights might be becoming routine, but they were still news, particularly when it seemed every mission broke new ground. Some flight objectives were less immediately gripping, like the launch of one military and two civilian comsats aboard STS-61-H. However, even such “ordinary” missions achieved some note. Two firsts in international crew were racked up with the flights of payload specialists Pratiwi Sudarmono, whose mission to support the deployment of Palapa B-3 aboard STS-61-H made her the first non-Soviet, non-American woman in space, and Nigel Wood, who achieved the honor of the first British astronaut in space overseeing the deployment of the Skynet 4 military communications satellite [1]. Other firsts were carried out to more immediate public notice. Millions of schoolchildren watched live broadcasts of the launch and mission of Christa McAuliffe, which aired on cable news. The next month, Columbia went to space for a look at Halley’s Comet, another mission whose ease of explanation carried it well into public knowledge. Uncrewed exploration allowed the Space Shuttle to again insert itself into headlines with the rapid-fire launch of two large science missions during the 1986 Jupiter launch window. In a demonstration of the quick-turn capabilities of the crews of Kennedy Space Center, the orbiter Atlantis launched carrying the space probe Galileo aboard STS-61-G on May 23rd, within 24 hours of the landing of Challenger after it in turn had carried the Ulysses probe aboard STS-61-F. It seemed every flight brought leaping advances, not just in the ability of even ordinary civilians and scientists to fly into space, but also in dispatching the next generation of exploratory probes through the Solar System. In this, the Shuttle’s crowning achievement of 1986 was opening eyes to the entire universe with the launch and “first light” of the Hubble Space Telescope on STS-61-J.






While these successes were dramatic, the launch of Hubble and the Shuttle-Centaur missions were emblematic of deeper rooted issues both in the Shuttle program and throughout NASA at large. While the capabilities of the Shuttle-Centaur were critical to the successful execution of the Galileo and Ulysses launches, the Johnson and Glenn teams responsible for Shuttle and Centaur respectively had barely come together to carry the project to the pad in time for the critical Jupiter launch window. The two teams had struggled over technical definitions of Centaur as either a “payload element” or a core element of the Space Transportation System. This subtle distinction affected whether control remained with Glenn and the existing Centaur team who were eager to put their skills to work to support the Jupiter probe missions or to Johnson, who were skeptical about the safety of Glenn’s plans and protective of their control of the Space Shuttle program. The two teams eventually resolved enough differences of opinion to establish a working relationship, but the astronauts aboard the flights using Centaur had half-seriously referred to them as “Death Star” missions [2]. The presence of tons of explosive cryogenic propellants inside the Shuttle’s payload bay had weighed on crewmember’s minds, as had the 106% power demanded from the three SSMEs. Reassurances that the risk of the Centaur tankage was a minimal addition to the thousands of tons of equally explosive propellants in the External Tank, or the tons of both explosive and corrosive toxins in the RCS and OMS pods spread around the vehicle, were not particularly effective.

Hubble, for its part, had run into continual issues during development, leading to its launch slipping four years from 1982. The most serious of these was a major flaw found in its original Perkin-Elmer mirror when cross-tested by Kodak as a sop for the cancellation of Kodak’s backup mirror project in 1981. Kodak had quickly found their instruments indicated a problem with the Perkin-Elmer mirror’s shape. Perkin-Elmer, in answer, blamed Kodak’s test instruments, saying it was in effect a “sore loser” trying to cast doubt on the solution of the contract winner. A minor scandal had erupted with the two companies sniping at each other in technical conferences while NASA worked to determine which set of testing instruments was correct. The result after weeks of frantic work by NASA was Perkin-Elmer’s carefully phrased announcement in late 1981 that they had found and corrected an issue in their mirror testing system, but that the telescope would be ready in spite of this for a 1986 launch--a two year slip from the 1984 date which had been targeted only months before. Kodak’s reaction to the statement that their backup mirror’s development was still to be cancelled to “ensure margin for correction of outstanding problems with the primary mirror” were unprintable. The eventual success of Hubble’s debut saw the beautiful images the new telescope revealed make headlines in popular press even as the astronomical community eagerly devoured its early returns. It was enough to cover many sins by the program on its way to flight in the minds of some at NASA Headquarters and in Congressional offices, but the near-failures along the way (like the debates surrounding the safety on Shuttle-Centaur) still lurked in the concerns of those at NASA’s field centers who had been responsible for working past them day-to-day.

Such growing concerns of small issues being papered over in the name of “go fever” were lurking across all of NASA’s programs, including on Space Station Enterprise preparations, as normalization of deviance raced to new heights. The Shuttle had flown ten times in 1986, and yet there were still milestones to clear. As the year raced towards its conclusion, NASA was still aiming to achieve more than one flight in a month. September would be critical to this goal, as NASA aimed for three launches, a campaign that would use each available Shuttle launch pad once: the full set of LC-39A, LC-39B, and Vandenberg’s SLC-6. The end result would be NASA for the first time having two Shuttles in orbit at once. In early September, Columbia launched a DOD mission from Florida (STS-61-N), the secret payload being the first of the SDS-2 military communications satellites. On September 27, only a few days after Columbia’s landing, Challenger launched on STS-61-I carrying the program’s first Indian satellite, INSAT-2, with a plan to retrieve the Long Duration Exposure Facility orbital laboratory satellite. The trio was completed with Discovery’s STS-62-B launch on Sept 29. For the first time, two orbiters were in space together, as the Shuttle program celebrated the twelfth flight of the year, executed in just nine months. However, the failures of program management and normalization of deviance were about to come home to roost. The challenges of supporting two Shuttles at the same time, launching from two coasts within days of each other, pushed NASA’s flight support teams to their limits. Low-priority reviews were abbreviated given the rapid turnarounds and short durations of the missions and the challenges of more critical support of the crew activities on orbit like the deployment of the Ford-built Indian communications satellite, then the maneuvering of Challenger to rendezvous with and retrieve the LDEF. The five day flight was packed and only on Challenger’s final day in space was review of the Challenger ascent imagery completed.

Only with the final report on the STS-61-I launch issued and reviewed was the flight support team belatedly able to begin the detailed ascent imagery analysis for STS-62-B on October 2nd. With just days to go before the planned completion of Discovery’s classified polar mission, the team at Johnson dug into the second set of data gathered from the Vandenberg recorder systems. These were slightly different from the data sets and camera positions they were used to evaluating from Cape Canaveral. Moreover, Vandenberg’s weather proved as much of an impediment as it had been to tracking uncrewed launches. Fog and clouds had lurked on launch day, and made interpreting imagery of the ascent for any off nominal performance or debris more of a challenge than it might otherwise have been. Two days of frantic labor by an already overworked team ensued, including several engineers working straight through the night. They examined shadows in individual frames and the smallest blips on radar to do the usual evaluation that the Shuttle’s ascent had shed no debris or otherwise had a result which might pose a risk to the orbiter. However, tired eyes and 48-hour days were the final critical normalized deviations which robbed Discovery’s crew of their chance to survive. Lost in the clouds and fighting against time, the Johnson engineers didn’t grasp the true size of a chunk of foam shed from the forward bipod, and could only partially model the risks of ET foam and other debris they could spot in the imagery. Their report was inconclusive, but phrased poorly gave false confidence: “Potential impacts identified in data from launch. Indications are some potential risk, but previous data sets indicate models for foam penetration are conservative.” After discussions, the flight directors took this as a clean bill of health. Discovery made her retro burn on October 4th, headed back to Vandenberg. Nothing could have been further from the truth. In fact, the foam which impacted Discovery was more than 600 times larger than any previously modeled, a factor so far beyond reasonable that any conservatism in the model was moot. During descent, the tiles which had been damaged by the impact failed. Scorching plasma penetrated into the primary structure, and despite the best efforts of the orbiter’s commander at the stick, the results were almost foreordained. NORAD radar, following Discovery’s descent, tracked anomalous returns and loss of signal as the orbiter broke up over British Columbia’s Purcell Wilderness. Neither the orbiter nor any of her crew would survive.

[1] From @nixonshead : “This would probably be a Skynet 4 satellite. IOTL Skynet 4B was the first of the series launched, in 1988, but that was a delay due to the need to switch from shuttle to expendable launchers, so 4A would likely be first ITTL. Probably no-one cares, but my first job out of Uni was on Skynet 5, so I have a soft spot for the series :)

[2] For more on this debate in real history, check out the fantastic book “Taming Liquid Hydrogen,” particularly Chapter 6 ‘Centaur Reborn’ and Chapter 7 ‘Eclipsed by Tragedy’.

[NOTE]: In OTL, one of the two Centaur G' units is on display outside of NASA Glenn in Ohio (The other stage was converted to the Centaur T standard, and used to launch Cassini to Saturn):
 
So it was foam in the end? Well it was always more likely, Challenger was bad luck with a flaw that wasn't likely to strike except at very low temps but given how often the foam problem had almost happened before it was inevitable. Role any pair of dice 113 time's and snake eyes was always coming up sooner or later, here its sooner.

Lets hope a stand down and the resultant review and changes give Thiokol time to make the OTL SRB upgrades and ensure an alt Challenger can't happen this time.
 
Nice update. On the maiden VAFB flight? Ouch. The USAF will be pissed at losing their hardware and astronauts.

I’d wondered where the Centaur at the US Space and Rocket Center had gone—it used to be on display next to Pathfinder.
 
While these successes were dramatic, the launch of Hubble and the Shuttle-Centaur missions were emblematic of deeper rooted issues both in the Shuttle program and throughout NASA at large. While the capabilities of the Shuttle-Centaur were critical to the successful execution of the Galileo and Ulysses launches, the Johnson and Glenn teams responsible for Shuttle and Centaur respectively had barely come together to carry the project to the pad in time for the critical Jupiter launch window. The two teams had struggled over technical definitions of Centaur as either a “payload element” or a core element of the Space Transportation System. This subtle distinction affected whether control remained with Glenn and the existing Centaur team who were eager to put their skills to work to support the Jupiter probe missions or to Johnson, who were skeptical about the safety of Glenn’s plans and protective of their control of the Space Shuttle program. The two teams eventually resolved enough differences of opinion to establish a working relationship, but the astronauts aboard the flights using Centaur had half-seriously referred to them as “Death Star” missions [2]. The presence of tons of explosive cryogenic propellants inside the Shuttle’s payload bay had weighed on crewmember’s minds, as had the 106% power demanded from the three SSMEs. Reassurances that the risk of the Centaur tankage was a minimal addition to the thousands of tons of equally explosive propellants in the External Tank, or the tons of both explosive and corrosive toxins in the RCS and OMS pods spread around the vehicle, were not particularly effective.

It's interesting to note that it was John Young who coined the term "Death Star." And it wasn't a joke.

Ars Technica had an interesting look back at Shuttle-Centaur a few years back. AmericaSpace also did one a few years before that. Hair-raising stuff, even if it did not get the chance to destroy a shuttle in our timeline, or this one.

(P.S. I thought Shuttle-Centaur missions required the SSME's to fire at 109% thrust, not 106%? Or is this a timeline butterfly?)
 
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the orbiter broke up over British Columbia’s Purcell Wilderness
Inevitable and probably unavoidable. On the plus side the are going to become aware of the foam risk considerably sooner than OTL meaning instead of winding down the program they are probably going to try and fix it. Whether it's possible to design an upgrade program that takes makes the Shuttle reasonably (1 in 1000) safe is another question. Another issue is that this disaster occurred during an exception period from a program management perspective, this probably kills the idea of having multiple missions going on simultaneously dead for ever and will also force a reduced tempo to allow sufficient ground support. But because the situation on the ground was so exceptional you might not have any other reforms and NASA desperately needs more reforms at this point.
 
On the plus side the are going to become aware of the foam risk considerably sooner than OTL meaning instead of winding down the program they are probably going to try and fix it. Whether it's possible to design an upgrade program that takes makes the Shuttle reasonably (1 in 1000) safe is another question.

The problem is, the foam strike issue is a lot harder (and much more expensive) problem to really *solve* - as opposed to "modestly mitigate and plan around" (what happened in OTL in 2005-2011) than the SRB o-rings were. And NASA is going to figure that out pretty quickly.
 
The problem is, the foam strike issue is a lot harder (and much more expensive) problem to really *solve* - as opposed to "modestly mitigate and plan around" (what happened in OTL in 2005-2011) than the SRB o-rings were. And NASA is going to figure that out pretty quickly.

That's my point. You basically have to either replace the foam with something that won't fall off or replace the tiles with something which won't be damaged by foam strikes. If you were willing to spend the money you can come up with a foam that's less likely to fall off and tiles that are less fragile but I'm not sure that will get you to a 1 in 1000 safety rate. The real problem is that the Shuttle is a fundamentally bad design driven by a combination of extremely ambitious goals and inadequate funding leading to short cuts.
 
Nice update. On the maiden VAFB flight? Ouch. The USAF will be pissed at losing their hardware and astronauts.
STS-62-B is actually the second Vandenberg flight. STS-62-A doesn't get a specific mention in the text, but was scheduled for July, 1986 and took place around then ITTL.
 
Can’t any of you guys write a shuttle failure where some of the crew survive? Sheesh.
It's really hard to kill an orbiter in a way that anyone survives. There's a very fine line in its operating environment between a failure that miraculously everyone survives and one where regrettably everyone dies.
 
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