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Author Topic:   STS-400? 100 missions per space shuttle orbiter
Fezman92
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posted 06-02-2011 03:42 PM     Click Here to See the Profile for Fezman92   Click Here to Email Fezman92     Edit/Delete Message   Reply w/Quote
When the shuttles were built they were designed to fly for 100 missions. If Columbia had not been lost and the shuttle program not been canceled, would have there been a STS-400 (four shuttles, each flying 100 missions)?

Hart Sastrowardoyo
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posted 06-02-2011 04:17 PM     Click Here to See the Profile for Hart Sastrowardoyo   Click Here to Email Hart Sastrowardoyo     Edit/Delete Message   Reply w/Quote
I've always wondered how the 100 mission standard was created. Was it based on 100 missions of four days each, which seemed to be the average planned length of a satellite deployment mission? Was it based on say, the airframe certified for so many hours, then dividing that number by the number of hours planned in a typical mission?

Anywho, the furthest out I've seen is a STS-91-T. STS-51-L was the 33rd mission (eight of which were canceled or postponed) and 61E would have been STS-34, so in three years to STS-91-T we would have gotten to STS-90 or 100. If the 20 flights a year for the three KSC orbiters combined could be sustained, it would take another 15 years post 1989 to reach STS-400.

The Vandenberg flights had their own numbering system, starting with STS-1V. Ironic that Discovery, now the fleet leader, had only been scheduled for four flights per year (the same sked with STS-91-T lists Vandenberg flights only up to STS-12V.)

issman1
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posted 06-02-2011 04:25 PM     Click Here to See the Profile for issman1     Edit/Delete Message   Reply w/Quote
I recall when Daniel Goldin, as Administrator of NASA in the late 1990s, spoke confidently about shuttle missions until 2020.

It could have happened but the Columbia disaster was the beginning of the end. Looking with hindsight (as everyone does), perhaps the shuttle's career ended prematurely. Only time will tell.

Other than building, maintaining and supplying the International Space Station there's not much requirement for its versatility. Servicing the Hubble Space Telescope was also exceptional, but the last time a shuttle mission actually repaired/rescued a commercial satellite was STS-49 in May 1992. So it was neither cost-effective nor lived up to its original billing, as satellite deployments shifted to expendable vehicles after Challenger, further reducing those potential number of missions.

It's easy to get overly sentimental about the past three decades - am I the only one who followed those round-the-clock Spacelab missions religiously? And while I empathise with all those within NASA and its contractors who lost their livelihoods as a consequence, human spaceflight has to be about more than endless laps around the Earth. Though it makes perfect sense to do so on board a space station.

Ultimately, that's a management and political failing more than engineering. The shuttle could have continued to carry more Spacelabs if there was no ISS and may be a retrievable satellite every now-and-then, like SPAS or SPARTAN, till STS-200 or 300 or 400.

There was no shortage either in the number of flight crews to fly so many missions because NASA recruited one its largest astronaut classes in 1996. That's because ISS and shuttle were tied together and thus needed each other, until now.

Hart Sastrowardoyo
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posted 06-02-2011 04:41 PM     Click Here to See the Profile for Hart Sastrowardoyo   Click Here to Email Hart Sastrowardoyo     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by issman1:
So it was neither cost-effective nor lived up to its original billing, as satellite deployments shifted to expendable vehicles after Challenger.
Shuttle was also billed as a vehicle where, prior to deployment, a satellite could be checked out and if there was trouble, could be returned back to earth. I seem to recall a graphic which had the number of failed satellites launched on expendable rockets, a number which supposedly could be lessened or eliminated with shuttle.

Expanding that role to bringing back or fixing satellites that failed, how many satellites did shuttle actually save, compared to the number of satellites that failed (whether due to satellite failure itself or launcher failure)?

Byeman
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posted 06-02-2011 05:03 PM     Click Here to See the Profile for Byeman   Click Here to Email Byeman     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Hart Sastrowardoyo:
Expanding that role to bringing back or fixing satellites that failed, how many satellites did shuttle actually save, compared to the number of satellites that failed (whether due to satellite failure itself or launcher failure)?
None, because that capability was rarely used. Most spacecraft were quiescent during launch and on orbit and did not "awakeup" until separation from there upperstages. The Syncom IV that failed on STS 51-D is a perfect example. The Syncom IV was dead the whole time of the mission and was designed to activate upon deployment.

Typical spacecraft launches on ELVs have umbilicals that provide power, data and commanding prelaunch. The umbilicals connect to EGSE in the base of the pad which through various communication lines are linked to the spacecraft launch control center located at CCAFS, KSC or Astrotech.

Once liftoff occurs, the connection is severed and the spacecraft is quiet until separation when it wakes up and tries to communicate with its ground sites. On rare occasions, the launch vehicle can provide some discretes (commands), interleaved data (2k rate) and power (batteries added for the spacecraft which reduces the lift capability).

The spacecraft for the shuttle followed this trend and it did not have the resources during launch (on orbit was different) to provide to the spacecraft.

BNorton
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posted 06-02-2011 08:12 PM     Click Here to See the Profile for BNorton   Click Here to Email BNorton     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Hart Sastrowardoyo:
I've always wondered how the 100 mission standard was created.

It was a simple matter of structural fatigue analysis. The loads on the spacecraft during launch and entry, and the structure design, essentially established the 100 flight limit. If an orbiter had made 100 cycles, I would guess that it probably would have been inspected and potentially re-certified for additional flights/cycles. The same is true of all aircraft: they are operated in the US for a fixed number of cycles (take off and landing). For example, many commercial domestic aircraft are "retired" after about 60,000 cycles.

328KF
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posted 06-02-2011 09:12 PM     Click Here to See the Profile for 328KF   Click Here to Email 328KF     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by issman1:
am I the only one who followed those round-the-clock Spacelab missions religiously?
Nope. I used to watch CNN's coverage of STS-9 for many more hours than I'd care to admit. That was back when I thought cable TV was named such because of the long cable from the TV to the box with the rotary channel selector

We didn't have our first VHS tape recorder yet (I think my Dad was still on the fence between that and BetaMax) so I used to record the audio on my cassette recorder right from the TV speaker...I still have the tapes!

Sorry for the flashback...

Hart Sastrowardoyo
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posted 06-02-2011 10:40 PM     Click Here to See the Profile for Hart Sastrowardoyo   Click Here to Email Hart Sastrowardoyo     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by BNorton:
It was a simple matter of structural fatigue analysis. The loads on the spacecraft during launch and entry, and the structure design, essentially established the 100 flight limit.

Based on which spacecraft or in general? Don't have the reference (it may be Dennis Jenkins' book), but I recall reading that Enterprise was placarded not to exceed a certain load amount, Columbia was certified for a higher amount, and that subsequent orbiters for an even higher load factor (and Columbia was eventually certified for that amount as well.)

OV-105
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posted 06-03-2011 01:36 AM     Click Here to See the Profile for OV-105   Click Here to Email OV-105     Edit/Delete Message   Reply w/Quote
After Challenger it was always said that if another Shuttle was lost it would kill the program. It did. They had to finish the ISS first since everything needed the Shuttle to orbit. The Shuttle was just starting to hit its mark by flying up to ISS with more payload than anything else. It also did something that nothing else could do, bring a large payload back from the ISS. It is sad that we have never been able to run to programs at once for the long term.

Tykeanaut
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posted 06-03-2011 03:11 AM     Click Here to See the Profile for Tykeanaut   Click Here to Email Tykeanaut     Edit/Delete Message   Reply w/Quote
Sadly the shuttle's capabilities are now redundant. All that is currently required is a simpler crewed vehicle for visiting and returning to the ISS.

Henry Heatherbank
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posted 06-03-2011 04:29 AM     Click Here to See the Profile for Henry Heatherbank     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Hart Sastrowardoyo:
The Vandenberg flights had their own numbering system, starting with STS-1V. Ironic that Discovery, now the fleet leader, had only been scheduled for four flights per year (the same sked with STS-91-T lists Vandenberg flights only up to STS-12V.)
Hart, I always thought the Vandenberg flight designations were going to follow the designations of the east coast flights post STS-9, so the the first west coast mission in late 1986 would be 62-A/Discovery (or course,commanded by Bob Crippen), and then 62-B etc. I have never heard of the STS-1V etc designations. Can you tell us some more about that?

Also, not to deviate from this thread, but at the time of the 51-L destruction, were there crews planned for the second and subsequent VOFT flights, post 62-A? Presumably Discovery was going to be the dedicated "west coast Orbiter".

issman1
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posted 06-03-2011 06:25 AM     Click Here to See the Profile for issman1     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by 328KF:
I used to watch CNN's coverage of STS-9 for many more hours than I'd care to admit. I used to record the audio on my cassette recorder right from the TV speaker... I still have the tapes!
I mainly followed the shuttle flights post-Challenger on radio, as well as watching news reports on terrestrial British channels then satellite TV news broadcasters like Sky News, CNN International and Deutsche Welle English Language. Newspapers were also compulsory for me the day after a shuttle launch or landing.

Radio was the best form until discovering the internet in the mid-90s, especially as I was able to tune into American Forces Network Europe on AM and also the Voice Of America on SW.

As a result I was able to hear good, realtime coverage from the space/science correspondents of AP, CBS, NPR as well as VOA. Rob Navias, who is now a NASA PAO, was really knowledgeable and I'm not surprised where he ended up.

garymilgrom
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posted 06-03-2011 06:47 AM     Click Here to See the Profile for garymilgrom   Click Here to Email garymilgrom     Edit/Delete Message   Reply w/Quote
I think we're missing an important point. The OP asked about the engineering behind the 100 mission design, but let's examine the management behind this statistic too. When built the STS was said to be capable of 50 launches per year so someone thought this country would need to be launching a Shuttle every week - why would we need that much capability?

issman1
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posted 06-03-2011 06:55 AM     Click Here to See the Profile for issman1     Edit/Delete Message   Reply w/Quote
Those in charge of NASA as Apollo was winding down may have been fearful that the entire US space programme was in jeopardy.

They went on the offensive, exaggerating and promising all things to all people. Yet, a flight rate of 50 per year seems so absurd I find it amazing the shuttle was ever approved.

garymilgrom
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posted 06-03-2011 07:33 AM     Click Here to See the Profile for garymilgrom   Click Here to Email garymilgrom     Edit/Delete Message   Reply w/Quote
My question put another way - does the United States launch 50 satellites a year? Does the entire world launch 50 satellites a year (or anything close to this number)? Maybe the planning rationale was to win all this business, but I don't know the actual launch rate. I guess we need to know how the launch rate has changed in the past 30 years too.

Robert Pearlman
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posted 06-03-2011 08:30 AM     Click Here to See the Profile for Robert Pearlman   Click Here to Email Robert Pearlman     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by garymilgrom:
Does the entire world launch 50 satellites a year (or anything close to this number)?
According to a quick count on Jonathan's Space Report Launch Log, in 2010 the world launched 60 times to put satellites into orbit, with each booster carrying one or more satellites (for the purposes of this discussion, I did not include space shuttle, Progress, Soyuz or Dragon launches but did include X-37B).

Of those 60 launches, 10 were by the United States (four Atlas, four Delta, two Minotaur).

According to Euroconsult, a consulting firm specializing in satellite communications, the previous decade saw an average of 77 satellite launches per year.

Hart Sastrowardoyo
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posted 06-03-2011 08:37 AM     Click Here to See the Profile for Hart Sastrowardoyo   Click Here to Email Hart Sastrowardoyo     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Henry Heatherbank:
I have never heard of the STS-1V etc designations. Can you tell us some more about that?
All shuttle flights had two designations: a numerical one and an alphanumeric (the 61-C or 1-V) which designated the payload. For example, until 51-E was canceled, 51-D was tasked with the LDEF retrieval, and that was true regardless of whether or not 51-D was a crew led by Shaw and O'Connor, or Brandenstein and Creighton, or Bobko and Williams, all of whom were named as the 51D crew at one point or another.

(The designations are not to be further confused with missions STS-26R through 33R, which NASA used for the first eight missions post-Challenger. Even though there were 25 flights, there had been 33 scheduled missions. The "R" signified reflight, although it was actually a reuse of the number. STS-94 was originally known as STS-83R in some documentation.)

Bobko, according to Who's Who, was rumored to be tapped to fly the third Vandenberg mission. No crews had been formally named, aside from Kathy Roberts for 62-B.

Ironically, most of the crew for 62-A - Gardner, Ross and Mullane - wound up flying some of 62-B's payload.

Getting back to the topic at hand, it was believed that not only would the US be using shuttle, but so would international customers - hence the flying of foreign payload specialists in order to court their business.

Whether there was enough business to fly almost every other week (20 launches a year) is debatable. As time has seen, MDD's EOM was supplanted by other, cheaper methods. And countries like Indonesia, which launched satellites on shuttle and came close to having the first female, Muslim astronaut, have their own concerns other than a space program to deal with.

Engineering-wise, I think the shuttle could fly 12 to 14 missions a year. 1985 almost saw 10, and that was with three orbiters for the most part.

But the problem in flying the shuttle is that its utility is also what's limiting it. Every flight is mission specific.

Say you want to use shuttle just for launching comsats in order to make money. Do you use PAM-A, D, or D2? IUS or Centaur? One, two, or three satellites, or do you claim national security, stack four in an orbiter and hope you don't have to do an RTLS? And if you fly one or two satellites, what else do you carry in the payload bay?

Unfortunately, despite early hopes and renderings to that effect, changing payloads on shuttle is not as simple. It's not like offloading passengers from an airplane and loading new ones. It's more like the 747QC, where the plane is stripped and reconfigured.

kr4mula
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posted 06-03-2011 10:59 AM     Click Here to See the Profile for kr4mula   Click Here to Email kr4mula     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by garymilgrom:
Maybe the planning rationale was to win all this business, but I don't know the actual launch rate.
Speaking with various shuttle managers from that time, I got the impression that everyone had a "build it and they will come" mentality.

The world only launches a handful a satellites each year because it is prohibitively expensive. NASA's logic was that if they could lower the launch cost to $100/lb (or was it $10/lb?), everyone would be building satellites because they could afford to send them to space, thus the customer base would get huge and the shuttle would fly twice a week.

Obviously that didn't work out because the shuttle we ended up with wasn't what they envisioned at the time and couldn't come anywhere near that $/lb target (a case of trading lower development costs for higher operating costs, instead of going the other way around, in my opinion).

Cozmosis22
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posted 06-03-2011 10:19 PM     Click Here to See the Profile for Cozmosis22     Edit/Delete Message   Reply w/Quote
When NASA announced it's "Citizen in Space" project back in about 1984 some people thought maybe it was the beginning of a new era for space exploration. Unfortunately we were wrong. NASA started with a "Teacher in Space" and were taking applications for a "Journalist in Space", the next phase, when the Challenger accident put a halt to the entire project.

People in various citizen advocacy groups like the L5 Society and National Space Society had big hopes of NASA putting rows of passenger seats in glass-topped capsules that would fill a shuttle cargo bay. Limited space travel would finally become "affordable".

Of course, nothing like that ever came about and was probably never seriously discussed beyond water cooler conversations in places like Lockheed, Rockwell, and Martin Marietta.

Considering the sizable cargo capacity of the orbiters, one might venture to guess that overall... the shuttles flew half empty. Indeed, few missions other than the HST completely filled the cargo bay...

Jay Chladek
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posted 06-08-2011 12:44 AM     Click Here to See the Profile for Jay Chladek   Click Here to Email Jay Chladek     Edit/Delete Message   Reply w/Quote
You can't necessarily go by "half empty" though as the weight and mass of the payload tends to be more critical than the physical size of it (as is the orbit where it is going to, which can affect how much a shuttle can carry uphill). That being said, indeed there were weight concerns somewhat early on as with an RTLS and a heavy payload, stopping a shuttle coming in for landing became problematic. That was until NASA finally installed the drag chute system (something which was planned for early on, but never added until after Challenger).

Even with a heavy weight payload such as Spacelab, when the pressurized lab module was flown, it still had a long transfer tunnel because the thing had to be loaded with center of gravity issues in mind. Ultimately what killed the Spacelab pressurized module was the creation of the Spacehab system as that module didn't have the same center of gravity concerns. So a pressurized Spacehab module could be loaded towards the front of the bay regardless of what was installed behind it.

OV-105
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posted 06-08-2011 11:48 AM     Click Here to See the Profile for OV-105   Click Here to Email OV-105     Edit/Delete Message   Reply w/Quote
Spacehab did not kill Spacelab. They both had different jobs. ISS took care of Spacelab, but then again that was the plan all along. There were some Spacehab flights where it was mid cargobay.

Cozmosis22
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posted 06-18-2011 11:14 PM     Click Here to See the Profile for Cozmosis22     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Jay Chladek:
You can't necessarily go by "half empty" though as the weight and mass of the payload tends to be more critical than the physical size of it...
OK, half utilized by weight OR by size. Finally went up to the full 7-person crews but the payload bay... not so full.

Hart Sastrowardoyo
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posted 06-19-2011 09:41 AM     Click Here to See the Profile for Hart Sastrowardoyo   Click Here to Email Hart Sastrowardoyo     Edit/Delete Message   Reply w/Quote
Except you can't have full seven-person crews _and_ a full payload bay. Look at STS-93. I'm recalling this from memory, so forgive me if I have this wrong, but I remember seeing somewhere that if the crew size was more than five astronauts, one had to subtract a certain amount of weight from payload.

Interestingly enough, I found my Rockwell model pamphlet, issued after the ALT flights. In it, it states that the shuttle will usually fly a crew of three (CDR, PLT and MS) and up to four PSs....

Jay Chladek
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posted 06-20-2011 12:09 AM     Click Here to See the Profile for Jay Chladek   Click Here to Email Jay Chladek     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Hart Sastrowardoyo:
Look at STS-93.
The thing about STS-93 though is they were also flying it with the heaviest weight orbiter in the fleet, Columbia. Of course the main reason why Columbia was used had to do with it still having an internal airlock installed on the mid-deck, meaning the Chandra observatory could take up the whole payload bay.

If another shuttle not already configured for ISS flights had been available to fly Chandra, it probably would have been scheduled and likely would have had enough up-mass left over to take up a seven person crew (if there was a need for a seven person crew that is).

NASA of the pre-Challenger 1980s might have stuck on a couple payload specialists to fill out the seats if such a mission had come up.

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