I'm very concerned about the lack of determination that is currently evident in our space program. While the Columbia disaster did warrant a major investigation and corrective measures. After one more flight conducted with many improved safety measure including cameras that could record falling debris, a careful examination in space, and a recuse plan involving a transfer to the ISS if a serious launch damage was found we on another major hold. My view is that with 114 flights and two losses we have under 2% chance of a total loss. It seems to me that for a new frontier while tragic this is not unacceptable.
After all this is a new frontier and grave dangers are to be expected. Consider this risk with say early aviation or climbing the most dangerous mountains. It goes with the territory. It has recently been claimed that the shuttle is unacceptably risky because it doesn't have an escape system like a figher planes ejection seats or the escape towers on Apollo. But neither do commecial airliners. Are they too dangerous for ordinary people to fly? We have designed the ISS modules to be launched on the shuttle plus it could be used to repair the Hubble telescope.
My view is that we should continue to use the shuttle until a suitable replacement is ready.
Iīm agree,spaceflight is a risk but not higher than extreme sports activity,hill climing,bungi jumping etc.But a further lost of a space shuttle+crew is inaccepable. The Challenger disaster was caused by human failures(ignored warnings of launching crew and overhauling personnel) By Columbia itīs more complicated,because the main construction the heatshield system is to sensible and unreliable.Caused by damage by center tank insulation froam itīs /would be the best to redesign the tankīs insulation to a rocket stage similar concept.Maybe an additional engine bundle hydrogen-oxigen engines could be installed to enhence payload capacity. An other way to prevent damage by loosing insulation could be a layer of wire mesh. This could be done in a very short time and the additional weight is acceptable.
I tend to agree with John: if we want to see advances in space exploration, better to take the bull by the horns and go on! After the Columbia accident, I have the feeling that too many safety precautions are being taken. It results a little risk mitigation which does not appear to be worth the effort (the risk is there anyhow!). For example, I think that in future flights to ISS, the astronauts will see almost one whole day (!) of their shedule dedicated to examinating the underside of the shuttle with a robot arm to discover eventual damage.
Obviously any "quick fix" that could be applied to the existing fleet of shuttles (3 vehicles) is good. I've sure that given the political pressures they have considered all that. My point is that the falling ice problem must have been there every for the last 25 years. After 114 flights we have one loss. That's less than 1%. I doubt that you can really design a heatshield system for the shuttle that would take a hit like the one in Columbia and not have serious damage. The odds are that for the remaining missions it won't happen if it does will detect it by inspection and transfer the crew to the ISS an return by Soyuz or another shuttle mission.
My bet is that if another shuttle is lost it will be from a third cause yet unknown rather than a repeat of the Challenger or Columbia disasters. What really concerns me is this move to the CEV. That basically saying the last 35 years of manned space policy was mistake! We basically could have done all of this with the Apollo back in the 1970s. I'd like to see the development of scramjets and SSTO shuttle with no external fuel tank.
There are many advantages and disadvantages of the space shuttle. Obviously one advantage is that the crew goes up with the cargo. No in orbit reundesvou is needed to achieve mission success. Everything is more or less right there. However, this also happens to be one of the biggest disadvantages from the standpoint of safety.
Most people tend to think that the new CEV concept is a great step backward--but let's look at this thing from the point of view of an astronaut.
The space shuttle, as much of a cadillac machine that it is, is incredibly fragile. it must operate in the extremes environments of launch, space ops, and then reentry followed by landing. O.K., any manned space craft must do the same. So what?
Well, if anything goes wrong (and there are about a million things that can!) because of the nature of the spaceshuttle, there is NO TIME to deal with it. When something catastrophic happens, by the time the astronauts understand the something has gone wrong, because of the speeds and energies involved the whole thing is a done deal. Their dead--and if they're still conscious--they just don't know it yet. There isn't time to eject, and nowhere to eject to if the vehicle is moving any faster than Mach 2.5. The crew cabin, as durable of a piece of hardware that it is, cannot survive reentry by itself, and cannot protect the crew to a safe landing in the event of a launch abort, even though in the case of the Challenger explosion, the cabin remained intact until ocean impact two minutes later.
So what do we do?
We make the cabin smaller. A smaller vehicle is stronger per unit volume than a larger one. Why? Because the intrinsic curvature at the surface is greater so it is easier to achieve a robust mechanical design that is stronger per unit weight than a large cabin. The Apollo capsules were conical with a spherical sector rear bulkhead sporting the reentry heat shield. The Russian Soyuz uses a small spherical reentry capsule. The CEV achieves a smaller cabin size (about one-third larger than the Apollo Command Module) and at the same time achieves the important safety goal of giving the astronauts an all mode, all attitude, all altitude mission abort option. This is something that the space shuttle has never had and will never have.
True the shuttle is a beautiful flying machine--any pilot worth their salt would probably love to fly one--but the practicalities suggest a smaller, simpler vehicle. The CEV may deliver this. By seperating the crew transportation from cargo transportation the overall safety is greatly incresed for the crew.
I was somewhat dimayed at the loss of the X-38 program which was to have developed a mini-shuttle. This could have been ideal for a assured crew return vehicle for the ISS and for shuttling up small cargoes/crews to and back from the ISS. I guess the CEV will pick up the slack here.
Most people tend to think that the new CEV concept is a great step backward--but let's look at this thing from the point of view of an astronaut.
I don't see anything in CEV that could have been done 30 years ago! Most earlier than that. This thing is basically Apollo Redux. Its greatest merit is that its cheaper than a true second generation shuttle. Also, it can be used for a basic return to the Moon mission which a shuttle can't. Given the current political realities I for CEV since being against it is equivant to ending U.S. manned space.
However, I see no reason not to fully utilize the remaining shuttle capabilities we have. Certainly there are mission like simply crewing the ISS or a shuttle rescue that the CEV would be great for doing. As far as safety goes it is true that a CEV crew would very likely survive a propulsion system failure and is unlikely to breakup on re-entry. However, I don't see spaceflight as an occupation for those driven primarily by safety concerns. Perhaps that is what is wrong with the space program. And don't forget that four people have died in capsules and three more nearly did (Apollo 13). So capsules aren't truely safe either.
Partly this attitute probably comes from the background the astronaut corps many of whom are ex-fighter pilots. Modern fighters are have ejection seats that can get them out of the plane under a wide variety of conditions. Many of the same failure mode if occured in a passanger or cargo plane would result in the deaths of all on board. So are we giving up on commercial flights?
If we were to develop a second generation shuttle many changes could be made to relieve some of the problems what we are discussing. Designs that won't have a tank above the orbiter and might have a crew compartment that is sort like the X-38 that could seperate (via explosive cords) to serve as an escape module. I think that it was particularly lame to have not funded the X-33. It also would have provided the first flight of aerospike engines to give us some improvement on specific impluse in atmosphere to space.
One of the key advantages of the CEV is that it has eliminated all risk associated with launch. The capsule is on top of the rocket stack, and not beside. Vibrations from acceleration cannot damage the CEV, and if anything below is in trouble, the CEV capsule has an escape tower. (Something the shuttle cannot boast or accomplish)
I do hate to see an old bird die, though. Maybe they can stay in use as OTVs, or permanent expansions to the International Space Station. More than likely, they'll end up in the Smithsonian if they aren't cannibalized.
Both John and Lord Flasheart make good observations concerning the shuttle. I believe it makes a lot of sense to use a sensible amount of shuttle hardware for a next generation vehicle. I'm not a real big fan of the Shuttle-C with an SSME powered expendible cargo can--this replaces the shuttle payload bay/OMS package with something that gets chucked every time. These are the most expensive components of the shuttle orbiter stack...
I like the inline system better--such as the Magnum booster which puts a payload shroud atop a modified ET, The ET becomes a core booster vehicle with a cluster of 4 SSME's at the bottom (although I like the idea of using the RS-68's used in the Delta IV Heavy.) Years ago I studied a concept vehicle that used a reusable propulsion module containing 8 SSME's and the equivalent of 4 OMS pods, surrounded by 4 four-segments SRB's. Such a configuration could have easily lofted 220,000 Kg into low earth orbit. recently More recently I've toyed with the idea of a vehicle that uses a more modified ET with a stretched liquid oxygen tank, and slightly stretched liquid hydrogen tank. The vehicle would be surrounded by four (or possibly as many as 8) reusable liquid propellant boosters sporting Russian RD-180's, and containing onboard RP-1 tanks. Liquid oxygen would be piped from the ET. The simplified booster tankage should easily allow for smaller 'fly back' booster technologies to be implemented and installing General Electric F101-GE-102 Turbofan engines for flyback capability (the same engine used in the B-1 Bomber.). Such a huge launch vehicle should begin to approach 300,000 kg into low earth orbit.
Anyways, the point is that it makes sense to use the hardware and infrastructure that works. Eventually phasing out the orbiter does not necessarily mean the deathnell for US crewed space flight. However, I would agree it also makes sense to develop a full on replacement for the shuttle. I think that is emminantly feasible and will serve very well. The shuttle was a fantastic experment--and it demonstrated that reusable space craft are possible. Now its time to take what we've learned and build the next generation vehicle. So what if it costs $30 billion to develop. It's just not possible to be a world leader in technology on a Top Ramen and PB&J budget!
+ Development of a Commercial Crew/Cargo Project capable of transporting humans and cargo to the International Space Station. The orbital cargo and human transportation demonstrations are scheduled for 2008 and 2010, respectively;
<end quote>
....the t/Space concept, based on the success of the SpaceShipOne/ White Night combination, seems particularly attractive.
The problem about the Shuttle isn't just one of taking reasonable risks or not; it's that the vehicle is inherently unsafe and inefficient.
It's not a good thing to put the crew and cargo on the same vehicle. Maybe for a few extreme mission examples it's OK to fly an orbital workshop, but the Shuttle has always been an example of flyingt a 747 to Paris, and using it as a hotel on the tarmac while it's there. Not to mention throwint a lot of it away during the course of the use. A "Shuttle" is just that - a vehicle for shuttling back & forth. It's not to be used on-site.
Using it as it has been used is very expensive -too much so. For a cheap cargo launcher, or to lift big parts of a space station, you do not need a winged, re-usable, crewed plane. Each of these requirements drives the complexity and cost up, and the combination drives it through the stratosphere! for cargo, you need a BDB.
For crew, you need something small enough to mount escape rockets on it, and a cargo launcher is too big. Everything from zero-altitude / zero-airspeed, to hypersonic sub-orbital survivability is the necessity for a safe crew launcher. The STS Shuttle should never have been anything but a special purpose experimental ship.
You don't need to treat cargo the way you treat crew. You insure a cargo, but you pamper crew and provide every possible contingency for survival, and the STS Shuttle is the worst ever launcvh vehicle: It's the first and only crewed launch vehicle ever to have no crew eject/escape capability during launch! It's a horrendous oversight that we've gone on this long relying on it for all of our crew launch needs.
The easiest way to address the problem of the exhorbitant cost to get to space is to build the Shuttle-C for cargo. This has been known since the 1970s. The Shuttle plane is the most expensive part of the launch stack, and the first to go if you want a reliable cheap cargo lifter, or if you want an assuredly safe reliable cheap crew lifter.
No, the Shuttle should be grounded and the entire budget diverted to accelerating the CEV and something like ATK Thiokol's "Safe, Simnple, Soon" HLV development. The only thing we need the Shuttle for is the Hubble, and maybe a couple of EVA support missions to the ISS. All the other ISS payloads, the bulk of the lifting should be deferred until an Shuttle-C can be used.
"Much has been made over the report produced by the Columbia Accident Investigation Board (CAIB). I have since read newspaper articles that called the report "scathing." Hardly. Its polite recommendations probably had Shuttle managers who made poor decisions dancing down their office hallways with relief. Essentially, it gave them a pass by proclaiming "culture" made them do it...
I do not believe there is a NASA culture other than a willingness by its engineers to work their butts off to keep us in space. It might be said, however, that there is a Shuttle cult. It is practiced like a religion by space policy makers who simply cannot imagine an American space agency without the Shuttle. Well, I can and it is a space agency which can actually fly people and cargoes into orbit without everybody involved being terrified of imminent death and destruction every time the Shuttle lifts off the pad.
With some important reservations, the CAIB recommended to keep the Shuttles flying but with more inspections, more bureaucracy... and more money. But I think piling on more inspections and people and dollars won't make the Shuttle any safer... The truth is no amount of arm-waving and worrying about "culture" can fix a flawed design. Every engineer knows a design that tries to bypass the realities of physics, chemistry, and strengths of materials by applying complexity will fail eventually no matter how much attention is given to it.
(cont'd at link)
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
I have read Homer Hickam's op-ed piece, and I have to agree with him. Having met the man in person I can honestly say he is 'down to earth' and is intelligent enough to apply 'common sense' to engineering...
It's something that has always bothered me even as a kid--every launch vehicle before the shuttle had "escape" rockets atop a an all liquid fueld booster: Mecury sat atop the Redstone and then later the Atlas--escape rocket on top of the capsule; Gemini sat atop Titan II--escape rockets nestled underneath the capsule (which also served as the retro motors for deorbit--a genuine weight and cost savinf feature!); Apollo which had the big escape motors mounted on a tower above the Command Module--also on a liquid fueled booster stack. And then the Shuttle--no dedicated escape tower--nestled to the side and aft of an enourmous propellant tank and stuck between two 160 ft long pipe bombs! As beautiful of a launch as the STS gives--this is no justification for such an inherent safety oversight (not so much an oversight as a 'feature.')
True, I think the engineers at the time did the best they could considering the budget cuts, Congressional meddling and the Air Forces insistance on tossing big payloads in orbit (the KH-11 was still on the drawing boards at the time, but if one wants to know about what a KH-11 looks like, then simply look at another unclassified product of the same Lockheed spacecraft manufacturing plant: The Hubble Space Telescope is the modified, civillian version of the NRO's preeminant optical reconaissance satellite...)
Seperate the heavy cargos from the crews--send the crews up in smaller, safer Capsule Spacecraft, or small Space Plane, fixxed atop an all-liquid booster, and then send the bulkier cargo up inside a payload shroud atop another booster possibly using solid rocket motors for thrust-augmentation(although I personally like liquid fueled boosters myself.)
Safety is one of the things that still makes me cringe about the current SRB/CEV concept, because once that solid rocket motor is lit, you are along for the ride for next two and a half minutes of your life. Atleast a liquid fueled booster can be commanded to shut down its engines--allowing a much safer Abort/Escape route...
It doesn't seem to me that Homer Hickman's position differs that much from mine. I didn't say Shuttle forever...I said let it fly. I don't think we are gaining that much about freting about every possible falling piece of ice. That stats clearly show that there is slightly less than a 2% chance of loss in a shuttle mission. This is a dangerous business. So is flying combat sorties against an enemy or going on patrol in the infantry, etc.
The lack of an escape system certainly isn't one of the Shuttle's stronger points. However, as I have pointed out before this is also true of airliners, cargo aircraft, private planes, helicopters, etc. Escape systems should be considered on the replacement system. Hopefully they will be feasible but we need to press on with the Shuttle for now. Even with ejection seats we still have a significant number of fatalities in figher jets.
It is past time to be working on what comes after the Shuttle. This project should have been underway since at least 2000. What we have instead is a major return to the past with the CEV. Of course given the realities of the current situation I support the CEV (somewhat reluctantly) as the practical alternative is the end of manned U.S. spaceflight. It is useful to allow a return to return to the Moon and it would be very nice to have two means to access space so that if the primary one is out of commission all activity would not need to stop.
I would like to see more R&D on scramjets as a way to replace those troublesome SRBs. So far we have had some very subscale experimentation conducted over a period of years. It would seem that a more aggressive program might yield results. Even if the Shuttle engines reuseability has proven uneconomical, we need to develop reusable engine concepts to have economical spaceflight. I would hope that thirty years of progress might yield something better that glue-on tiles as heat shielding.
Interesting point from Googlenaut about the Gemini's escape rockets also being the de-orbit rockets: That's something that's come to make a lot of sense to me since I've been looking into this stuff. If you're escaping before orbit insertion, then you don't need the OMS/circularization/de-orbit delta-V, and if you've made it to orbit then any weight lifted off the pad in the form of escape rockets was wasted.
1.5 sec of 8G for an escape rocket, if throttleable, means ~2+km/sec of OMS delta-V. This is another thing that hybrids would be great for. Either burn it all at once getting away from the vehicle, or use it for the upper stage motors.
I was at the recent Mars Society 'Con when Scott Horowitz (an astronaut since gone to work for ATK Thiokol) gave a presentation on the "Safe Simple Soon" concepts before it hit the press or 'net. I raised the question of sending crews on the SRBs. Before Challenger, as long as the temperature was low, there wasn't a hint of a problem with them. After Challenger, with the mods made after that, there's not been a hint of a problem with them. Historically, solids have been the most robust and forgiving rockets around. Effectively no moving parts, only one thing matters: getting the pour down right, and then they're accurately predictable, every time. Liquids are complex and cantankerous at the best of times.
Also note that the SRBs as used in the CEV launcher have an extra layer of predictability over their every-day use in the STS stack: No "twang" in the booster stack as it lifts off the pad, from the off-center thrust of the SSMEs.
I'm not sure myself. I don't like the huge roman candles personally, but they are available and they are man-rated unlike anything else -that is, ANYTHING else right now! We've got either that, or the Soyuz R-7, or nothing but a long R&D program to make something else from scratch, and we all know how reliable NASA is about generating a huge cost over-run program to feed the aerospace industry beore the entire project gets cancelled after spending bilions and doing nothing (AKA the X-33).
They say an elephant is a mouse built to government specifications. I'd say that a Diplodocus is the NASA version, except it's got to have 5 heads, and it can't do anything unless at least 3 of them agree, so as often as not, it starves.
BTW I notice that the "Safe Simple Soon" site no longer has mention of the Shuttle-C earlier Shuttle-Derived booster. Too bad if they're not urging building it ASAP.
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
The lack of an escape system certainly isn't one of the Shuttle's stronger points. However, as I have pointed out before this is also true of airliners, cargo aircraft, private planes, helicopters, etc.
Anybody remember what (if any) escape system was envisioned for ground-launched Orions ? ....I believe we have some fans of that concept on this message board.
Good points about the SRB's. Good points about the lack of escape systems for airliners. Good points about the danger of the biz---all too true.
I've begun to wonder if it would be possible to basically put the 'capsule' into aerospace plane. In other aircraft, such as the supersonic XB-70, the crew could be ejected in ballistic capsules, supposedly allowing for ejection at Mach 3+ speeds. I think that a similar system could be engineered---creating a jettisonable cockpit capsule, possible a truncated right-frustrum cone, that could be nestled within the planform of a hypersonic fuselage giving the crew an all-mode escape system. The weight penalties for such a system are probably severe, but could give an aerospace vehicle an integral doscking hard docking port without the need for an external adapter--a possible plus. Provided that Orion's engine could be 'safed' then the crew could eject with similar capsules. A two stage escape burn could even put a few tens of kilometers between them and Orion, so a subsequent Range Safety Demolition explosion could safely vaporize most of the remainder of Orion so large pieces like the propulsion section and the pusher plate don't land on a populated area...but it would still be pretty messy and risky...
John Franz--I think that the delta-v achievable from an 8G 1.5 second burn is about: 8*9.8m/sec^2*1.5*sec=117 m/sec delta-v. This is close to what would be needed to deorbit. I think the Space Shuttle OMS burn imparts about 200 m/sec of delta-v which changes the perigee to something like 60 miles, well within the atmosphere.
I'd like to see the shuttle complete the space station--and you're absolutely correct about us needed to have R&D'd a replacement in the 1990's. I would have liked to see Lockheed's Venture Star takeoff--but they were experiencing severe technical probelms with the complex geometries of the composite cryogenic tankage. Perhaps a resurrection of the Venture Star with the new Aluminum-Lithium alloy using friction-stir welding is an option. It's ashame to plunk all that money into a design that never flies---nature of the biz I guess...
I would like to see a Shuttle Derived booster built---recycling as much existing infrastructure as possible when the Orbiter is retired. makes sense to me...
Still, I like to think that the materials of the ET being delivered to orbit should be considered as part of the payload. I understand why NASA has discarded them so far--anything left up in orbit is the responsibility of the country or orginization that put it there. An ET is a rather large chunk of hardware, with large heavy fittings that probably don't entirely burn up in the atmosphere. An uncontrolled reentry could dump a lot of heavy chunks of steel and aluminum on somebody's head--which is bad for PR. A future vehicle servicing a third generation space station could deliver a 'clean' tank (no poly-urethane insulation) to an orbital materials processing depot, where metals, parts, pipes, and cut plates can be scavenged and used to make more station or vehicles. The main engines could either be returned later, recycled in orbit, or dumped depending upon the cost functions of the various uses. If most of the vehicle can get a second life as 'recycled' parts or raw materials, then the space transportation dollar will go just that much farther...
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
Hi Members. In this moment Space Shuttle is very urgend for ISS buildup and should be go with the payloads for it A.S.A.P.But the risk is still present(no escape systems,sensible termal protection tiles,solid rockets segments sealing problems-and the age of all components). My opinien is the last,the oldering aspect the major problem by Space Shuttle Program.The developing engineers,facilities,manufactors,parts and skills becomes more and more a problem,because the most of the developer becomes pensioners,facilities are gone,new parts arenīt not more availeable,etc,etc. The same like if you have to maintain an very old car. At last a suitable joke: A woman will be asked about Space Shuttle what are she thinking about it.She answers,please wait,I have to ask my husband first.Than she comes back and says:"OK, we take two"! Regards: Martin
That's one of my points. The ISS was designed so the its modules would be orbited in the shuttles bay rather than on unmanned rockets. We need the shuttle for that and also for a few other missions. I see no reason not to keep the shuttle alive while introduction the CEV for pure personel transfer operations (and rescue) and future trips to the Moon. Of course I'm probably projecting a NASA budget higher the goverment is will to support at this time.
I think that we really should be working on a next generation shuttle as well. After all the shuttle is basically early '70s technology with a tight budget. The replacement shuttle could consider better configurations, heat shielding, escape systems, propulsion concepts, etc. I could proceed in concept development phase in parallel with the CEVs full scale development. Then enter its on full scale development when the CEV becomes operational.
I agree that a second generation shuttle should be built. Carefully designing the craft will remove many of the problems and deficiencies of the current Shuttle Transportation System. Boosting the 'stack' in a verticle position instead of the horizontal mode that is currently used will reduce or eliminate the possibility of ice strikes on the thermal protection system. Also, incorporating an ejectable capsule that is the cockpit/flight deck with its own seperate heat shield and parachutes and high performance ejection motors will ensure that the crew can atleast have a chance to escape at any point during the launch. Carefully designing a shuttle airframe that can incorporate something akin to a CEV crew module will promote crew survivability during 'all mode' abort scenarios. The weight penalty ought to justify the increased safety.
Also, seperating the crew from really big cargoes and launching them seperately increases safety too. This is the part I actually like about the CLV and the Magnum booster concepts currently on the drawing board.
I am not a complete risk aversion type--going into space is a dangerous activity and will always be. There are always risks in this business. However, I think it is a moral responsibility to reduce those risks to minimum levels whenever the opportunity presents itself. We should be looking at the impending retirement of the space shuttle as a good thing--so that it can make way for the next transportation system. And I would like to see more backup transportation systems--having the Delta IV, Atlas 5, the CEV/CLV, a new shuttle (perhaps a mini-shuttle), and the Magnum LV all up and running at the same time will promote increased payload throughput...
It seems to be agreed that the really large payloads (and possibly the really small ones too) should be launched with dispossable bosters. So the shuttle should most likely be sized to handle say those payloads within one standard deviations from the median plus several people. Also, it must have at least the safety for the crew and passenger that a capsule system would have. Also, it should have a clear economic advantage over disposable systems. We need to take into account operations and support costs as well as the cost of the vehicles.
It would be nice to have engines and fuel pumps that are not so pushed to the limit that they have very short high maintainence life cycles. Perhaps we need a multimode ram/scram/rocket jet technology in order to achieve this goal. If we didn't need to carry all of the oxidizer on the vehicle which for a LH2 and O2 system is 8/9s of the propellant mass we would have a much smaller vehicle. The problem is that little has been done with this technology todate.
Air breathing SCRAMjet's have their own issues, although I am not as well versed in the engineering of such machines as I am with rocket engines. Even though the scram's don't need to carry all of their oxidizer (aside from a small amount of menuvering fuel/oxidizer) they have to deal with the dual issues of drag and friction. These two issues, while less at high cruise altitudes, are nevertheless very substantial. It is entirely possible that higher heating rates (and higher peak temperatures) may be encountered in a scramjet's flight regime than in a conventional reentry path, this is because the speed and duration of a scram trajectory is required to be lower with higher speed to accelerate closer to orbital velocity.
Because of these issues I don't see a HTOL SSTO vehicle being able to take off from "San Francisco International Airport, and flying to an Orbital Hilton" with chemical propulsion systems. There just isn't enough energy in the propellant to do it in a reasonably large vehicle. Nuclear power in some form however may someday make this possible.
A nearer term Shuttle II would probably be either larger or smaller depending upon the configuration and payload requirements. If equal or nearly equal payload capacity to current shuttle (17m by 4m payload bay, 25,000 kg payload,) then a Shuttle II will probably be larger. I would imagine a vehicle about twice or three times the size of the current shuttle so that it could carry propellant for its own Main Propulsion System. A booster vehicle, possibly an even larger vehicle that has the capacity for flyback may be needed. Such a combo would probably be even more expensive to operate than the current shuttle. Also there is the problem of purging the unpressurized void spaces within the airframe, which is a substantial volume, to ensure that no explosive accumulations of oxidizing and fuel gasses occur. Even with the shuttle this is a concern for engineers, as some of the void spaces are filled with cryogenic oxygen and hydrogen tanks beneath the cargo bay--these are the fuels needed to run the onboard fuel cells, and provide drinking water and breathable oxygen for the crew. A larger vehicle will have more void space, requiring more purging, usually with either helium or nitrogen.
A smaller mini shuttle could ferry crews and small cargo (up to maybe 1-2 metric tons) to and from the space station. Its smaller size will reduce some of the complexity involved with space craft, and should also increase the robustness of the heat shield. I think a mini shuttle is the way to go...
About Shuttle-Replacement: My opinion is we couldīnt solve the the difficult matter to replace the Shuttles with aircraft like spaceships,because the worse surface to volume relations.Further is aircraft shaped form unsuitable for the space.Like an Airship is different from a Seaship and a Submarine is different too.I would prefer a cone- or dome-shaped form instead aircraft-or pencil-form,like mentioned bevore.So when we use a dome-shaped vehikle,we could install a lot of Hydrogen/Oxigen Shutte Derrivates.Because I=480seconds it could reach Orbit as a single stage and therefore the return could be done without complicated heatshilding,because the surface is big and the weight is low in relation to volume and surface. Even the payload and crew are on the top,an escape system is possible. When NTR engines are availeable(without radioactive exhaust pollution)the relation takeoff- and arrival weight are closer together than LOX/LH2 chemical performence. NTR propulsion could bring ist more ecconomy like today. But we discuss the problem about NTRīs disbehavior in parallel. But Iīm looking forward this problem could be solved. Also Prat & Whitneyīs Titan combo engine could be suitable. Regards: Martin
There used to be a lot of other discussion here of Shuttle survivability (none) and other design criteria for crew safety.
http://nasaproblems.com/ scroll down to: Concept Paper for Space Shuttle Crew Escape Concerned American Aerospace Engineers "Space Shuttle II with Crew Escape Pods" by Don A. Nelson, Rtd NASA Aerospace Engineer July 2003
(Note: I really dislike the difficulty in altering text size/font etc and hard carriage returns when copying text from other webpages!)
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
Interesting website, John. I agree that the current shuttle is impossible to increase crew survivability. My thinking for a Shuttle II would be one that does not possess an external tank--the tanks are internal. A booster vehicle would also have internal tanks, and would cross feed propellants to the orbiter for a genuine two stage launch--greatly increasing payload, performance, and decreasing the chances of ice strikes. Also, I think that designing a vehicle with assured crew survivability from the word go, will ensure that things like center of gravity issues, and automation are worked out. I haven't detailed the idea but I rather like the notion of 'cut and paste' [complete oversimplification, I know, but it illustrates the point] a CEV capsule into an airframe and then building the rest of the orbiter around that. O.K., it will probably be ugly. It will probably not be efficient. But it will provide the crew with an all aspect abort option--from launch pad catastrophic failue, all the way up to orbitat abandonement, a jettisonable flight-deck with its own RCS, parachute, and ablative TPS system to take the entire crew away to safety makes sense. However, such a system will still likely be plagued with many of the same administrative problems that the current STS suffers.
Quick access to space; quick turn arounds; automated vehicle checkout. They are all things to strive for, but they are technologically moving targets. Space transportation relying on rocket technologies is complex, difficult, and risky. And will always be.
[I share your pain in the editing of pasted material. I'm not sure if I can fix that, but I will see what I can do. Ty Moore]
I thought one of the facts on the NASA problems site was very interesting and that is that the Soyuz and the Shuttle have about the same safety rates! Yet we are just going to abandon the Shuttle to go to a Soyuz-like CEV because of its safety. This just doesn't make sense to me. Also, note that this record has been achieved in a no escape system vehicle.
I hope that people here are not taking me to be callous. Two the worst days of my life were the days that two astronaut crews died in space shuttle disasters. They are our very best. But, they also knew the risks and the were volunteers. If given the chance to fly in an up coming shuttle mission I'm game. While the though sounds scary I can't really believe that I would go.
With that said I'm not sure that escape systems are worth the cost in performance. First they do add a lot of weight and a of questionable worth overall. For example take our latest loss. In the event of a structural breakup on re-entry what would the survival changes be for the crew? What sort of g-forces would they be suddenly be subject? I think that a good escape system would have saved the Challenger crew.
The issue should be studied fairly and if a next generation shuttle be built the opportunity to incorporate this improvement would be there. But, give that we have three workable shuttle vehicles that are as safe as the alternative (capsules) I see no reason to abandon them. In fact given the issues in the NASA problems site it seems to me that making a two or three more shuttles based on the known design with evolutionary changes were improvements can be made.
> I thought one of the facts on the NASA problems site was very interesting and that is that the Soyuz and the Shuttle have about the same safety rates! Yet we are just going to abandon the Shuttle to go to a Soyuz-like CEV because of its safety.
>give that we have three workable shuttle vehicles that are as safe as the alternative (capsules) I see no reason to abandon them.
Please point out to me that part. I'm sure there's a lot more to it than you're stating.
the main point: "no reason to abandon them". How about the fact that they're overcomplex, that several primary design criteria are fabricated (re-usable main engines supposedly saving money among others), they're demonstrably not close to ideal for either crew launch or cargo launch (not survivable for crew, too complex and deliberately over-expensive for cargo).
No. If it were not for what Hickham called a "Shuttle Cult" within NASA management, they should have gone over to something like the HL-20 when it was first designed, before the Discovery took off following the re-design after the Challenger disaster. Fly cargo up on the Shuttle-C to keep using the launch infrastructure, but make it several times cheaper to launch more cargo since the flying-cost-overrun orbiter is left behind.
It was purely a money politics decision to return to the Shuttle following the Challenger (ditto for the post-Columbia era). A bureaucracy's primary mission is self-preservation, and the Shuttle keeps them employed, and it's simply not in their best financial interest to do things any differently. For the mountains of money we throw at it, we could operate a fleet of cheap crew vehicles and an assembly line operation of the Shuttle-C. The design of the present Shuttle is conducive to the pressure to go ahead and fly even though it is inherently dangerous -the same "Go Fever" that killed Challenger, killed Columbia, and it what's driving things now. If we keep trying to fly 15+ more Shuttle missions to the ISS, we have no choice but to ignore serious inherent design flaws and safety hazards, and we'll lose another crew to "Go Fever". All the while spending far too much money to do too little work (the one thing the Shuttle orbiter is ideal for).
The Shuttle as we know it is fraud, deception and it is graft. Graft and big money is its main purpose and the only reason we're still using it.
-- Edited by john fraz at 02:39, 2006-03-15
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
NASA had claimed that the CLV/CEV launch system would be safer than the Shuttle and would have a 1/2000 loss rate. When challenged they retracted this unsubstantiated claim. Historically the Russian Soyuz launcher has the best safe flight rate with 68 successful launches before a catastrophic failure. The second actual best loss rate was that of the Shuttle with 67 successful launches. It is very doubtful that the CEV will provide any actual improvement for crew safety even with the launch crew escape system because of the increased risk of crew module failures during entry. Of particular concern are the excessive high acceleration loads the crew will experience during an abort or hard landing.
My thinking is basically that there isn't a lot of statistical significance between the Shuttle and the Soyuz, i.e. 68 flights to loss vs. 67 flights to loss. Plus the article is strongly challenging NASA's claims about the projected safety of the CEV. If it were to turn out to be no better than Soyuz then the whole safety rationale for leaving the shuttle is in favor of the CEV is gone. There is further commentary to the effect that the existing NASA budget doesn't support the real cost of developing the CEV/CLV system. So it seems to me that we are putting the whole near term U.S. manned space program at risk to improve on safety when in fact we may not even be doing that.
While there are a lot of concepts all are years from realization but we have three shuttle vehicle that can fly starting later this year. A bird in the hand if you will. I like the idea of a scram jet style SSTO system but there is plenty of techology development before that can be considered practical. Other system suchs as you or Googlenaut perfer would still take years to perform engineering development and production before they could be in service. So why not just stay with the shuttle for now while devoping the techologies for a real advance 20 years from now? The is why I then suggested building perhaps two more orbiters to keep the fleet viable in for that time.
All these ideas of SCRamjets and such "second Generation" future Shuttle follow-ons are irrelevant to discussion of the present fix we're in regarding only one hyper-expensive, very risky manned spacecraft, and it's scheduled to be grounded permanently in only a few years.
The worst thing about it is that it has been touted as the best way to do it for 30 or so years, flagrantly defying the best engineering and aeronautical thinking to the contrary. Solely as a NASA government jobs program to the subcioontractors in the most congression districts possible (if they'd made it simpler and cheaper, it wouldn't let them keep so may people employed -honestly or not- or provide so much political graft). Many aspects of its design and operations principles are meant to be over-complex and not to actually assist in the agency's mission, to further the exploration of space. It's not necessary or even relevant to continuing with the Moon/Mars plans, it's in the way of real science -including precursor missions in advance of manned missions, it's probably not necessary to the ISS -cutting the Shuttle's involvement with ISS might even make it run more smoothly and efficiently since they wouldn't be operating under the primary assumption that they've got an infinite share of NASA's budget to burn. Make the ISS operate by assembly flights from unmanned Shuttle-C (delivering 3-4 times as much payload as a Shuttle, more cheaply than the Shuttle) and crews flown safely in Soyuz/CEV flights. The only thing the Shuttle itself is desperately needed for at present is 2 more flights to the ISS, and NASA is dragging their feet about even admitting that their decision to let it die was basically fraudulent.
It's not possible to upgrade or improve the Golden Goose in any meaningful ways, without drastically changing major factors of it. As for the spaceplane, the best (only) thing to do is to defy the Astronatics Corps and remove crewed piloting functions and put crew in escape pods. At that, it would drastically reduce the cost of flying the Golden Goose, and maybe make it less egregiously a rip-off to keep operating it at all. Aside from that, the best thing to do is to abandon it as a crewed launcher, and use the infrastructure of the STS by flying the booster as the Shuttle-C.
This is a fairly good recent look at what they're doing:
The most egregious budget lines are the two surviving programs that are being maintained on billions of dollars of life support--the space shuttle and the International Space Station (ISS). A question: In NASA's budgetary calculus, is it necessary or logical to maim the successful, scientifically productive and visionary part of the space program to feed the cost overruns of the Shuttle/ISS programs, which are scheduled to be canceled in 2010 anyway? Put more metaphorically, this concern was voiced by Rep. Sherwood Boehlert (R-N.Y.), chairman of the House Committee on Science when he said that "Science funding should not be taking a backseat to operational programs that have much less impact. We have to be sure that we are not demonstrating that science is a 'crown jewel' of NASA by seeing how much we can get for it at the pawnshop."
There is no easy way to quantify the science returned by the robots, but there's no question it goes way beyond what the shuttle and ISS can do. Despite some nominal science done on some shuttle missions, and its invaluable employment to place and maintain in orbit one of the most productive telescopes in observatory astronomy, the Hubble Space Telescope, it is not much of a scientific or space exploration system. And as for the science output past, present and future on the ISS, only few scientists would consider it on the positive side of cost versus benefit.
So in trekking through Washington's lunar-cold budgetary landscape, NASA obviously had to make some hard decisions. We will go on with manned missions, our goal to return to the moon and then on to Mars. This is good, very good. But first there is that little hurtle: we have got finish up the shuttle program, which, apart from fixing Hubble, serves no greater purpose except to service and complete the ISS as it circles above, on its way to where it was 90 minutes ago, waiting to be completed so it can be decommissioned.
...(cont'd)
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi
apart from fixing Hubble, serves no greater purpose except to service and complete the ISS as it circles above, on its way to where it was 90 minutes ago, waiting to be completed so it can be decommissioned.
I've heard of no plan to decommission the ISS...have you? My understanding is that the present plan is to complete the ISS using the shuttle and then use Soyuz/CEV to transport crews to and from the ISS. Maybe they were referring to the shuttle.
Anyway science as such isn't what the space program is about. It's about human evolution into the space environment. If we can do some science in the process that is good but it is secondary to the real purpose. The real reason for the shuttle was to keep manned space alive back in the anti-progressive '70s.
I still haven't heard any good responses to my point that the claim safety of Soyuz/CEV types systems is mainly an illusion. If the Shuttle and Soyuz has about the same safety record what's the big deal. I have no problem in principle with escape capsules, i.e. they would have saved lives in the Challenger but I'm not so sure about Columbia. That happened so fast I wouldn't the g-forces have killed the crew anyway?
I agree that our lame research policies have led to the situation that we can't immediately move to developing a true next generation system. Scram jet technology has been left dormant for over 30 years. The X-43 being the exception. We should being making a lot of small unmanned prototypes to develop and test the technology. So the only immediate choice is between taking a giant step back to 1970 with the CEV and just staying with the shuttle. We a going to take the step backward regardless of what I think but still it seem to me that continuing with the shuttle and making another two or three of them with what improvements can be done would be a better idea.
This is similar to the situation with fusion where we've sat on our ass for the last twelve years or so and now ITER will be built in France as an international effort when the U.S. if it had any vision could have already completed the project.
The last I heard, there was no plan to continue the ISS past maybe 2015 or so. I'll have to dig around, but they never had much intent to continue funding it past their conservative life expectancy -especially since it's horribly over expensive and basically bankrupt for any science rationale. The only serious rationale they had for it was to continue flying the Shuttle -they specifically chose this tinker-toy modular design to give the Shuttle another 35 or so flights so they could keep the money flowing to contractors in a lot of congressional districts. Since the Shuttle is so unsuitable for having anything to do with interplanetary manned flight (the thing they've always held out to us as a hope but with no budget for it), there's little hope for them to keep their funding up without having to do some real work.
> Anyway science as such isn't what the space program is about. It's about human evolution into the space environment.
Sure, you and I know that's the ultimate purpose, but there's absolutely no official recognition for that. You'll never hear anything but insincere politicians saying anything like that. The general public thinks of bad S.F TV shows when you say anything about humans living off-Earth. The real prospects for Earth and Humanity and Gaian life in general are unknown to hundreds of millions of voters and taxpayers.
>I still haven't heard any good responses to my point that the claim safety of Soyuz/CEV types systems is mainly an illusion. If the Shuttle and Soyuz has about the same safety record what's the big deal.
It all depends on what he's using as criteria for judging them. What "catastrophic failures" have the Soyuz had (3 killed decompressing on re-entry a long time ago)? they haven't had a serious problem with the R-7 while people were riding it, and that might not be called a failure of the Soyuz anyway.
One big difference is that if there is a problem with the Shuttle launch stack, it can't be anything but a catastrophe with total loss of vehicle and crew, congressional inquiries while the entire manned spaceflight program is grounded for at least a few years, and possible permanent grounding of the only manned launcher we've got. It isn't necessarily about statistics before a catastrophe, it's about a inherently fatally flawed system that's completely unforgiving.
Nobody says space is safe, or that we're demanding it to be so. It's a question of flying a system that is flawed because of mutually conflicting design requirements that drove complexity and cost and recycle cost through the roof, and has been kept alive artificially beyond its usefulness because it's the only politically alive game in town. It should never have been relied on as our regular launch system because it was designed to satisfy Air Force requirements which killed it as a reliable cheap launcher. These requirements are the source of its problems: manned with EVA support, winged runway landing with cross-range requirements of a bomber, and cargo bay and main engines included with the crew. None of this supports science or extending the range of human endeavors into space. The USAF can accept total loss in a launch failure because they're involved in warfare, and accept the risks on secret missions. These risky features should never have been part of our long-term manned launcher for so long. The Shuttle is a stratospheric fighter/bomber and an experimental craft, or it's nothing but a big waste of money. The USAF gave up on it as being to big, expensive and unwieldy, and we were stuck with it. It's long past time so accept that they're too old and not needed for any mission except what's been specifically designed to require them, just to keep them in the money.
> I have no problem in principle with escape capsules, i.e. they would have saved lives in the Challenger but I'm not so sure about Columbia. That happened so fast I wouldn't the g-forces have killed the crew anyway?
If a wing comes off or some other large piece of your airframe fails at 60km high and 6km/sec speeds, nothing's going to save you. The problem originated when the main engines were ordered to be on the orbiter by the USAF. They were supposedly going to be cheaper to operate than expendables but it never ever turned out to be even remotely so. Having engines on the plane meant the plane had to be at the bottom, with its fuel tank standing above it. This (remnant of a USAF design requirement which did nothing for civil space travel but make it more expensive) is what killed both of them. Challenger died because the strap-ons (another part of the AF needs) weren't adapted (in the cold) to the stresses of the off-center thrust of the main engines thrusting from the side. Columbia died because the plane is in the back of the launch stack, in the worst part of turbulence and stress during launch.
If the engines were at the bottom of the core (the ET), the spaceplane would go on top of the tank (eliminating ice-falls). If the cargo weren't being treated as equally important as the crew, it could have had escape systems to get it away -like the HL-42-, which would have saved the Challenger. Also if cargo weren't included in the same airframe as the crew, the whole thing is smaller and cheaper.
Statistics between the Soyuz and the Shuttle aren't the point. It's an inherently dangerous and unforgiving design, and as Hickham wrote, it pushes the state of the arts too far because of these artificial, contradictory design requirements thrust onto it for purely short-sighted political reasons. On top of that, it's ridiculously over-complex and costly for the missions we need done.
Its dead weight (airframe including all those hideously expensive manned reusable parts) is ~4 times its cargo load. The mass the basic booster stack could put up is greater than the dead weight, meaning that it's carrying 1/5 of what it's capable of, and that in the most complex, finicky, expensive manner possible -a manned, re-usable, fly-back plane. All the problems relate back to that decision by the Nixon White House to force NASA to accept USAF money and requirements.
Ditch the spaceplane, and you've got a cheaper (non-man-rated, non reusable) cargo lifter. Ditch the cargo bay and main boost engines on the plane, put it atop the thing so it can have escape rockets (I like the HL-20/42, but a capsule does OK, except for the excessive G loads), and at least it makes sense and you've got each function being performed by a vehicle that makes sense for its stated purpose.
If you're headed out into the mountains to do some prospecting/settling, do you take a sleek, fast and pretty thoroughbred race horse, or a sturdy mule; barely smart enough to follow directions, but it carries its own weight anywhere, eats anything that grows, and keeps plodding along even if it's not getting the best feed? We don't and never did really need a do-everything super advanced beast. We either needed a people-friendly light and comfortable PLS/CEV, or a big dumb booster -NOT both of them haphazardly crammed into one vehicle, so it doesn't do either task well.
-- Edited by john fraz at 02:45, 2006-03-24
__________________
"A devotee of Truth may not do anything in deference to convention. He must always hold himself open to correction, and whenever he discovers himself to be wrong he must confess it at all costs and atone for it."
Monhandas K. Gandhi