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  • in reply to: The MiG-25 Unsurpassed interceptor #2475741
    michelf
    Participant

    The Mig-25 inlet is one of its secrets. It is very complex 2D inlet, with upper and lower ramps and duct guide tree, all intended to ensure stabilised airflow.
    There is no west eqivalent to this type of inlet.
    Because of this, the MiG-25 do not suffer from ‘unstarts”.

    From engineering point it is a technological marvel.

    I guess what you wrote is not what you meant….;)..

    And as you state it helps in low speed, high alpha flight.. not sure how its relevant to M3 flight but hey ho..

    As to the records…mmmm we have had this discussion before…

    Operational versus non-operational airframes….
    Actual payload capability…v SR-71 at 2T…

    I think we should stop….

    in reply to: The MiG-25 Unsurpassed interceptor #2475854
    michelf
    Participant

    The Mig-25 inlet is one of its secrets. It is very complex 2D inlet, with upper and lower ramps and duct guide tree, all intended to ensure stabilised airflow.
    There is no west eqivalent to this type of inlet.

    There are plenty of western inlets that have upper and lower ramps.. but indeed none that have the particular ‘tree’ type flow guide vanes. Now why might that be… well the SR used a completely different type of inlet.. so no need for the tree…and the XB-70 used a completely different type of inlet.. agin no tree needed.

    So the absence of a similar western inlet is not surprising. Nor does it indicate anything other than there was no need for this type…

    Because of this, the MiG-25 do not suffer from ‘unstarts”.

    From engineering point it is a technological marvel.

    I think you’ll find the MiG does not suffer from unstarts ( or as much) because the propulsion core (the R-15) is able to accept a far greater range of airflow speeds. This was needed becuase the inlet design of the MiG was not able to reliably control the airflow as much

    The ordinary Mach 2 engines uses external compression inlets, so the normal shock wave stay in the inlet lip. It doesnt enter inlet so there can not be unstarts.

    I’m struggling here to match what you are saying with what the diagrams that show the shock wave creation pattern on say a Concorde or SR inlet show. This indicated that there are a number of shock waves created from the intake lip to within the inlet itself in order to reduce the speed. The important issue here is to ensure that the location of these pressure waves is maintained with respect of the comopressor face. It also does not figure with the unstart being viewed as the shock wave moving ‘out’ of the inlet or off the lip and created an overpressure in the inlet..

    This is a matter of design, not metallurgy. The mixed compression propulsions (as used in SR-71 ) are susceptible to unstarts by its nature, because even the slight air density change can induce unstarts. Any fighter like maneuvers are out of the question.

    As the SR is the only mixed mode propulsion system to have reached (known)operational status….a sweeping generalisation is factually incorrect.

    The nature of the SR mission called for a highly optimised inlet in order to reach the efficiency of the propulsion system to generate the speed and range. This optimisation narrowed the acceptable range of flight manoeuvres within which such a system could operate. This in turn fixes the max rate turn/ pitch up/down and roll figures that the SR can accpet at speeds…..

    The change in temperature/ density causes a change in the behaviour of the air within the inlet…. it is the inability of the control system to react quickly enough to the change that causes the unstart. This is true of all supersonic inlets with variable geometry (Mig 25 included). The frequency/ serverity of the unstart is directly proportional to the optimisation of the inlet. Highly optimised inlets (for example the SR) suffer far more from the unstart issue than a more generic 2D inlet.

    So we get back to the basic issue….In order to minimise the unstart issue there are two approaches..
    1) Design an inlet that reduces the risk.. (the SR/ Concorde etc) and creates optimum intake airflow to enable the core to function as efficiently as possible. Needs sensors/ controls that react very quickly and finely…

    2) Design an engine that can take a far greater range of airflow velocities. This permits two things….an much wider range of airflows to be accepted.. both in speed and direction, which in say the MiG 25 was a prerequisite to the basic mission. In addition this makes for a core (in this case the R-15) that relies far less on optimsed inlet design to function correctly and reliably….and one which relies far less on fine/ rapid control of the inlet.

    What it does do is force the use of different materials in the engine in order to accept this wider range of airflows. In the case of the unique R-15 engine this was the creation of a transonic compressor stage…this is a big big achievement..

    Again its about using the known strengths to create the best for the known mission…it is also about creating a design that is optimised for the intended mission. If you look at the propsals for the F-108 Rapier the intention was to use 2D inlets…very much of the same type/ size as the MiG 25’s inlets. So the solution is the logicla conclusion of a design process that reveals simialr solutions for similar roles, unsurprising in view of the universal properties of physics…

    Yes. In ordinary Mach 2 engines (J-79, R-35, F-100 etc) the exhaust gas velocity is about the same as the speed of sound in the local hot gas exhaust plume.
    In the Mig-25/31 it is much higher than local exhaust speed of sound, and because of that they exhausts are called “supersonic exhausts”.

    To be sure I understand this you are saying is this.. for the R-15 the speed of the exhaust gas is far higher than the local speed of sound in air that is at the temperature of the exhaust gas.

    However in other engines the exhaust gas is moving approximately the same speed as the local speed of sound in air that is at the temperature of the exhaust gas.

    This makes a degree of sense.. however both exhausts are ‘supersonic’ as they are moving at a velocity in excess of the normalised speed of sound. Indeed you could argue (successfully) that being at the speed of sound (local) is to be supersonic. Its splitting hairs but it serves its purpose…

    You probably did not know, but the speed of sound in the hot gas exhaust airstream is much higher than in the surrounding air.

    Sadly I knew that already..;)

    The issue however remains the same. Nobody here is saying the Mig 25 is not a fanastic peice of engineering nad design. However jsut because it is that it does not mean….

    1) Its the best interceptor/ fighter/ bomber or recce aircraft ever built.
    2) Just because it has unique characteristics not present in other aircraft that it was becuase others were unable to do so…

    What it means its that this was the only aircraft that did make it to operational status that combined the speed/ altitude/ fighter performance.

    It was not the fastest, nor the highest flying, nor the most manoeuvrable….but it took dedicated airframes to exceed its performance.

    That is its real strength.

    in reply to: F-18 Hornet #2477050
    michelf
    Participant

    The post about making the SH a bigger platform and having more powerful engines is an interesting one.

    The result would have been something akin to one of the design studies that Grumman did during the F_14 development… a fixed wing F-14. (I can;t remember the project number 303F). From memory the wing was quite similar to the F-15 wing in its basic geometry.

    One would therefore imagine that a larger SH would resembe something like that project, with SH intakes/ leading edge configuration perhaps….

    in reply to: The MiG-25 Unsurpassed interceptor #2477474
    michelf
    Participant

    True. The Mig-25/31 have supersonic inlets and also supersonic exhausts.

    As I said earlier, the R-15 engine has transsonic compressor, with no west equivalent.
    It is in fact very clever solution, intended to avoid “unstart” problems associated with mixed compression propulsion used in Blackbirds and XB-70.

    Because of that, the MiG-25/31 can perform all sorts of fighter maneuvers without fear of shoch wave pops-out of the inlet, and thrust loss.

    It is unique design and, in fact, the only one possible for any efficient Mach 3 fighter.

    The Russian designers, rightly, thought that it is not enough to have Mach 3 a/c which will be capable only for a streight line flights.

    Now now Firebar… don’t let imagination run away with the reality of the choice…

    The R-15, at least initially, was designed to be used in a one way airframe….it was not meant to be very efficient nor be located behind a complex inlet that was designed to provide fully optimised airflow at all speeds.

    You have to remember that the control laws for a 2D inlet (as the Mig 25 has) which uses upper and lower ramps to maintain the shockwave in the ‘optimium’ location rely on three compments that the Soviets (and others) were, at the time finding hard to ‘reliably create and maintain’…

    1) Solid state circuit boards able to accept the rapid sensor inputs and react accordingly…
    2) High speed physical control mechanisms, either hydraulic or electro-mechanical…
    3) Precision high temperature sensors to provide constant inputs…

    Now it was not just a Soviet problem, it was a ‘state of the art’ both in the US and the USSR problem. Each however reacted very differently to the challenges…

    The US threw money and resources at solving the problems (solid state electronics/ high temp electronic sensors/ high precision hydraulics etc)…..the common reaction: the Soviets sought to intelligently avoid the problem, by using alternative solutions which provided them with the answer they wanted…unstarts are not an SR-71 only problem, they potentially affect all supersonic aircraft, try looking up the BA/AF unstarts during Concorde operations or those affecting the B-58…

    The risk increases with the optimisation of the engine efficiency…ie the narrower the range of acceptable inlet airflows and the greater the reliance on precision control of the airflow, the greater the need to avoid unstarts. So the SR and for example Concorde whose ‘efficiency’ in supersonic flight was the prime consideration have a history of unstarts.

    The MiG 25 whose need to fly at M3 (I’ll not debate that figure for now) is primarily a ‘dash’ speed, could afford to have a less optimised inlet, a more forgiving (but less efficient) initial compressor stage but one which allowed the airframe to carry out its mission.

    This kept the solution within the areas of known expertise (metallurgy) and avoid the need for massive research into solid state electronics etc which may have delayed the programme for relatively little (performance wise) gain in the intended role.

    I’m not sure I understand the comment about supersonic exhaust that you made. Most large turbojets (see Concorde, Phantoms, SRs etc) have a supersonic exhaust plume, so the R-15 is not unique (as far as I know) in that regard. Perhaps you meant something somewhat different.

    It would be interesting to see if we can compile a database of know unstart rates for a/c such as Concorde/ Tu -144/ SR-71/ B-58/ Blinder/ Backfire…..

    We could include the MiG 25 but would possibly exclude the B-1 and Tu 160 as both benefitted from much later electronics.

    It might help to establish what really is what.

    in reply to: The MiG-25 Unsurpassed interceptor #2477664
    michelf
    Participant

    Got news for you. ALL jet exhausts are supersonic. About the only ones that might not be is the bypass air on high-bypass airliner engines. BTW bypass ratio of the D30-F6S is 0.55 which is higher than the Super Hornet’s

    I ‘think’ that what Firebar meant is that the MiG-25 engine is capable of handling a supersonic ‘inlet’ flow.

    To a degree he is correct in that the first two stages of the compressor are designed to accept a transonic airflow. Certainly amongst contemporary engines globally this was a unique capability, however it was more a legacy of the original engine’s application than.

    The bonus from MiG’s point of view is that the engine was able to accept a far greater range of airflow speeds, massively reducing the complexity of the inlet and associated shock wave management systems. From a conceptual, technical and operational stand point this was a very intelligent and robust solution. Sure the engine itself was not as ‘efficient’ (SFC) or as long lasting, but those were downsides that were perfectly in line with the pragmatic approach to war time operations then espoused by the Soviet military.

    in reply to: Nimrods offered to Museums #1215409
    michelf
    Participant

    Nashio.

    The prospect of Nimrods being donated to Museums was fine. I think it somewhat relevant that I was told by an RAFM official that a Nimrod, Hercules and VC10 would be donated to Cosford. This was before the new building had the ground broken. I was also told that it was a condition of any new building that all airframes should be kept inside with the exception of the Hunter gate guard. Do you not agree that with those conditions imposed and the knowledge that three large and significant airframes would be donated within the next few years, that it was a bit shortsighted and that provision was not made for these airframes to be kept under cover? As well as breaking the imposed conditions?

    You went to Cosford today, I went yesterday. Cosford was and remains a wonderful collection, I just can’t say the same about the shortsighted planning of a National Collection, the NWCE, which now means that any future large acquisitions for Cosford are destined to remain outside.

    Regards,

    kev35

    Kev,

    James K kindly posted this image of the original publically posted proposed museum.

    You will notice a couple of interesting aspects…

    1) Two buildings are detailed showing a/c inside. (Not one)
    2) They mention 20 airframes being inside.

    Now…

    The 14,300m2 is for what? Both buildings or merely one? Not clear.
    20 airframes are mentionned in the text; 20 airframes are shown spread over the two buildings.. and yet 20 are currently in the smaller built building…

    Admittedly one of the airframes would appear to be a 707…the Herc is not immediately apparent nor is the Valiant and the Dakota doesn’t appear to be there.

    Perhaps the original plan for the museum comprising the two buildings is still applicable… one for the NCWE and a second display hall for the larger airframes as and when they become avaliable.

    It wouldn’t be the first time a national aircraft collection has taken a pragmatic approach to getting some of its actual airframes under cover, all the while knowing that others were due (that were conditioned on donation/ loan that they should be under cover) that would necessitate either a new building or a major change of the exisiting collection arrangement to accommodate them….

    A quick look at some key dimensions of the VC-10, Herc and Nimrod gives a rough area of 4,750m2 net needed to house the airframes (if you draw a box around each one wingspan x length) its a good guide to getting an area at this stage.

    Then add approx. another 25% to that area for all the rest (other display areas, toilets, plant spaces, structure zones and so forth)….= c.6000m2…added to the c8,000m2 already built and you have the c.14,000m2 mentionned originally.

    It would therefore not be too much of a stretch to imagine that the RAFM will build another, perhaps more hangar-like structure to house these airframes as and when they are actually on site. (They have their ‘icon’ and any further lottery funding would be based on gaining additional area for continuing the work started in the NCWE).

    Notice that the computer generated view of the original barrel vaulted museum is cropped to a view of the second building…..

    Just a thought….

    in reply to: RAFM Cosford, 31st August #1218426
    michelf
    Participant

    Sorry guys.. had to do some work this afternoon….

    James,

    Thanks for the pics.
    Actually I remember the Mozzie being perched and difficult to see…but at the same time that was part of its beauty, you never got the whole picture, you never saw it all…a very accurate depiction of war.

    Perhaps appropriate in a War Museum, less so in a aircraft museum.

    The numbers….they are not ‘assumptions’… they are based on benchmarking exercises (some very recent, some older) that were carried out on building typologies.

    Whilst assumptions is not the best word it serves to make it clear these are not precise figures but give the mid point of a range…for example the construction inflation (mid year 2005 to mid year 2008) figure varies between 12.5 to 16% depending on the sector and size of project. Within the ‘cultural sector’ there is no specific figure for aircraft museums, it is for museums and the range is from 14.7% to 16%, all museum types together. My ‘assumption’ is therefore that a figure of 15% is correct as aircraft museums are towards the simpler end of the building spectrum , yet have high cost elements in them (increasing IT and cost of steel). So whether its 14.7% or 15.5% I do not know, I take a figure that I feel is appropriate for comarative purposes.. an assumption, but one which can be supported by facts.

    In the same vein the constructions costs for non specific ‘shed’ work is based on current market prices (2008 contract awards) as we are seeing them on work in the UK. These are real figures.

    The same applies to the extra overs…they are real orders of magnitude, selected to cover the level of discussion. This is not to say that additional detail is not needed, but it serves to dilute the point.

    As an aside, within the design process there is (at least in the work we do) an on going comparative process to make sure that the technical solutions as well as the design solutions being put forward are economically sound as well as technically sound. So when proposing say a steel strucutre other options are also considered and evaluated on both financial and technical grounds to ensure the money is ‘well -spent’.

    The numbers I fear are what makes the difference. Had the price of the NCWM been the same as for Newark this entire issue would have not arisen. But that not being the case there is a need to illustrate that just because project A provides a certain type and quantum of accommodation at a certain price that project B, which provides a different quantum of a different of different accommodation at a different price that A could be scale up or the B is unnecessarily profilgate. Sadly the process does not deliver this scaling principle, even for supposedly the ‘same’ building type.

    The issue of the Superhanger is one which I got from working with the IWM staff itself. Perhaps a bit of revisionist history going on…or genuine recollections of those driving the project at the time I don’t know.

    As for how accountable a national , publically fund institution should be…oh boy what a subject, certainly now there are far more onerous demands placed on reporting than at the time or even during the AAM and AS projects, so there was a desire (if not a need) to have projects more accountable. Certainly more should be done in an accessible manner, delving thro the IWM website to find its chater, Trustees and records of meeting is time consuming.. but its there.

    As for the environmental aspects.. hanging onto any concept for the sake of it is wrong. If its no longer working then start over, new ideas etc, be that environmental, techncial or display. It should however aim to be clear as to why things are changing. The cost of such a solar array is prohibitive.. and selling back to the grid more complex than at first considered (for everyone).

    The split world is rather different..has it really ditched that concept? In its display? In the building…or has the world ditched that concept?

    Twin,

    The facts are incomplete, not incorrect. I could say that the NCWM cost £9m and have supporting facts, the same applies to a £12m figure. Neither are wrong provided there is a clear understanding of what is included in that cost.

    The same applies to Newark, a ‘project’ cost needs to be comparable…and whilst you did not indeed say it was comaprable you made is clear that for you a series of building such as Newark gave a better result than the AS and NCWM.

    Just as an aside it would be interesting to understand how a Belfast with tis 48m wingspan would fit into a space able to take a 29m Varsity, other than building a bigger building.. which has a different £/m2 rate…always upwards.
    Again to push to the other extreme a garage costs £125/m2…should the Newark hanger be at the same rate.. after all its a basic shed.

    The issue is that to house all of teh V bombers in the same hall, with the Belfast etc demands a bigger more expensive structure on a £/m2 rate than to house a Varsity.

    If even a pretty simple shed (ie a Newark style shed) is in the region of £6m (to have the bare necessities of public access for such a large building, then addition £3m buys a lot of heating, power etc that raise the ‘quality’ of the environment to a ‘national/ global museum’ standard.

    You might not like it but the reality is that it is that order to magnitude that is needed.

    To be honest I recall vividly a day at the AAM..I had taken my son there for the day..and we were in the AAM…by the B-17 on a glorious day…Sally B parked outside.. an elderly man…with his son and family was entralled by the B-17 inside and out….then he drifted off to the window…..hand on the glass looking out across the airfield. Sally B in front of him and John Romain taxing out in a Spit and you could see, feel and you knew he was gone…a time travelling.. a young man on a day in 1944, yet he was old, he missed his comarades… thoughts he could not share really with his family who had gathered round him.. grandson asking.. what’s up Grand dad?

    That moment made me realise fully to listen to people bicker about whether or not its too much or not good value is utter and total rubbish. That moment, made possible by creating the great window at Duxford justifies every penny spent, negates any discussion about viewing angles of hanging planes etc…they are swept aside by the sheer power of that connection and relationship.

    His family sat down beside us…very quiet and subdued..until my son piped up to the other lad.. ‘this is my daddy’s building you know’….the old man came across and taking my hand very formally thanked me for making his trip back to the UK for the first time since 1945 worthwhile.

    Now sorry guys…moan about money all you want…complain about hanging planes as long as you like..but to be honest it is irrelevant; that moment made it clear what was important and what was not important in the AAM.

    in reply to: RAFM Cosford, 31st August #1218673
    michelf
    Participant

    James,

    Thanks for a very good post…as usual.

    Its interesting to read through the list of what you see as the failures of the NCWM; the way you present them lists the vistor experience issues first. There is no excuse for some of them either as a functional building, nor indeed it would appear from a design point of view.

    I’ll not comment on the design per se, as it is a very personal view and not relevant to the discussion.

    Your choice of comparators is equally interesting, especially the FAA Museum… not crowded?..Must have been a different one than I visited a couple of months ago, especially the WW2/ Korean War section.

    Agree with the Science Museum..an empty space, gutted of its soul and passion fondly lived in during my formative years..with easily accessible cockpits (Hunter, Beagle, 747 proceedures trainer, Comet, C-47) all allowing dreams to take flight.

    Agree with Pensacola… truely one of the greats, alongside Dayton, NASM (old and new) and Seattle.

    My memory of the RAAF Museum is over-shadowed by the sheer energy and vitality of the Memorial Museum in Canberra…if ever a war museum had a life this was it….so many veterans with families in tow.. the sound of childrens’ laughter and cries mixed with the reflective moods of those remember fallen friends bought home to me what it is all for…and why it is absolutely necessary to create these spaces and make sure they work and are enjoyed by as wide a variety of people as possible.

    Your point about the remit of the RAF Museum is however the key…what is it really trying to do? Perhaps we can view the NCWM as an accurate reflection of its own turmoil and fractured nature?

    But the issue I aimed to address was the issue of the VFM, in particular that these landmark schemes cost the earth, delivered little and were all about getting gongs for certain people…and made no attempt to provide the aircraft enthusiast with a decent location to take a some decent pics of our ‘pet’ aeroplane.

    Certain posters have made it clear that they begrudge the funding spent on national museums and see it as spending ‘at the expense’ of local museums, and that if the locals had the cash there would be more aircraft under cover at a much more reasonable cost. Others feel that these ‘iconic’ designs are inherently wasteful…without justification.

    There is sufficient financial room for both. The local can gain access to HLF funding, on an appropriate local level to create appropriate facilities…yes it is expensive to do so and percieve they do not have the finances to prepare an application. Attack those who set the cost of doing so…they are the ones who limit the access. Similarly the nation museums must be made to stretch the boundaries, to create a new offer. They are the ground breakers, whose ever wider furrow captures more and more vistors who in turn may seek local museums to support. They are also looking at a very different pot of money than the locals.

    Finally my interest..its in past posts…but its easy, professionally I earn my living designing and building buildings and the AAM is one that has provided an income and responsibility for part of my life.

    in reply to: RAFM Cosford, 31st August #1218820
    michelf
    Participant

    Many familiar arguments coming out; sadly I’ll re-quote myself::o

    “Several years ago I attended a seminar organised by the British Aviation Preservation Council [BAPC] at Duxford in the summer of 2000. The seminar reviewed the way forward to protect the Benchmark and Significant airframes on the National Aviation heritage Register [NAHR] and one very interesting figure emerged from the review. Assuming a typical cost of between £250 and £300 to provide one square metre of basic under cover aircraft accommodation, it would “only” cost between £35 and £40 million to get all the Benchmark and Significant airframes listed on the NAHR under cover. I highlight the word “only”, because this is a small amount when you look at what has been poured into ventures like the Millennium Dome, etc.

    For up to date costing data refer to Flypast – March 2005 and Newark’s Heritage Lottery Funded Hangar, project cost £533,000 to provide 2,400m² of basic under cover accommodation at a cost of £222 per m². Admittedly this does not provide accommodation to the standards being achieved by the national museums with their environmentally controlled facilities, but it certainly slows the deterioration to a more manageable level.”

    http://forum.keypublishing.co.uk/showthread.php?t=53556&highlight=HLF

    These also make interesting reading:

    http://forum.keypublishing.co.uk/showthread.php?t=64094&highlight=HLF

    http://forum.keypublishing.co.uk/showthread.php?t=57865&highlight=HLF

    http://forum.keypublishing.co.uk/showthread.php?t=52906&highlight=HLF

    Yup.. you do keep on trotting out incomplete information…

    The Newark project is very interesting…

    1) It provides ‘basic’ accommodation for the airframes.
    It does not however meet the requirements of the large museums in terms of their remit. This basic accommodation can omit certain parts of a museum which are not possible when building a larger building; aside from preservation issues (heating/ ventialtion, humidity control and cooling) there is a far lower requirement for the public facilities, such as lifts/ new additional WCs, specific lighting, safety equipment, etc. It can also afford, in this guise to omit any additional displays, with attendant costs for additional power/ IT…etc.

    The design life of the basic hanger is in the order of 15 years, that of the AS/AAM/NCWM more like 30-40 years, with minimum of 25 years.

    The upgrade from the basic to a ‘comparable’ standard to AS/AAM/NCWM is in the order of 100%. Add in inflation since 2005 and you are looking at something more like 115% (taking the £222 to £477).

    2) Its a relatively small span building.
    For Newark this is fine, but sadly not an option for museums that have large span aircraft.

    As I said before the cost for this is more in the region of £800 to £1000/m2.

    The issue is one of what do we want our museums to do…house the maximum number of aircraft in the simplest and cheapest possible hangers, or house a rational number of important airframes in a longer lasting, better quality offer…

    in reply to: RAFM Cosford, 31st August #1218840
    michelf
    Participant

    IMHO a more telling factor to consider – how many extra airframes went under cover in Airspace when compared to what were housed in the Superhangar?

    Interesting, but is it really relevant.
    The Superhanger was created as a restoration space for major airframes. It took a relatively ‘off the shelf’ design for a large hanger and adapted it slightly for restoration use…mainly air extract for stripping/ painting airframes.

    Once this process was underway it became clear that funding for on-going restoration projects was reducing and that the museum needed to protect its previous expenditure (ie its restored airframes) rather than return them to the outside, if possible.

    It was at this juncture that the Superhanger became a display space. The space was then filled as well as could be, with no airframes suspended. It retained a level of restoration activity, but this much reduced.

    So the basic structure was not designed around a collection of aircraft, it was for ‘aircraft’….this means it is ‘relatively inefficient’ as its a bit one size fits all…lots of space, yet it is still packed with aircraft.

    Note also that the extension is not for display.. it is to recreate a large aircraft restoration bay….not a display bay. Had the intention been to create a single space the existing doors would have been removed and a single space created. Sure the new back wall would have been to a different design but this solution would have created more useable floor space. As it is we ahve a display space and restoration space.

    Also we are forgetting the creation of the education suite, the hospitality area…neither of which generate exhibition space, yet their cost is part of the building.

    in reply to: RAFM Cosford, 31st August #1218921
    michelf
    Participant

    I don’t know the budget breakdown but the £25m for AS included a few mil for the entrance building and the car park….

    Not going to help the cost per airframe. From memory there was something in the region of £8m for that little lot…

    Brings it down to £17m for the building…and so the rate per airframe is less.

    Also bear in mind that the ‘refurb and extension’ bit is soemwhat of a misnomer. The complete skin was replaced…and all of the structure stripped and repainted in situ…the unit cost of which was very close to the new build.

    I do not know the extent of the BAe support, but it may have been part of the ‘matching’ that was needed, so one biggy rather than many small one.

    Kev,
    Sorry, not ignoring you, I missed your post.

    You were clear about what you did not like, as you have been in the past. However its your view…and whilst very important that is all it is..sure you do not like/ understand/ find value in certain choices however others do. Whose’s view counts ?

    I do not have the figures for Cosford so there are no details to share.
    However I have been involved in other HLF funded aircraft museum projects and know that there are a number of ways of presenting the figures to suit the case.

    It is easy to use a ‘project’ cost for project XYZ that includes for VAT (as needed), professional fees, inflation, internal displays etc etc and use a ‘construction cost’ for project ABC and say look that one is twice the price of the other.

    Or include other bits of work on the project that are not directly related, such as the AS project whose ‘cost’ includes the car park and entrance building. It is correct to say the AirSpace project cost c.£25m and houses 30 airframes… yet at Cosford the c £12m houses 20….which is better value for money and which was more expensive?

    If you take out the c £8m for the entrance and car park the figures change a bit…

    Or even if you look at the published construction cost of Cosford c. £9m. So what does the £12m include? Fees? VAT? display fit out?

    £9m for 20 airframes begins to be even better value…

    It can be presented as £9m for over 8,000sqm; or £1125/m2 or £104.5/sqft.

    Just as a comparator currently traditional domestic construction is around £75/sqft, that’s for a 2 storey brick building with small spans.

    Large span warehouses (say 25m span max) works out at £500/m2 for the shell and slab to warehouse loads and exceptional span buildings with normal loaded slabs are c£800-1000/m2. These are the really big sheds you see in distribution centres near motorways etc etc.

    I think the extra over of £125/m2 for a slab that can take the point loadings of aircraft on jacks and has a superstructure that can take a hanging load on a clear span in excess of 50m, demountable walls to allow a/c in and out at times, is pretty good value.

    Just to reiterate:- a clear space that big would cost in the region of £6.5m to £8m if it were just a distribution warehouse.

    Add in specfic costs related to being an aircraft museum; openings large enough to allow aircraft in or out…a door that size easily adds £0.5m to the cost. And an extra over to allow for the point loads… say £300K, plus additional structure to hang a few airframes…say another £0.5m and before you know it you have a budget figure of around best case £7.8m, worse case £9.3m…

    These are basic construction costs… the £9m begins to look pretty much in the ‘range of good value’.
    I do not know the extent of the heating system in the NCWE. A basic one is assumed but as soon as more careful control and humdity control are added the cost could increase by a factor of 4 (so from say £200K to say £800K…)…plus IT infrastrucutre and lighting, another £200K..

    Lets also throw in public toilets and lifts as well…not needed for a warehouse..but needed for the museum.. say another £100K…

    Big sheds are relatively cheap….but big sheds that are museums are not, regardless of the shape. A shed that can house a 50m span a/c is going to be expensive regardless of its shape….a rectangle might be slightly cheaper, but not massively.
    Similarly as soon as you do have that type of clear span adding structure to enable a/c to be suspended is cost effective; sure it adds some, but it allows a reduction in floor area to pay for it…

    Its clear at least to me that you cannot say the iconic design has added a cost to the project. In such a building every addition in one area can be offset against intelligent omission or subtraction. To say it costs more because of its design is not necessarily the case.

    Nor is this to say that a cheaper solution was not possible, but that would would have received no funding.
    In this case the additional cost of the design is offset against recieving additional (or any) funding…which has its own ‘value for money’….

    in reply to: RAFM Cosford, 31st August #1218983
    michelf
    Participant

    Crikey, I know I’m a lawyer but I do try and avoid using the legal part of my brain on a friday afternoon 🙂 after all, thats what friday afternoons are for, surfing the web.

    , it means that instead of rotting away before I can take my kids to see them in 20 years, the airframes will still be there -conserved and preserved for all time – who knows what building they will be in then?

    TT

    TT,

    You reserve only Friday afternoon’s for surfing….oh boy are you missing out..

    I know Friday’s are tough..

    Seriously tho…this VAT issue is a tough one…had a project here where the ‘official’ position was that using the main space for corporate events was OK and most likely it would be accepted at zero rate. However this could not be guaranteed until post completion. If VAT was then assesed as being due it would be due as a lump sum plus interest etc etc. However if VAT was paid then no assessment would be needed and no further VAT liability was due.

    Charity took the approach that paying as part of the overall cash flow was a risk reduction exercise rather then having to ring fence the equivalent sum plus interest to hedge against future risk….

    Don’t know what as done at Cosford.

    Its taxing 😀 my brain now.

    and +1 for the last comment.

    in reply to: RAFM Cosford, 31st August #1219106
    michelf
    Participant

    TT,

    In theory yes you are correct. However IIRC the charity can chose to pay the VAT on the capital project if it intends to generate revenue from the facility which is not linked to its charitable purpose.

    So as I understand it the building is potentially avaliable for corporate hire (which is revenue generation not linked to the charity’s purpose) then VAT may or may not have been paid.
    Had hire only be avaliable to other charitable institutions then this would not be an issue or if it were hired out exclusively to associations linked to the purpose of the charity then its even more complex…

    It makes it difficult, unless you are party to the correct information, to establish what the cost was and what it included.

    With respect to the AS people forget, or never knew, that the ‘magazine published’ cost was for the enitre AS project, including works to the entrance/ shop building and the car park.

    in reply to: RAFM Cosford, 31st August #1219123
    michelf
    Participant

    The costs for the original design were in one of the magazines some years ago but I’ve no chance of finding them now. From memory it was something like half the cost of what was built.

    The project in the pictures Kev posted gave 14,300 square metres of display space, what was built is “over 8,000 square metres”.

    From the RAF Museum’s website describing the proposed new structure:

    “In keeping with Cosford’s hi-tech ethos and its prime location on the Wolverhampton – Telford High Technology Corridor, the main building is being planned to incorporate what will be Europe’s largest solar roof . This will enable the building to produce more non-fossil fuel power than the Museum currently consumes.”

    That sounds a good idea with the current drive to renewable energy sources. The surplus was to go into the National Grid. However, it wasn’t built.

    So we’ve got around double the cost, just over half the area originally designed and no low cost energy.

    Brilliant.

    ‘Brilliant’ indeed…if you are comparing apples to apples….

    So we have ‘a cost’ published.. we know nothing of what that cost included…such as VAT..all the displays equipment inside…professional fees..infrastructure costs…inflation?….etc…

    And we have a similar well know cost of what was built.. which may or may not include all, any none of those things…

    So basically we know nothing….and yet you are prepared to voice an opinion…!.

    (Just as a little guide…
    VAT= 17.5% extra on EVERYTHING.
    Professional fees for construction c. 14% of construction costs (Exclusive of display fit out budget.
    Inflation over the PROJECT life c. 12%

    Internal display costs (Construction) usually in the range of 30% of building cost. plus fees (c 20% of construction costs), plus VAT.

    Infrastrucutre costs (landscape and road improvements not on site) 2-5%.)

    So we can quote at length the ‘cost’ of the project and its £/m2 rate.. but depending on why you are doing the figures you can get it to say whatever you want.

    As to the area…have you considered that hanging the aircraft permits a space useage to exceed the 1.0 coefficient of not hanging them…so for the same measured floor space you can house more airframes…may you had or then again maybe not.

    As I said before….opinion is one thing, don’t make it out to be anything else.

    And lets just remember that the cost of the original design is a tad irrelevant.. if the original design was unable to gain HLF funding then it was not going to be built, regardless of its cost. Its trying to say a TSR2 is better or worse aircraft than an F111. As the TSR2’s life was so short, we can only extrapolate and hypothesise, a true, credible comparison is impossible.

    in reply to: RAFM Cosford, 31st August #1219466
    michelf
    Participant

    I don’t think anyone is complaining that rare airframes are indoors – especially good to see the Comet inside; now paint her in proper military colours – the black/dayglo scheme would do!!

    What is a complaint is that Cosford could have had a much better building to display aircraft in if they hadn’t had to meet the requirement of having a ‘Landmark’ (i.e. fancy design so that the building is ‘iconic’ rather than just what’s in it) building foisted on the as terms of the HLF grant.

    Its interesting to note that without the HLF grant there would be no building and so the airframes would still potentially be outside.

    The choice for museums is to ‘self-fund’ developments of this nature either from revenue or ‘private’ sponsorship…or to appply for HLF funding and accept that in order to qualify the rules set by the HLF are to be respected.

    Note for those who recall the HLF grant to Newark the sums involved were very different and each funding threshold has different criteria.

    So whilst we can bemoan the fact that the aesthetics of the building and the way the museum elected to display its assets may not be to our own tastes two important issues needed to be kept in mind..

    1) The aircraft are indoors…which means their long term future is far more secure.

    2) The ‘offer’ that the museum can now make is to a far wider audience. This in turn brings more people into contact with the aircraft and hence has a greater potential to stimulate interest….thus ensuring the museum itself has a longer term future.

    These set the overall tone.

    We should also look at the overall financial impact that we as aircraft enthusiasts have on large museums such as Cosford and Duxford…it is a small one and one which is decreasing rather than increasing.

    Its interesting to note that getting people to visit the AAM at Duxford is far easier if its based on the building than the aircraft.. I’d say my current ratio is something like 100:1 building versus aircraft…to the museum that represents their financial life blood. The fact that the U-2 is ‘out of reach’ or that we cannot easily see the cockpit of the Avenger is not of great relevance to them.

    As for ‘having a much better building for displaying aircraft’…says who? You? Do you have a factual basis for that statement or is it just your personal opinion? If you think there is a better museum out there then use that as an example.

    Also who says the design was ‘foisted’ on them? You make is sound as if the client (the RAF Museum) was not part of the process that developed that design and agreed to it being ‘their’ design in the application. You make it sound as if the museum was ‘told’ that this was the design they were getting regardless of their desires…and they could take it or leave it…

    Sadly the process does not work like that. Sure the museum may well have initially shown a more conventional design and used that to get people on board..and they may well have received advice that the design was not going to be successful and that something else was needed in order to win funding, but the changes would have been done with the agreement of the museum at the appropriate levels and they are the supporters of the design.

    So complain away about how the funding rules pushes museums to develop designs that may need to be more than sheds, or that they need to provide educational aspects and a ‘wow’ factor…but do not pretend that the museums are being lumbered with designs they do not want or feel have value to them as part of their offer.

    In truth we CANNOT disassociate the design with the funding in the current set up, so we cannot on the one had applaud the fact the a/c are under cover from the cover they are under.

    The system may indeed be one you disagree with but unless you change it (by voting) its the way that these captial projects will be funded at the moment and for the foreseeable future.

    And as for kev’s notion that the display is permanent and it will not change….fortunately its not the case and the displays will change in time.. perhaps not as quickly or in a way we want but its not permanent….just look at the AAM…

    Also kev can you provide any factual support for your assertion that you could have a ‘better result at less cost’? Such as what is a better result (if you know of a museum with a comparable size of exhibit that you think is better then use that)?

    The costs are more difficult to find but do you really know what the costs involved were? And how they stack up?

    Or are you just voicing an opinion…based on nothing really specific but it looks different and is therefore must have been expensive?….

    Lots of opinions….not a problem… but make it clear its an opininon…otherwise all you do ‘aircraft enthusiasts’ no favours in the process; it makes us look ignorant, selfish and narrow minded and therefore far less credible to those who are driving the process. This in turn means valid desires and comments get sidelined as ‘ranting’ and not taken seriously.

    We need threads like this to establish what we like and dislike, but make sure its clear why you think so.. such as an MSP in an Belfast when they did not carry otu airdrops for instance…or inappropriate colour schemes etc. Making sweeping statements of opinion unsupported by evidence makes aircraft enthusiasts less relevant and credible in the process.

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