Why only 7G ?
Join Date: Jul 2006
Location: by the Great Salt Lake, USA
Posts: 1,542
Likes: 0
Received 0 Likes
on
0 Posts
Which is why those F-35 customers which will be using it as their primary fighter are buying the 9G F-35A... which IS a pretty good A-A fighter!
Last edited by GreenKnight121; 27th May 2012 at 02:26.
Join Date: Oct 2007
Location: fort sheridan, il
Posts: 1,656
Likes: 0
Received 0 Likes
on
0 Posts
I remember that the p51 H had a lower G rating, lower overall weight and higher airspeed than the other p51's.
I would like to think that the amazing advantage of stovl outweighs the improved g of standard takeoff/landing
also, I recall that the F8F Bearcat had a lower g loading than the other navy fighters and had other special qualities.
so, I'm sure , like all planes, there are tradeoffs.
now, me, I'd like to see an F106 SUPER
I would like to think that the amazing advantage of stovl outweighs the improved g of standard takeoff/landing
also, I recall that the F8F Bearcat had a lower g loading than the other navy fighters and had other special qualities.
so, I'm sure , like all planes, there are tradeoffs.
now, me, I'd like to see an F106 SUPER
Join Date: Sep 2006
Location: Back of beyond!
Posts: 131
Likes: 0
Received 0 Likes
on
0 Posts
Sevenstrokeroll,
Trade offs was my point. Keeping the cost down while preserving customers' Key Performance Parameters is why we have the variants we see now. The slight exception is STOVL as the weight reduction changes in 2005 did alter the design. USAF demanded the A have an internal gun and be 9g capable. Big deck USN was range and approach speed (driving wing size and a need for ailerons at slow speed). UK and USMC was bring-back, hence the crash diet in '05 that made the weapon bay shorter (1000lb vs 2000lb stores)
In response to JTO, UK doesn't want or need F-35 as its primary fighter yet. When it does the requirements to replace Typhoon will be created and IF F-35A meets them it MAY be chosen. It may not. We may be looking at a 6th Gen UCAV fighter that can manoeuvre up to 25g should it's 50 internal BVRAAM fail to do their job.
From our perspective these are separate issues to address.
Trade offs was my point. Keeping the cost down while preserving customers' Key Performance Parameters is why we have the variants we see now. The slight exception is STOVL as the weight reduction changes in 2005 did alter the design. USAF demanded the A have an internal gun and be 9g capable. Big deck USN was range and approach speed (driving wing size and a need for ailerons at slow speed). UK and USMC was bring-back, hence the crash diet in '05 that made the weapon bay shorter (1000lb vs 2000lb stores)
In response to JTO, UK doesn't want or need F-35 as its primary fighter yet. When it does the requirements to replace Typhoon will be created and IF F-35A meets them it MAY be chosen. It may not. We may be looking at a 6th Gen UCAV fighter that can manoeuvre up to 25g should it's 50 internal BVRAAM fail to do their job.
From our perspective these are separate issues to address.
Last edited by ICBM; 27th May 2012 at 08:41.
agreed it will be a much much better A2A machine than the B.
Still I'm not terribly convinced it will be the best A2A machine out there.
Even the (usually rather diplomatic) comments from test pilots indicate to me a step back rather than forward wrt kinematic performance compared to what is lovingly called 'legacy' fighters, including the kinematically formidable Typhoon and Rafale.
Just hope no one finds a way to defeat stealth for the next 40 years...
Originally Posted by ICBM
the HOB mxs can do the rest.
Originally Posted by ICBM
You want 8 internal AMRAAM/METEOR per weapon bay?
Also remember that all that stealth technology becomes far less effective as your main self-protection method once you start transmitting radar and datalink - especially if you have to keep the target illuminated until A pol. All that time, you're closing on the bad guys (even with a signifiacnt crank manoeuvre).
Originally Posted by ICBM
So, a few F-22As with a few F-35s are a very good mix for a strike package for a multitude of reasons.
Originally Posted by Just This Once
You can give avionics and stella SA to any platform at any stage of its life. What you cannot do is give it better aerodynamics, better energy management, supercruise or an increase in either corner speed or max G. The F-35 is what it is and I am not convinced that at IOC plus 7 years that anyone will hold it in high regard.
Originally Posted by sevenstrokeroll
I would like to think that the amazing advantage of stovl outweighs the improved g of standard takeoff/landing
Originally Posted by henra
Still I'm not terribly convinced it will be the best A2A machine out there.
Originally Posted by sevenstrokeroll
I'd like to see an F106 SUPER
ICBM
On balance I believe they've got F-35 mostly right in capability terms.
Possibly.... For a USAF/USN strike fighter, sort of an F-117 plus SA and self-defense, adverse weather and moving targets, with pylons for Day Two, - with other fighters leading against the adversary fighters.
For others, as the F-16/F-18-type fighter for strike, CAS, DCA, OCA, air defense, air policing, maritime, show of force, NTISR, making coffee and bringing in the coal... Not so sure.
Cost and schedule runaways aside of course but for that you can blame politics at all levels.
I don't. Neither does RAND.
Root Cause Analyses of Nunn-McCurdy Breaches, Volume 1: <em>Zumwalt</em>-Class Destroyer, Joint Strike Fighter, Longbow Apache, and Wideband Global Satellite | RAND
Long read, but worthwhile. This program has been fully funded at all times.
On balance I believe they've got F-35 mostly right in capability terms.
Possibly.... For a USAF/USN strike fighter, sort of an F-117 plus SA and self-defense, adverse weather and moving targets, with pylons for Day Two, - with other fighters leading against the adversary fighters.
For others, as the F-16/F-18-type fighter for strike, CAS, DCA, OCA, air defense, air policing, maritime, show of force, NTISR, making coffee and bringing in the coal... Not so sure.
Cost and schedule runaways aside of course but for that you can blame politics at all levels.
I don't. Neither does RAND.
Root Cause Analyses of Nunn-McCurdy Breaches, Volume 1: <em>Zumwalt</em>-Class Destroyer, Joint Strike Fighter, Longbow Apache, and Wideband Global Satellite | RAND
Long read, but worthwhile. This program has been fully funded at all times.
Last edited by LowObservable; 27th May 2012 at 13:26.
Join Date: Sep 2006
Location: Back of beyond!
Posts: 131
Likes: 0
Received 0 Likes
on
0 Posts
Just this once we seem to be in agreement.
12 years ago we set out on a requirements path for a STOVL carrier aircraft to fulfil our means and replace the venerable sea jet and GR9. It beggars belief that the requirement suddenly changed 2 years ago when some over-zealous senior officers sought their own nirvana of a British CVN-style CAG. They were fed incorrect cost and schedule data for conversion of CVF by sources close to the carrier programme and, unfortunately, somehow bent the ear of a fresh, new government that actually heeded this tripe. A poor move indeed. That has resulted in an embarrassing u-turn by the coalition politicians and red faces by those that said this could work - those individuals have IMHO made things worse than staying with the original plan. However, when you are a former Navy that once had eyes on 2/3rds of the globe it's hard not to resist a last minute upgrade to its current small fleet is it?!
All in all a bit of buffoonery
12 years ago we set out on a requirements path for a STOVL carrier aircraft to fulfil our means and replace the venerable sea jet and GR9. It beggars belief that the requirement suddenly changed 2 years ago when some over-zealous senior officers sought their own nirvana of a British CVN-style CAG. They were fed incorrect cost and schedule data for conversion of CVF by sources close to the carrier programme and, unfortunately, somehow bent the ear of a fresh, new government that actually heeded this tripe. A poor move indeed. That has resulted in an embarrassing u-turn by the coalition politicians and red faces by those that said this could work - those individuals have IMHO made things worse than staying with the original plan. However, when you are a former Navy that once had eyes on 2/3rds of the globe it's hard not to resist a last minute upgrade to its current small fleet is it?!
All in all a bit of buffoonery
Last edited by ICBM; 27th May 2012 at 14:48.
Join Date: Sep 2006
Location: Back of beyond!
Posts: 131
Likes: 0
Received 0 Likes
on
0 Posts
LO
The Programme has always been funded; don't disagree there. How about LM politics of not being transparent with what was achievable in time and cost? How about those in the Pentagon who would not let a bad word be said on F-35 or let bad news out to those above? How about the politics of 8 partner international nations and not losing face; being seen to be out of control of issues?
They only came to light because they were impossible to hide or explain any more.
The Programme has always been funded; don't disagree there. How about LM politics of not being transparent with what was achievable in time and cost? How about those in the Pentagon who would not let a bad word be said on F-35 or let bad news out to those above? How about the politics of 8 partner international nations and not losing face; being seen to be out of control of issues?
They only came to light because they were impossible to hide or explain any more.
Join Date: Dec 2006
Location: UK
Posts: 799
Likes: 0
Received 0 Likes
on
0 Posts
ICBM and Others,
I absolutely agree that the SDSR decision and the subsequent U-turn is a major cock-up. Although, perhaps, Hammond may deserve some credit for changing course when all the best evidence told him he had to. In 'Yes Minister' terms, it was certainly a 'brave' decision.
I don't know all the insider details, but trying to pin it on 'Over-zealous senior officers' in a 'Former Navy' who were pursuing a 'Nirvana' seems simplistic at best. I have heard, from reliable quarters, that by SDSR 2010 there were plenty of scientists and Service officers (including RAF and RN) who were briefing hard against the F-35B. My take, for what it's worth, is that is plenty of blame to go around.
It's fair to criticise the programme, and also right. It's had plenty of problems and will have more. There are decent books to be written about the reasons, I'm sure, at some time in the future. But there has been plenty of independent, published reporting and analysis (GAO, Congressional Research Service and the US DoD to name three) throughout the project. You could, fairly, look at the lack of visibility on some UK and European projects, and wonder what PPrune would have been saying had they been subject to this level of scrutiny. As I said, I think this scrutiny is all good. But it needs to be rational.
My take is that the F-35 is a fairly typical US programme - they aimed very high, and are pushing the bounds of what is achievable. They are fired and fuelled by optimism, a 'can-do' approach, and of course, very large budgets. For my part, I like to focus on what they are getting right as well as their problems. Especially the stuff that our UK engineers and pilots are getting right.
Best regards as ever to those doing the job,
Engines
I absolutely agree that the SDSR decision and the subsequent U-turn is a major cock-up. Although, perhaps, Hammond may deserve some credit for changing course when all the best evidence told him he had to. In 'Yes Minister' terms, it was certainly a 'brave' decision.
I don't know all the insider details, but trying to pin it on 'Over-zealous senior officers' in a 'Former Navy' who were pursuing a 'Nirvana' seems simplistic at best. I have heard, from reliable quarters, that by SDSR 2010 there were plenty of scientists and Service officers (including RAF and RN) who were briefing hard against the F-35B. My take, for what it's worth, is that is plenty of blame to go around.
It's fair to criticise the programme, and also right. It's had plenty of problems and will have more. There are decent books to be written about the reasons, I'm sure, at some time in the future. But there has been plenty of independent, published reporting and analysis (GAO, Congressional Research Service and the US DoD to name three) throughout the project. You could, fairly, look at the lack of visibility on some UK and European projects, and wonder what PPrune would have been saying had they been subject to this level of scrutiny. As I said, I think this scrutiny is all good. But it needs to be rational.
My take is that the F-35 is a fairly typical US programme - they aimed very high, and are pushing the bounds of what is achievable. They are fired and fuelled by optimism, a 'can-do' approach, and of course, very large budgets. For my part, I like to focus on what they are getting right as well as their problems. Especially the stuff that our UK engineers and pilots are getting right.
Best regards as ever to those doing the job,
Engines
Join Date: Aug 2007
Location: London, New York, Paris, Moscow.
Posts: 3,632
Likes: 0
Received 0 Likes
on
0 Posts
And to the |OP| you may ask why only 9g when you are paying how many hundreds of millions per airframe?
Still I suppose it saves a bit on the Combat Edge apparel...
Still I suppose it saves a bit on the Combat Edge apparel...
ICBM - Thanks for the clear-up.... I see you're not among the "Congress made us do it" or the "we'd be fine if it wasn't for the testing mafia" group.
It was unfortunate, I think, that the program coincided with the Iraq/Afghan wars - so that Congress and the media were looking the other way as it went off the rails.
It was unfortunate, I think, that the program coincided with the Iraq/Afghan wars - so that Congress and the media were looking the other way as it went off the rails.
Join Date: Dec 2006
Location: UK
Posts: 799
Likes: 0
Received 0 Likes
on
0 Posts
LO and others,
I freely admit to being in the F-35 supporter camp - but as I've posted before, criticism is always a good thing.
I do, however, have to offer a view that this programme has not had any sort of honeymoon from the media or the politicians. There has been a steady stream of reports since it started, offering a wide range of views, analysis and opinions. Some of it is inaccurate, but many of the most critical reports (GAO are a good example) are stuffed with really very accurate detail. Go and take a look.
I also have to offer the opinion that the F-35 is not 'off the rails'. Problems? Yes, sure. Being tackled? Yes, that's what programmes like the F-35 are about. Nimrod MRA4 was 'off the rails' for years and no-one noticed. And it was REALLY off the rails. Typhoon had a very sticky couple of years and nobody leapt about, mainly due (in my view, anyway) to the low standard of UK defence reporting, as well as our natural secrecy.
To answer the question posed by the thread - why only 7g? Quoting my old aircraft design prof at Cranfield, you can imagine an aircraft's design space as a large balloon. The overall size of the balloon is driven by aerodynamics, physics and chemistry. Pull one bit out or push it in, and you will get a compensating push or pull somewhere else. For F-35B, the driver was weight, and taking 1.5 g's worth of metal off the airframe was, in the view of the designers and the customer, the right trade to do.
F-35, whatever variant, is not a light weight air superiority fighter, which is where the F-16 started out. Nor is it an Air Dominance fighter like F-22. Different requirements generate different designs, and comparing one bit of the performance envelope of two different aircraft is always going to be a bit of an academic exercise. The F-35 team, in my view, made a conscious decision to trade a high G capability for more internal volume for weapons, avionics and fuel. More internal volume means more structure, which in turn means that getting to 9g adds literally tons of metal.
Hope this helps a little
Engines
I freely admit to being in the F-35 supporter camp - but as I've posted before, criticism is always a good thing.
I do, however, have to offer a view that this programme has not had any sort of honeymoon from the media or the politicians. There has been a steady stream of reports since it started, offering a wide range of views, analysis and opinions. Some of it is inaccurate, but many of the most critical reports (GAO are a good example) are stuffed with really very accurate detail. Go and take a look.
I also have to offer the opinion that the F-35 is not 'off the rails'. Problems? Yes, sure. Being tackled? Yes, that's what programmes like the F-35 are about. Nimrod MRA4 was 'off the rails' for years and no-one noticed. And it was REALLY off the rails. Typhoon had a very sticky couple of years and nobody leapt about, mainly due (in my view, anyway) to the low standard of UK defence reporting, as well as our natural secrecy.
To answer the question posed by the thread - why only 7g? Quoting my old aircraft design prof at Cranfield, you can imagine an aircraft's design space as a large balloon. The overall size of the balloon is driven by aerodynamics, physics and chemistry. Pull one bit out or push it in, and you will get a compensating push or pull somewhere else. For F-35B, the driver was weight, and taking 1.5 g's worth of metal off the airframe was, in the view of the designers and the customer, the right trade to do.
F-35, whatever variant, is not a light weight air superiority fighter, which is where the F-16 started out. Nor is it an Air Dominance fighter like F-22. Different requirements generate different designs, and comparing one bit of the performance envelope of two different aircraft is always going to be a bit of an academic exercise. The F-35 team, in my view, made a conscious decision to trade a high G capability for more internal volume for weapons, avionics and fuel. More internal volume means more structure, which in turn means that getting to 9g adds literally tons of metal.
Hope this helps a little
Engines
Join Date: Jul 2006
Location: by the Great Salt Lake, USA
Posts: 1,542
Likes: 0
Received 0 Likes
on
0 Posts
Quote:
Originally Posted by GreenKnight121
Which is why those F-35 customers which will be using it as their primary fighter are buying the 9G F-35A... which IS a pretty good A-A fighter!
Are you really sure about this?
agreed it will be a much much better A2A machine than the B.
Still I'm not terribly convinced it will be the best A2A machine out there.
Even the (usually rather diplomatic) comments from test pilots indicate to me a step back rather than forward wrt kinematic performance compared to what is lovingly called 'legacy' fighters, including the kinematically formidable Typhoon and Rafale.
Just hope no one finds a way to defeat stealth for the next 40 years...
Originally Posted by GreenKnight121
Which is why those F-35 customers which will be using it as their primary fighter are buying the 9G F-35A... which IS a pretty good A-A fighter!
Are you really sure about this?
agreed it will be a much much better A2A machine than the B.
Still I'm not terribly convinced it will be the best A2A machine out there.
Even the (usually rather diplomatic) comments from test pilots indicate to me a step back rather than forward wrt kinematic performance compared to what is lovingly called 'legacy' fighters, including the kinematically formidable Typhoon and Rafale.
Just hope no one finds a way to defeat stealth for the next 40 years...
I never said the F-35A "will be the best A2A machine out there", that is your distortion of my statement.
I said the F-35A is "a pretty good A-A fighter"... which is a very different thing.
All the USAF brief for F-35A said was "exceed agility and maneuverability of F-16".. nothing was said about Typhoon/Rafale/etc. So naturally, it compares favorably to F-16, but not so well against Typhoon or Rafale.
F-16s never could beat MiG-29s or Su-27s, but they could hold their own... which is all F-35A has to do against the various MiG-35/Su-33/J10, etc models... and to put up a credible defense against T-50s & J-20s.
Does this mean combat losses? Yes... but not overwhelming losses, and there won't be all that many T-50/J-20s (or MiG-35/Su-33/J-10s) to defeat... since Russia is having to keep a much smaller air force (as is China) than the huge numbers they fielded in the 1970s-80s-early 90s.
Last edited by GreenKnight121; 28th May 2012 at 08:01.
Do a Hover - it avoids G
Join Date: Oct 1999
Location: Chichester West Sussex UK
Age: 91
Posts: 2,206
Likes: 0
Received 0 Likes
on
0 Posts
Why only 7G in a jet fighter when the pilot can for short periods endure 9G
I'm worried that if the best version is considered 'pretty good' compared to 70's designs where does that put the lesser versions in 20 years from now?
All the USAF brief for F-35A said was "exceed agility and maneuverability of F-16"..
However, I saw this statement always followed by 'in a normal combat load configuration', i.e. compared to F-16 with drop tanks and lots of ordnance.
Could you point me to a statement from a test pilot where he compares F-35 against F-16 clean A2A with maybe 2 heaters and 2 AMRAAM and 50% internal fuel?
F-16s never could beat MiG-29s or Su-27s, but they could hold their own... which is all F-35A has to do against the various MiG-35/Su-33/J10, etc models... and to put up a credible defense against T-50s & J-20s.
not mentioning wing loading and thus turn rates.
And we are still talking the 9g variant. I wouldn't want to sit in a B against such a thing. The C Version should have at least very good low speed turn rates (ITR+STR) with that big wing area and low sweep even at 7,5g.
Does this mean combat losses? Yes... but not overwhelming losses, and there won't be all that many T-50/J-20s (or MiG-35/Su-33/J-10s) to defeat... since Russia is having to keep a much smaller air force (as is China) than the huge numbers they fielded in the 1970s-80s-early 90s.
Originally Posted by ICBM
Chuckle
FBW designed in limitations to performance are all the rage in design these days.
(That said, maneuver isn't the only way to deal with SAMS, but it's part of the tool kit).
EDIT: From the Rand piece.
Unrealistic Baseline Estimates for Schedule and Cost.
The requirement to replace aging fighters, the need for affordability, and the belief that significant cost savings would be realized from implementation of acquisition reform practices all contributed
to an overly optimistic schedule and cost estimate.
to an overly optimistic schedule and cost estimate.
Snow job, not that unusual in acquisition.
The JSF Schedule Was More Aggressive Than the F-22 Schedule. Although the JSF baseline program schedule allowed more time than most aircraft between contract award and first flight, and between contract award and IOC (March 2012), these time periods were less than those for the F-22. The original schedule for STOVL from contract award to IOC was tighter than for both F/A-18E/F and F-22.
Wonder how the OBOGS/Oxygen system is doing.
Last edited by Lonewolf_50; 30th May 2012 at 21:52.