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New Canadian F-35 Brochure



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SpudmanWP
PostPosted: Apr 22, 2013 - 05:07 PM Reply with quote Back to top
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Spaz posed a new doc that shows some new info.

http://www.f-16.net/index.php?name=PNph ... 131#251131


I noticed one interesting thing while looking at the latest F-35 doc as it relates to Canada.

On page 4 it says:

Quote:
Greater than 700 nm mission radius in both air-to-air and air-to surface low observable combat configurations


Thoughts (simple type, increased estimations, etc)?

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hb_pencil
PostPosted: Apr 22, 2013 - 10:39 PM Reply with quote Back to top
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700nm is possible for air to air on internals alone: Removing 4000 lbs of bombs and a hi-hi-hi profile will offer the extra 220 nm miles required. Thats a sort of gold standard for the RCAF fighter operations (the CF-18's range can be an issue.) 700nm a2g is a bit more problematic. It might be possible if you only carried 500 lbs of bombs and stayed in hihihi, or with external tanks.
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SpudmanWP
PostPosted: Apr 22, 2013 - 11:13 PM Reply with quote Back to top
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No external tanks as it said "low observable combat configurations "

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hb_pencil
PostPosted: Apr 22, 2013 - 11:23 PM Reply with quote Back to top
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Who knows. I suspect if you bolted on one SDB and flew it 700 nm miles thats considered "good enough"
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spazsinbad
PostPosted: Apr 22, 2013 - 11:43 PM Reply with quote Back to top
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Some more graphics from the Canadian Brief whilst more are at the SWP URL above.

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spazsinbad
PostPosted: Apr 22, 2013 - 11:46 PM Reply with quote Back to top
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There is a quote somewhere from Burbage I think about optimising range figures for each variant, rather than using the original one set of benchmarks which have proved to be outdated/no longer suitable? Maybe the Oz Parliament sessions has that info. I'll go look.

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maus92
PostPosted: Apr 23, 2013 - 12:39 AM Reply with quote Back to top
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LM has scheduled a webinar on 30 April for Canadian citizens to circumvent traditional media and present its case directly to the citizenry:

"All Canadians invited to webinar on the F-35 Lightning II
Monday April 22nd 2013 - Lockheed Martin Press Release


Canada’s plan to recapitalize the Royal Canadian Air Force’s fighter capability has been one of the most dominate and sustained media stories, political issues and topics of discussions since the Government announced its intention to procure 65 F-35 Lightning IIs in July 2010.

Since that time, many media reports have been filed, there has been much political debate and many studies have published on the issue. While some of the information presented publicly has been accurate and factual, much of it has been inaccurate and incorrect.

On Tuesday, April 30, 2013 at 1:00 p.m. Eastern Time, Lockheed Martin will host a webinar, open to all Canadians, on the F-35 program in order to set the record straight on several issues and provide Canadians with accurate and factual information on the F-35."

http://skiesmag.com/news/articles/18743 ... ng-ii.html
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spazsinbad
PostPosted: Apr 23, 2013 - 12:59 AM Reply with quote Back to top
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Is this the same event? Oh No - not another repeat? What is the time difference in the Great White UP compared to - I dunno - Eastern Time...

F-35 for Canada. A Pilot’s Perspective. Posted 16 April 2013

Event Date: Tuesday, April 30, 2013 at 1pm EST, 12:00 PM CST

http://www.f-16.net/f-16_forum_viewtopic-t-23768.html

https://event.on24.com/eventRegistratio ... de=preview

Quote:
"With unmatched capabilities, interoperability with allies and the potential for billions of dollars in job-creating industry partnerships, the F-35 Lightning II is the right partner for a secure Canada.

Join us as an F-35 expert and F-35 test pilot discuss why the F-35 is the best solution for Canada, including:

Unmatched stealth and agility to protect Canada’s borders

Industrial partnerships with more than 50 Canadian companies

Full interoperability with allies for a more secure world
The 60 minute webinar will feature a presentation by Steve O’Bryan, Vice President of F-35 Program Integration and Business Development, and Billie Flynn, Senior F-35 Test Pilot and former Royal Canadian Air Force CF-18 pilot."

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SpudmanWP
PostPosted: Apr 23, 2013 - 01:19 AM Reply with quote Back to top
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Same event.

The link at the bottom of the skiesmag.com article points to the on24.com page listed in Spaz's post.

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hobo
PostPosted: Apr 23, 2013 - 03:40 AM Reply with quote Back to top
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SpudmanWP wrote:
Spaz posed a new doc that shows some new info.

http://www.f-16.net/index.php?name=PNph ... 131#251131


I noticed one interesting thing while looking at the latest F-35 doc as it relates to Canada.

On page 4 it says:

Quote:
Greater than 700 nm mission radius in both air-to-air and air-to surface low observable combat configurations


Thoughts (simple type, increased estimations, etc)?


The difference could easily be attributed to differences in how the flight profiles are calculated. Letting the F-35 stay at its efficient cruising altitude for a greater percentage of the flight, less time on station/over the target, different assumptions about combat.
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spazsinbad
PostPosted: Apr 23, 2013 - 05:00 AM Reply with quote Back to top
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Same info here more or less: http://www.f-16.net/index.php?name=PNph ... ett#242380
&
original 'SWP' post: http://www.f-16.net/index.php?name=PNph ... ett#220218

PARLIAMENTARY JOINT COMMITTEE ON FOREIGN AFFAIRS, DEFENCE AND TRADE 20 MARCH 2012
Department of Defence annual report 2010-11 (Public)
Quote:
“...Senator FAWCETT: I have one last question, if I can. Speaking of the key performance indicators, obviously for the overall program they are cost, schedule and performance. In cost and schedule we have seen a number of changes and rebaselining to allow for things that have happened. In terms of the KPIs against your original ops requirement document — you do not have to disclose which ones have not been met — but at this point in time have all of the original essential requirements from the ORD been met?

Mr Burbage: We have 16 key performance parameters on this airplane. Half are logistics and sustainment-related, half are aeroperformance-related and one or two are in classified areas. We have an oversight body called the Joint Requirements Oversight Council, the JROC, that looks at those requirements every year and makes decisions on them — 'Are we going to meet them, are we not going to meet them? If we are not going to meet them, what is the impact of that?' We have one this year which was the range of the Air Force airplane which had a specific set of ground rules associated with how that range is calculated which is not similar to either of the other two airplanes. The airplane flies a large part of its mission at a non-optimised altitude in the original calculation. The JROC agreed to change the ground rules to fly that airplane as the other two were flown and, when that happened, the airplane had excess margin to the range requirement. For any performance-related requirements, we artificially penalise the engine by five per cent fuel flow and two per cent thrust. Those margins are given back as we mature the design and get more and more solid on exactly what it is going to do. They are there for conservative estimation up front. We have not taken back any of those margins yet so, when those margins are taken back, the airplane will continue to be well in excess of its basic requirement. The airplane is meeting all of the other requirements today.

Senator FAWCETT: So have those requirements like schedule & cost been rebaselined, or are they are still the original ORD?

Mr Burbage: Schedule and cost are not KPPs. I thought you were talking about performance.

Senator FAWCETT: No, I recognise that. You have rebaselined schedule and cost as you have gone along. What I am asking is have the KPIs been rebaselined & does the statement you just made apply to today's KPIs or does it also apply to the original ones?

Mr Burbage: To the original set. Today, all the KPPs are green because that ground rule was changed to be common across all three airplanes on the range. But we have not taken back the margins that are being withheld to make sure those performance predictions are conservative. We are not going to have degraded engines. We basically measure our performance characteristics with a highly-degraded engine capability. Our actual flight test information coming back from the engine is better than nominal. These calculations are not done using actual airplane test data. They are done using an artificial penalty that gets paid back as the design matures....”

http://www.aph.gov.au/Parliamentary_Bus ... arings.htm

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Last edited by spazsinbad on Apr 23, 2013 - 06:41 AM; edited 1 time in total
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delvo
PostPosted: Apr 23, 2013 - 06:14 AM Reply with quote Back to top
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SpudmanWP wrote:
No external tanks as it said "low observable combat configurations "
Stealthy tanks... but I agree we're probably talking about flying without them in this case anyway.

hb_pencil wrote:
700nm is possible for air to air on internals alone: Removing 4000 lbs of bombs and a hi-hi-hi profile will offer the extra 220 nm miles required. Thats a sort of gold standard for the RCAF fighter operations (the CF-18's range can be an issue.) 700nm a2g is a bit more problematic. It might be possible if you only carried 500 lbs of bombs and stayed in hihihi, or with external tanks.
An air-to-ground load doesn't need to be 2000-pounders on each side. Most of the AtG weapons for internal use are 1000-pound-class items, including not only single bombs or cruise missiles but also sets of SDBs. And roughly 1000 pounds not much more than what you'd put on the same internal hardpoint for AtA: 335x2 for just the AMRAAMs alone, or 407x2 if Canada were to go with Meteors, plus the weight of the dual ejector. (For that matter, an AtG load could consist of 500-pound-class JDAMs or Paveways, each of which weighs less than a pair of AtA missiles.)
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hb_pencil
PostPosted: Apr 23, 2013 - 06:22 AM Reply with quote Back to top
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I think you've basically repeated my point. I was thinking if one or two SDB could basically fulfill an a2g loadout.


Frankly, knowing how some of the other competitors have been making exaggerated claims, I think LM is playing fast and loose with the facts.
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spazsinbad
PostPosted: Apr 23, 2013 - 06:45 AM Reply with quote Back to top
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'hb_pencil' from above OzParly quote why cannot there be a dramatic 100NM range addition when the F-35A flown at OPTIMUM Altitude/IAS parameters? These calculations must be easy today for mission planning via computer - peruse some NATOPS charts (sadly we do not have any for the F-35 family) to see how changing altitude or airspeed or both and doing so in a step fashion as weight reduced during flight can dramatically increase range:
Quote:
"...We have one this year which was the range of the Air Force airplane which had a specific set of ground rules associated with how that range is calculated which is not similar to either of the other two airplanes. The airplane flies a large part of its mission at a non-optimised altitude in the original calculation. The JROC agreed to change the ground rules to fly that airplane as the other two were flown and, when that happened, the airplane had excess margin to the range requirement...."

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PostPosted: Apr 23, 2013 - 08:02 AM Reply with quote Back to top
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hb_pencil wrote:

, I think LM is playing fast and loose with the facts.


Awesome phrase. Cool
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