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PostPosted: 01 Sep 2004, 09:29 
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<i>Relax a few constraints and maybe you can get there from here.</i>

<b>JSF Program Alters Layout To Meet Performance Parameters</b> (Posted: Wednesday, September 01, 2004)
[Defense Daily, Sept. 1, 2004]
By Lorenzo Cortes

Apart from tackling weight and propulsion issues to meet key performance parameters (KPP) for the short takeoff, vertical landing (STOVL) variant of Lockheed Martin's [LMT] F-35 Joint Strike Fighter (JSF), the JSF program executive officer also said that the program reconfigured the weapons layout for STOVL.

"It was clear to us that with the weight overages that we have seen that we weren't going to get there just by reducing weight in the airplane," Rear Adm. Steven Enewold said yesterday in a interview with Defense Daily. The government/industry steering group for the JSF program thus looked at weight, the propulsion performance, the ways the aircraft would be used in combat and also explored the possibility relaxing some of the requirements for the aircraft.

KPPs for the STOVL JSF include a combat radius of 490 nautical miles and the ability to take off from a 550-foot flight deck for U.S. aircraft and 450 feet for the British version. Earlier this year the Pentagon said it was restructuring the JSF, adding about $5 billion and one year to the development program. The problems were largely associated with weight growth in the STOVL variant of the aircraft.

In June, the Pentagon's Defense Acquisition Board (DAB) signed off on a two-year delay to fielding the planned multirole fighter (Defense Daily, June 29). In addition to the STOVL variant, Lockheed Martin is also building a conventional takeoff and landing (CTOL) aircraft for the Air Force and a carrier variant (CV) for the Navy.

Relaxing requirements in this case center on the way the STOVL version of JSF stores weapons for combat operations. "Specifically, we've asked to move away from a common internal weapons bay and go back to a weapons bay that is smaller," Enewold explained. "We had a unique STOVL weapons bay when we started. It was a smaller weapons bay to carry two 1,000-pound JDAMs (Joint Direct Attack Munitions) and two AMRAAMs (Advanced Medium Range Air-to-Air Missiles) as the KPP load out. Because we thought we could reduce the amount of flight testing and certification and a whole bunch of other good things in the STOVL airplane, we decided to go to a common weapons bay that was common with the conventional and the CV airplanes and we found out we couldn't."

Other modifications include reducing the number of dual-carriage weapons the STOVL could mount externally. "The airplane doesn't look like it has the ability go real fast, real low," Enewold noted. "And so we backed off on the max airspeed of the airplane to match what we think the airplane aerodynamically will do."

The Air Force recently had considered developing an internal configuration of the 25mm cannon for the STOVL JSF. Presently, the program plans to equip STOVL aircraft with a missionized gun on the centerline. In 2002, Lockheed Martin decided to change the cannon for JSF, dropping the longstanding BK 27 27mm gun offered by Alliant Techsystems [ATK] and the Mauser subsidiary of Germany's Rheinmetall and going instead with General Dynamics' [GD] GAU-12 25mm gatling cannon (Defense Daily, Nov. 18, 2002).

"The Air Force is interested in integrating the internal gun into the airplane, predominantly to preserve the signature," Enewold said. "We did some initial looks at it. It looks possible, but not easy. It would add weight and drag to the airplane, we think. So right now we have recommended we not do that in the STOVL design right now."

The steering group, which includes government and industry personnel and is co-chaired by Air Force acquisiton chief Marvin Sambur and his Navy counterpart John Young, approved the STOVL modifications earlier this month.

The next big step for the JSF program is a meeting of the DAB in mid-October. During this meeting, the DAB will ascertain the program's progress.



THE CRAPTOR ENGINEERING TEAM <img src=icon_smile_big.gif border=0 align=middle>
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PostPosted: 01 Sep 2004, 09:50 
Think this will work Stress?

"I came here to kick ass and chew bubblegum...and i'm all out of bubblegum".


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PostPosted: 01 Sep 2004, 10:24 
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It Should.

Bare in mind the Harrier is a light weight when operating from the LHA's

Also recovery is fairly light. The X35 has a much larger Regime with Take off and Stovl recovery.

X35 will exceed the Harriers performance. They just cant be asking the aircraft to take Fixed wing loads as they attempted in the beginning of the program.

For the longest time the Navy punched off expensive stores for recovery in both the fixed wing force and the harrier force. This is no longer an economical option.

All aircraft have a safe minimum trap weight that needs to be met.

The Super Hornet has the best recovery of all of them. Many tradeoffs are gambled for the sake of economy in force and sustainability of operations.

In the AF if we dont drop ordnance it gets returned to inventory or the aircraft gets retasked to new targets.

In the navy, if a Jet comes back cold.. they dump the load in the ocean to make up for the safety trap shortfalls. This is not economical and prevents the CArrier wing from beng productive, as they are required to leave the mission area, and transfer new ordnace to the carrier. Many delays that can no longer be afforded.

Aircraft may need to fly more to meet their missions, Recovery attrition, logistics footprint Make their Value increased in a campaign.

"The power to Destroy the planet, is insignifigant to the power of the Air Force----Mudd Vader


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PostPosted: 01 Sep 2004, 11:31 
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<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>
Think this will work Stress?
<hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>

Abandoning commonality is the right thing to do in order to determine what the state of the STOVL art really is right now. After they have determined the optimum aircraft capability, another crisis is looming. The question asked in the Senate Hearings will be this: "Mr. Defense Secretary, why are we spending three times more per plane compared to the F-35A to achieve half the range or half the payload?". I can hear the crickets chirping while everyone looks at each other blankly.

THE CRAPTOR ENGINEERING TEAM <img src=icon_smile_big.gif border=0 align=middle>
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PostPosted: 01 Sep 2004, 11:39 
LOL

"because it's <i>TRANSFORMATIONAL</i>...or something."

"I came here to kick ass and chew bubblegum...and i'm all out of bubblegum".


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PostPosted: 02 Sep 2004, 19:54 
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It's a CAS plane (despite what the British say) and it should be optimised for that role. It's still a major improvement over the Harrier.


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PostPosted: 02 Sep 2004, 23:55 
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Hog Driver

Joined: 09 Nov 2002, 05:10
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<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>
...CAS...
<hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>

There we go throwing that word around again...


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PostPosted: 04 Sep 2004, 13:00 
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Joined: 31 Mar 2004, 11:34
Posts: 139
<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>
<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>
...CAS...
<hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>

There we go throwing that word around again...
<hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>

"CAS is a mission, not a platform."

I don't know which pointy-nosed, star-wearing individual said that, but they'll continue to eat those words in the future.

ATTACK!


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PostPosted: 07 Sep 2004, 13:36 
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Oh yeah. They should also announce a new avionics suite that is unique to the F-35B. It will not have the A2A features of the other versions (offensive and defensive) but it will be lighter and cheaper.

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PostPosted: 08 Sep 2004, 13:35 
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I think we need full A2A for the export versions. Take the Harrier II+ for example, it has the radar to give the Spanish and Italians BVR capability for fleet defense. We had to refit some of our Harriers to that standard to justify the expense even though the LHA/Ds don't even carry AMRAAMs for them to shoot.


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PostPosted: 08 Sep 2004, 14:35 
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<BLOCKQUOTE id=quote><font size=1 face="Verdana, Arial, Helvetica" id=quote>quote:<hr height=1 noshade id=quote>I think we need full A2A for the export versions. <hr height=1 noshade id=quote></BLOCKQUOTE id=quote></font id=quote><font face="Verdana, Arial, Helvetica" size=2 id=quote>

Are you willing to go for broke to keep the BVR A2A? Remember, there are other groups with equal priority pushing their point of view too. For instance, manufacturing says we absolutely need a certain structural assembly breakdown to meet cost projections. Armament also says they absolutely need 2000 lb JDAM capability to be effective against hard targets. Survivability says they absolutely need Mach 1.2 on the deck. It goes on and on. If you won't give in, neither will they, and the airplane stays overweight and too expensive. Without progress, the customers will throw in the towel. Decisions, Decisions.

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PostPosted: 08 Sep 2004, 22:48 
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Personally, I don't think the F-35B should even exist, let alone have half the stuff it has. The LHDs are going to need a major refit just to get them and the Osprey on the deck without a significant drop in airframe numbers. Unfortunately, uncle sam isn't paying all the bills. The Brits and Italians have spent money on the project and expect STOVL versions to be built for their carriers.


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PostPosted: 08 Sep 2004, 23:37 
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Stress, I like your avatar.
That's some state-of-the-art looking HUD.


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 Post subject:
PostPosted: 09 Sep 2004, 06:41 
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<i> Speaking of progress. Here's some published stuff from Aviation Leak. It's good to hear they are not building the overweight configuration of the STOVL.</i>

<b>JSF Team Shifts Course on First STOVL Version</b> (Posted: Thursday, September 09, 2004)
[Aviation Week & Space Technology, Sept. 5, 2004, page 38]

<b>Joint Strike Fighter team updates software, flight test strategy</b>

Robert Wall
Washington

F-35 Joint Strike Fighter managers have again tweaked project plans, this time to speed up testing of a production-representative short takeoff and vertical landing version of the multi-role fighter.

Resumption of Stovl JSF flight testing is planned for late 2007, this time in a production representative configuration that will differ significantly from the prototype. Credit: LOCKHEED MARTIN (Click on photo for an enlarged view)

Moreover, representatives of the Lockheed Martin-led JSF industry team are updating the program's schedule and software plans for presentation to senior Pentagon leaders in October. The meeting could put an end to the turmoil the program has been in for more than a year, since developers discovered the Stovl model was more than 3,000 lb. overweight.

When the team initially regrouped after the weight problem was found, it determined the first two of 14 flight test aircraft built during the system design and demonstration phase would have to be in the "heavy" configuration. But the contractors' so-called Stovl Weight Attack Team (Swat) was able to complete most of its work faster than expected, opening up the opportunity for the first Stovl to be in the "optimized" configuration, says Tom Burbage, Lockheed Martin vice president and JSF general manager.

The switch doesn't come without a price. First flight of B1, the first Stovl JSF, would now take place about three months later, approximately late 2007. However, Burbage points out the change eliminates a lot of engineering activity that would have gone into designing a one-off "heavy" Stovl airplane. Moreover, it should make initial flight test data more relevant.

During an informal review last month, the Pentagon gave the green light to the strategy.

The "optimized" B1 will feature a smaller bay for the Stovl version. It has been shrunk about 14 in. and will limit that version of JSF to carrying two 1,000-lb. bombs--the other models will still carry 2,000-lb. bombs. British military officials indicated some unease about the move, but Burbage says the design change was put to a vote. All Stovl customers--the U.S., the U.K. and Italy--approved the decision. B1 will also feature a redesigned top inlet used during hover and a smaller diameter lift nozzle. Both changes make the engine more efficient and help mitigate weight.

Production of the B1 will begin in late 2005 with the fuselage section at Northrop Grumman, says Steven Briggs, Northrop Grumman's JSF manager.

The weight reduction effort has shaved more than 2,700 lb. from the aircraft, and generated additional savings by relaxing performance requirements. As a result, the program has weight margin going forward, Burbage says.

Between now and October, when the next formal JSF review takes place, developers hope to have detailed plans for the various program elements in synch with the new approach. For instance, the extra engineering time has put more pressure on the flight test schedule, which is now being scrubbed. Additionally, the content and schedule of avionics software blocks are being redefined. Some software functions initially planned need updating because technology has evolved, and others are being rearranged to conform to the new program schedule.

A lesson JSF has taken from the F/A-22's troubled software experience is to locate all integration laboratories at a single site. Moreover, managers have identified possible times when those facilities will be in heavy demand, and they are trying to determine if more capacity can be made available somewhere else.

Another concern of the program was figuring out how to do all the wiring in the confined space of the JSF, particularly the Stovl with its lift fan. But that has been resolved, Burbage says. And some wiring that wasn't needed at certain weapon stations has been eliminated to save weight.

Production of the first aircraft, the "heavy" A1, is already well underway, Briggs notes. Northrop Grumman expects to deliver the first fuselage to Lockheed Martin next year, where it will be mated with the aft and forward fuselage section and the wing. Even though it is still early in the program, the company already has set up a multi-shift production process that runs seven days. The arrangement of two 10-hr. shifts worked Monday through Thursday, and two more Friday through Sunday gives the program surge capacity should schedule pressures build, while at the same time eliminating the need for costly overtime, Briggs says.

The center fuselage is furthest along. BAE Systems last week formally inaugurated its aft fuselage production line, says Tom Fillingham, the company's vice president and JSF manager.

Production so far appears to be moving ahead at a good pace. Burbage says the often complex process of establishing an enterprise-wide digital design system is paying dividends.

Looking forward, the program is essentially focused on two paths, managing international agreements and building the aircraft. In 2006, U.S. officials hope to have agreements with the partners on future production plans. Dealing with issues of training and global sustainment--including technology release for aircraft maintenance--also have to be addressed.

The other path focuses on executing the development program. Critical design review (CDR) for the first "optimized" conventional takeoff and landing aircraft is set for March 2006, concurrently with B1. But government officials would like to accelerate that by a few months. CDR for the first carrier version won't occur until 2007.

The exact production flow in the current phase also is still being devised. After A1 and B1, the program will likely build an additional Stovl aircraft and one or more of the eight non-flying static and fatigue testing versions, before delivering A2.

Burbage notes that progress is also being made on key subsystems, in particular the radar Northrop Grumman is developing and the electronic warfare suite at BAE Systems. Components are already undergoing flight testing on various surrogate aircraft. Despite delays Pratt & Whitney encountered with the F135 Stovl engine, Burbage says the propulsion arena appears to be on track to support the current schedule.



THE CRAPTOR ENGINEERING TEAM <img src=icon_smile_big.gif border=0 align=middle>
"The F-22...It's the poo"

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