Sweetman = no agenda? Have you been reading his stuff??? The man hates the F-35 with a passion (and has been reprimanded for it).
Not paid? What do you call advertisers?
A cynical person might assume that Mr. Sweetman was reprimanded because he was critical of a program run by a major advertiser in his publication, rather than being inaccurate.
JSF cost has several estimates, none solid
Lockheed Martin:
“The average estimated unit recurring flyaway cost for the F-35A is about $65 million in 2011 dollars,” said Lockheed spokes-woman Laurie Quincy, reiterating the company’s claim in an email Aug. 31.”
JSF program office:
“….Lockheed’s $65 million price tag claim is “disingenuous” because the figure does not include the Pratt & Whitney F135 engine that powers the jet.”
“… the program office has repeatedly asked the company to stop using the $65 million figure.”
Source: Navy Times
http://www.navytimes.com/news/2011/09/navy-jsf-cost-has-several-estimates-f35-091111w/
…..the SH has an automatic landing system and the manual landing ability is just kept for technical failure and to keep the qualification demands.
Patently untrue.
The British and Germans have no problem to have a time-out for their naval fighters for some years. It is no real capability gap because the training needs of modern fighters do not differ that much from shore-based examples. All modern main fighters are 24h all weather multi-role examples, when sim-domes allow to train special missions. In the worst case of urgency funding is no issue.
Landing on a 10K ft runway is completely different than landing on a carrier deck moving in 3 dimensions at night in foul weather. It can be simmed to a point, but cq is a perishable skill.
V/R,
CA
Annapolis
Burbage: IPP failure an “explosive event”
As reported by Australian Aviation:
“Burbage added that there was an “explosive event” that was controlled by the aircraft’s onboard fire bottles. “There was a flame – we don’t know the extent of the damage yet,” he said. “There is some damage in the surrounding area, parched areas.”
http://australianaviation.com.au/2011/08/f-35-grounding-explained/
F-35 Head Blasts $918M Cost Rise
Vice Adm. David Venlet:
“[cost increases are] an extreme and problematic burden to the US Air Force, Navy and Marine Corps.”
“Costs must come down significantly to make this aircraft one we can afford.”
“The first three initial production contracts are exceeding target costs by 11-15 percent. Over-target cost projections for the 28 U.S. aircraft in these production lots total $918 million. The U.S. Government is responsible for paying $635 million and the contractors [Lockheed Martin and Pratt & Whitney] pay $283 million by reducing their target fee. Adding to the extreme burden, and a product of the plan that is concurrently testing and producing aircraft, $136 million [to fix cracked bulkhead on F-35B and other problems] is required to modify early production aircraft to attain useful service life and capability,”
http://defense.aol.com/2011/07/19/f-35-head-blasts-918m-cost-rise-extreme-and-problematic-burde/
F-35A IOC ~2018
The F-35A IOC of ~2018 may have come from Shackleford via ARES:
“There were troubling words from the Air Force about the F-35A. The inability to demonstrate the Joint Strike Fighter’s ability to conduct offensive counter air and suppression as well as the destruction of enemy air defense in heavily defended environments is going to delay the strike fighter’s operational debut by another two years.
Last summer, the Air Force estimated that F-35’s IOC would be declared in 2016. But when an analysis is complete later this year, “we currently expect up to a two-year delay” that will push establishment of the first operational unit into 2018, Shackleford says.”
Top 10 F-35B issues
More on the F-35B: drive shafts, roll post nozzle actuators, lift fan clutch, generator (apparently the problem lies with newer generators,) wing roll-off.
http://www.flightglobal.com/blogs/the-dewline/2011/03/top-10-list-of-f-35b-flaws-and.html
LM execs describe F-35B flaws, fixes
AAI doors: short term fix is to modify software to open the doors at low airspeeds; long term fix to to redesign hinges and doors to withstand 250kt forward airspeeds.
Bulkhead (#496): short term fix is reshaping a hard edge to extend life to 1500hrs, long term fix is to reinforce with a steel or composite patch.
VLBB: Vertical lift bring back to be increased by either uprating the propulsion system or lightening the aircraft, or a combination of both.
Durability: Blamed on suppliers. Short term, buy more spares. Long term, increase quality (reliability.)
F-35B’s will not operate from CVN’s
“The agreement formalizes an earlier decision not to deploy F-35Bs from carriers, but rather to have all Marine squadrons deploying on carriers flying the same C version as their Navy compatriots. The STOVLs will operate from land bases and amphibious ships.”
Also noted is the Navy plan to operate 2 F/A-18E/F and 2 F-35C squadrons per CVN by the mid 2020’s.
The Navy also intends to develop a 6th generation aircraft to replace the Super Hornet, noting that it will not operate a CVN with an all-F-35 loadout.
Gen. Amos and the F-35C
While Gen. Amos is “optimistic” about the F-35B http://www.dodbuzz.com/2011/03/08/im-optimistic-on-f-35b-gen-amos/
he opens the door to the possibility of the USMC purchasing the F-35C http://defensetech.org/2011/03/08/amos-marines-may-buy-some-f-35cs/
What? You’re saying that the partner nations will rely on the F-18E for air superiority? Canada, Denmark, Norway, Australia, Turkey, the Royal Navy etc will all have USN carriers with F-18Es on tap? Amazing!
In the USN, the Super Hornet’s role will be is anti-air, while the primary mission of the F-35C will be strike. Both aircraft are multirole, so packages and roles can be adjusted as tactically necessary. How other nations intend to utilize F-35’s is up to them, but it looks like they have decided that single role aircraft are not the way to go.
Maybe because the US Navy and most of the partner nations will be relying on the F-35 to deliver air superiority?
Negative – that’s the Super Hornet’s job.
Dis’ a Super Hornet to your own detriment… if you have ever seen one ~hover at high alpha, you know what I mean.
Why do people compare a multirole F-35 to an air superiority EF and expect them to compete? The EF is going to be more agile, and the F-35 is going to plink targets at will…
I don’t think that the plane feeling solid to fly, was a critique. It sounded far more like a compliment(especially in light of other comments such as it’s easy to fly, and I really think pilots are going to enjoy flying this plane, etc…)
The way I took his comments were that the plane was more “solid than the F-18” in the sense one compares the ride/road feel of an Audi or BMW vs. a Ford or Chevy. The “stiffness” I take as a perception of the rigidity of the airframe. Both are complementary observations.