F-35 program documents
I'll bite - where is F135 listed as a '43,/28k'? I can answer 'where' but you will have to ask LM 'why'.
http://www.f135engine.com/proven-tech/e ... cter.shtml
http://www.f135engine.com/proven-tech/e ... cter.shtml
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spazsinbad wrote:I'll bite - where is F135 listed as a '43,/28k'? I can answer 'where' but you will have to ask LM 'why'.
http://www.f135engine.com/proven-tech/e ... cter.shtml
PW has 43k lb listed on their site > http://www.pw.utc.com/products/military/f135.asp
Didn't quite follow, so do you have any idea when that changed?
Cheers, Cola
At the link 'cola' provided the info is this: (under the 'characteristics' tab). 'TEG' will probably have an explanation whilst 'g3143' seems to be close, perhaps engine control software limits engine output for prolonging engine service life? Anyway:
Engine Characteristics
Conventional Take Off and Landing CTOL / CV Engine Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Intermediate Thrust (in pounds): 28,000 (128.1 kN)
Length: 220 inches (5.59 meters)
Inlet Diameter: 46 inches (1.17 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio: 0.57 Overall Pressure Ratio: 28
--------------------------------------------------------------------------------
Short Take Off and Vertical Landing STOVL Propulsion System Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Short Takeoff Thrust: 38,100 (169.5 kN)
Hover Thrust: 39,400 (175.3 kN)
Main Engine: 15,700
Lift Fan: 20,000
Roll Post: 3,700
Length
Main Engine: 369 inches (9.37 meters)
Inlet Diameter: 46 inches (1.17 meters)
Lift Fan: 50 inches (1.27 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio
Conventional: 0.56
Powered Lift: 0.51
Overall Pressure Ratio
Conventional: 28
Powered Lift: 29
Engine Characteristics
Conventional Take Off and Landing CTOL / CV Engine Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Intermediate Thrust (in pounds): 28,000 (128.1 kN)
Length: 220 inches (5.59 meters)
Inlet Diameter: 46 inches (1.17 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio: 0.57 Overall Pressure Ratio: 28
--------------------------------------------------------------------------------
Short Take Off and Vertical Landing STOVL Propulsion System Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Short Takeoff Thrust: 38,100 (169.5 kN)
Hover Thrust: 39,400 (175.3 kN)
Main Engine: 15,700
Lift Fan: 20,000
Roll Post: 3,700
Length
Main Engine: 369 inches (9.37 meters)
Inlet Diameter: 46 inches (1.17 meters)
Lift Fan: 50 inches (1.27 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio
Conventional: 0.56
Powered Lift: 0.51
Overall Pressure Ratio
Conventional: 28
Powered Lift: 29
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F-35 Lightning II Program Status and Fast Facts
July 17, 2012.
July 17, 2012.
- Attachments
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- F-35-Fast-Facts-July-17-2012.pdf
- F-35 Lightning II Program Status and Fast Facts
July 17, 2012. - (143.33 KiB) Downloaded 1247 times
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21 March 2012
F-35 Program Status and Weapons Roadmap
Precision Strike Annual Review 2012
Author: Col Mark Werth Director, Air System Requirements
Original Location: Available Here
Highlights:
1. 2012 Objectives (pg 12)
2. Per-Blk Weapon Certification (pg 4-6), including UK Weapons
3. Blk 4 weapons (pg 7) to include new cannon rounds and the Turkish SOM (JSOW equiv)
.
F-35 Program Status and Weapons Roadmap
Precision Strike Annual Review 2012
Author: Col Mark Werth Director, Air System Requirements
Original Location: Available Here
Highlights:
1. 2012 Objectives (pg 12)
2. Per-Blk Weapon Certification (pg 4-6), including UK Weapons
3. Blk 4 weapons (pg 7) to include new cannon rounds and the Turkish SOM (JSOW equiv)
.
- Attachments
-
- WERTH[1].pdf
- (681.76 KiB) Downloaded 6484 times
"The early bird gets the worm but the second mouse gets the cheese."
Thanks SWP. My Acrobat Reader 10.1.3 generates an error message on page 3 indicating perhaps that information is missing from that page. Anyway here is another example page (edited) from same PDF. Page 3 (with error message not shown) also attached. Plus now 'candidate weapons for Block 4' page attached.
Last edited by spazsinbad on 06 Aug 2012, 23:57, edited 1 time in total.
OK thanks. Probably a 'font thing' I'll mess around with whatever I can (currently testing Acrobat 11 which generates same message also). Using Windows 7 64 bits and I can test it in Windows 8 wappidywap 64 bits candidate BETA release. Too much info I'm sure.
Facts of much Fastness by LM 2012 13aug:
http://f-35.ca/wp-content/uploads/2012/ ... 3-2012.pdf
"On July 17, the first CV flight with Block 2A software was conducted.
&
On August 6, AN-1, the first Netherlands F-35, and AF-20 flew for the first time."
http://f-35.ca/wp-content/uploads/2012/ ... 3-2012.pdf
"On July 17, the first CV flight with Block 2A software was conducted.
&
On August 6, AN-1, the first Netherlands F-35, and AF-20 flew for the first time."
- Attachments
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- F-35-Fast-Facts-August-13-2012.pdf
- (52.43 KiB) Downloaded 1091 times
Joint Tactical Data Enterprise Services (TDES) Migration Plan (JTMP) 2009
http://idlsoc.com/Documents/Symposiums/ ... s_OASD(NII).pdf (5.4Mb)
http://idlsoc.com/Documents/Symposiums/ ... s_OASD(NII).pdf (5.4Mb)
- Attachments
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- D2_MAIN_US_TDES_Migration_Panel_Moderator_David_Nark_Narkevicius_OASD(NII).pdf
- (5.31 MiB) Downloaded 5832 times
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spaz just 4 u
Management of Australia’sAir Combat Capability—F-35A Joint Strike Fighter Acquisition - Sep' 27, 2012
http://www.scribd.com/doc/107874602/12/ ... agreements
Management of Australia’sAir Combat Capability—F-35A Joint Strike Fighter Acquisition - Sep' 27, 2012
http://www.scribd.com/doc/107874602/12/ ... agreements
- Attachments
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- Australian-National-Audit-Office-Audit-Report-No-6-2012–13-Management-of-Australia’s-Air-Combat-Capability-F-5A Acquisition.pdf
- (4.66 MiB) Downloaded 2442 times
Fast Facts Maam - nothing but the facts maam - nothing but the facts:
F-35 Lightning II Program Status and Fast Facts September 5, 2012
http://f-35.ca/wp-content/uploads/2012/ ... 5-2012.pdf (164Kb)
F-35 Lightning II Program Status and Fast Facts September 5, 2012
http://f-35.ca/wp-content/uploads/2012/ ... 5-2012.pdf (164Kb)
- Attachments
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- F-35-Fast-Facts-September-5-2012.pdf
- (163.52 KiB) Downloaded 790 times
Just the Facts - nuttin' but da facts....
F-35 Lightning II Program Status and Fast Facts October 15, 2012
http://f-35.ca/wp-content/uploads/2012/ ... 152012.pdf (150Kb)
"...On October 3 [2012], STOVL variant achieved 350 vertical landings to date...."
F-35 Lightning II Program Status and Fast Facts October 15, 2012
http://f-35.ca/wp-content/uploads/2012/ ... 152012.pdf (150Kb)
"...On October 3 [2012], STOVL variant achieved 350 vertical landings to date...."
- Attachments
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- F-35-Fast-Facts-October-152012.pdf
- (149.41 KiB) Downloaded 872 times
F-35 Lightning II Program Status and Fast Facts November 11, 2012
Original here: http://f-35.ca/wp-content/uploads/2012/ ... 1-2012.pdf
Original here: http://f-35.ca/wp-content/uploads/2012/ ... 1-2012.pdf
- Attachments
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- F-35-Fast-Facts-November-11-2012.pdf
- (138.2 KiB) Downloaded 674 times
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