F-35 program documents
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
It's not either of those.
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
similar but WAY more densely populated and for all three versions.
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
That's the one! Thanks botsing!
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
botsing wrote:P.s., that linked image was originally posted by doge.
I knew it HAD been I just couldn't find it for anything. Now I have it saved offline.
marsavian wrote: So the F-35A can do Mach 1.55, F-35B/C Mach 1.5 when loaded with external sidewinders. No real degradation.
Not quite, they HAVE done 1.55M/1.5M with "external AA".
1: they may be able to go faster and just didn't test it or include the data here. We know an F-35A went to 1.67M but that isn't shown. We know an F-35C went 1.0+M with external AG and that isn't shown.
2: It is NOT a BAD assumption to say that "external AA" means "tip-winders" and nothing else. It COULD mean the Gun Pod for the B/C, it COULD mean AMRAAMs, that much we DON'T KNOW. I think it would be safe to say that External AA is at least the AIM-9Xs.
Just being technical.
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
sprstdlyscottsmn wrote:That's the one! Thanks botsing!
Ditto. So many diagrams - not enough clues. PDF of main graphic attached & I'll make a 3 x CHART diagram. PDF attached - GIF made from this PDF.
- Attachments
-
- F-35 Block 3F.pdf
- (158.38 KiB) Downloaded 2416 times
-
- F-35 Block 3F variant CHARTS x 3 crop.pdf
- (157.67 KiB) Downloaded 2394 times
- Elite 4K
- Posts: 4474
- Joined: 23 Oct 2008, 15:22
We know the F-35C went between M1.1+ to M1.2 with 6 GBU-31, 2 AIM-120, and 2 AIM-9X. The A should be even faster. With an A2A only load, there shouldn't be much degradation at all, on top end speeds.
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
marsavian wrote:Interesting, so the F-35A/C hit Mach 1.6 at 25kft but the F-35B does it only at 30kft. Why, less thrust ?
It's the lower KCAS limit, not less thrust.
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
- Elite 5K
- Posts: 5999
- Joined: 10 Mar 2006, 01:24
- Location: Nashua NH USA
wrightwing wrote:We know the F-35C went between M1.1+ to M1.2 with 6 GBU-31, 2 AIM-120, and 2 AIM-9X. The A should be even faster. With an A2A only load, there shouldn't be much degradation at all, on top end speeds.
Do we know it went past 1.1M? AFAIK it was 1.0+M. Could have been 1.01M for all I know.
"Spurts"
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
-Pilot
-Aerospace Engineer
-Army Medic
-FMS Systems Engineer
-PFD Systems Engineer
-PATRIOT Systems Engineer
- Elite 4K
- Posts: 4474
- Joined: 23 Oct 2008, 15:22
sprstdlyscottsmn wrote:wrightwing wrote:We know the F-35C went between M1.1+ to M1.2 with 6 GBU-31, 2 AIM-120, and 2 AIM-9X. The A should be even faster. With an A2A only load, there shouldn't be much degradation at all, on top end speeds.
Do we know it went past 1.1M? AFAIK it was 1.0+M. Could have been 1.01M for all I know.
The pilot said M1.1+, when describing the photo and load.
USN Test Pilot CMDR 'Brick' Wilson says "Mach 1 plus" in the video kindly provided by 'Dragon029'.
download/file.php?id=25878
Tailhook 2017 Symposium - Update on F-35C testing from LM test pilot [start 60 sec]
https://www.youtube.com/watch?v=ZSIzWFxznvM
download/file.php?id=25878
Tailhook 2017 Symposium - Update on F-35C testing from LM test pilot [start 60 sec]
https://www.youtube.com/watch?v=ZSIzWFxznvM
Who is online
Users browsing this forum: No registered users and 7 guests