FWind

Yeah, different nozzle and fairing of stabilizer actuator, different drag.

Airframe maybe not have change when have OWS. Just about with crack growth analyses and strain.

Compared with F-15

Another data from ACEVAL/AIMVAL

design limit seem 9 G in spectrum.

Roll off Pitch on

Spectrum in report https://forums.eagle.ru/topic/254416-g-limits-and-dogfighting/?do=findComment&comment=4498077

From some reports.

Well.............. AIAA-81-2461 Fleet Flight Loads Survey monitoring and analysis techniques and Statistical analysis of aircraft maneuvering data

https://apps.dtic.mil/sti/citations/ADB010399 The report was write in 1977. some technology in the report may be used to the AIM-54A/C.

But AIM-54 used SA-PD in SARH，Is it not used PD transmit messages？

https://forums.eagle.ru/forum/english/licensed-third-party-projects/heatblur-simulations/dcs-f-14a-b/7126386-aim-54-changes-new-api-fixes-are-live-in-today-s-patch?p=7138555#post7138555

https://forums.eagle.ru/forum/english/licensed-third-party-projects/heatblur-simulations/dcs-f-14a-b/7126386-aim-54-changes-new-api-fixes-are-live-in-today-s-patch?p=7138555#post7138555

COMPUTER DESIGN REQUIREMENTS FOR DIGITAL AIR -TO -AIR MISSILES https://arc.aiaa.org/doi/10.2514/6.1976-1977

It is cool.

COMPUTER DESIGN REQUIREMENTS FOR DIGITAL AIR -TO -AIR MISSILES * BY Bruce A. Hall, Frank J. Langley, and Knut 0. Wefald Raytheon Company, Missile Systems Division Hartwell, Road, Bedford, Mass. 01730 https://arc.aiaa.org/doi/10.2514/6.1976-1977 It will show something about AIM-54A and AIM-54C

The laser will not arm or fire above 25000feet(pressure altitude)

https://www.facebook.com/100001199821488/videos/1191537627562887/[video=facebook_2017;100001199821488/videos/1191537627562887/]https://www.facebook.com/100001199821488/videos/1191537627562887/

7:20

Google DC uncovering the Grumman F-14A-B-D TOMCAT NAVAIR 01-F14AAAP-1 01 September 2004

NAVAIR 01-F14AAP-1.1