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The F-14 Tomcat was designed as both an air superiority fighter and a long-range naval ... Max takeoff weight: 74,350 lb (33,725 kg) Fuel capacity: 16,200 lb (7,348 ...
The AN/AWG-9 and AN/APG-71 radars are all-weather, multi-mode X band pulse-Doppler radar systems used in the F-14 Tomcat, and also tested on TA-3B. [1] It is a long-range air-to-air system capable of guiding several AIM-54 Phoenix or AIM-120 AMRAAM missiles simultaneously, using its track while scan mode.
An electrical umbilical cord connected the pod to the control panel that was positioned on the left side of the rear cockpit. A hose from the ECS from the F-14 cooled/heated the internals of the pod in flight and kept the appropriate humidity levels constant. In 1987 VF-111 was the first squadron to deploy with a KS-153 camera system in bay two.
The Monarch Butterfly has a very low 0.168 kg/m 2 wing loading The McDonnell Douglas MD-11 has a high 837 kg/m 2 maximum wing loading. In aerodynamics, wing loading is the total weight of an aircraft or flying animal divided by the area of its wing.
A TF30-P-412A being prepared for installation in an F-14A Tomcat on board a carrier. The Grumman F-14 Tomcat with the TF30-P-414A was underpowered, because it was the Navy's intent to procure a jet fighter with a thrust-to-weight ratio (in clean configuration) of 1 or better (the US Air Force had the same goals for the F-15 Eagle and F-16 ...
F-14A Tomcats of VF-1 in flight in 1970s. The Tomcat made its combat debut during Operation Frequent Wind, the evacuation of American citizens from Saigon, in April 1975.F-14As from Fighter Squadron 1 (VF-1) and VF-2, operating from USS Enterprise, flew combat air patrols over South Vietnam to provide fighter cover for the evacuation route.
The F/A-18 inverted above an F-14 shown here is an example of fly-by-wire control. Fly-by-wire is a term used to describe the computerized automation of flight control surfaces. Early fourth-generation fighters like the F-15 Eagle and F-14 Tomcat retained electromechanical flight hydraulics.
The F-14 would use a wing sweep program to optimize lift and drag at all combat speeds, twin tails for stability, greatly reduced weight through extensive use of titanium to achieve a better thrust to weight ratio than the F-4, a pancake fuselage for increased lift, a raised tandem cockpit for reduced drag and increased visibility, a gun for ...