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The F-14A was initially equipped with two Pratt & Whitney TF30-P-412A (or JTF10A) augmented turbofan engines, each rated at 20,900 lb (93 kN) of static uninstalled thrust, which enabled the aircraft to attain a maximum speed of Mach 2.34. [52] The F-14 would normally fly at a cruising speed for reduced fuel consumption, which was important for ...
F-14A Civilian aircraft with 575 hp (429 kW) Pratt & Whitney R-1690 Hornet radial and wing mounted directly on fuselage. C-14 Y1C-14 Designation for 20 Hornet-powered examples bought for the United States Army Air Corps in 1931, later became the C-14. Y1C-14A Last of the 20 Y1C-14s re-engined with a 575 hp (429 kW) Wright R-1820-7 Cyclone. Y1C-14B
The new aircraft emerged as the F-14, armed with the same AWG-9/AIM-54 outfit originally intended for the F-111B. On the F-14, the AWG-9 is capable, and its doppler system allows it to have look-down, shoot-down capabilities. [3] Hughes delivered enough AWG-9 systems and spares to equip approximately 600 F-14A/B aircraft for the Navy, and an ...
Stall speed or minimum steady flight speed for which the aircraft is still controllable. [7] [8] [9] V S 0: Stall speed or minimum flight speed in landing configuration. [7] [8] [9] V S 1: Stall speed or minimum steady flight speed for which the aircraft is still controllable in a specific configuration. [7] [8] V S R: Reference stall speed. [7 ...
F-86 Sabre: Fighter aircraft North American Aviation Used extensively during the Korean War. [34] Built for a 1944 request for a single-seat high-altitude fighter. [47] Derived from the FJ Fury. [47] 1947 [47] 1949 [34] [47] 9,860 [34] XF-85 Goblin: Parasite fighter: McDonnell Aircraft Part of a conceptualized idea for Airborne aircraft ...
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 Fighting Falcon).
The DC-10 used Honeywell's digital air data system in 1969 [13] and the F-14 CADC used on the F-14 in 1970 used custom integrated circuits. From the late 1980s much of the USAF and USN aircraft fleets were retrofitted with the GEC Avionics Rochester-developed Standard Central Air Data Computer (SCADC).
The F-14's Central Air Data Computer, also abbreviated as CADC, computes altitude, vertical speed, air speed, and mach number from sensor inputs such as pitot and static pressure and temperature. [1] From 1968 to 1970, the first CADC to use custom digital integrated circuits was developed for the F-14 .