In 1955, Phase II evaluation of the F-101A was
completed. Although the new “Type II”
inlet ducts improved pressure recovery within the inlet duct, the F-101A would
still encounter compressor stalls at high speed and altitude. Range performance was 15% below predicted
values, the afterburners would blow out at high altitude, and lateral control
was not as desired. Work on the engines
to improve surge margin and alleviate compressor stalls, along with changes to
increase cruise efficiency, were undertaken by Pratt & Whitney while
McDonnell worked on further improvements to the inlet ducts to eliminate
compressor stalls during maneuvering flight.
First Photo: Maj. Austin A. "Gus" Julian at the controls of the second F-101A, 53-2419, which had been held on the production line for installation of the new Type II inlet ducts.
Photo Credit: National Archives and Records Administration via Mark Nankivil.
Second Photo: The first two ships in formation over Edwards AFB. The longer Type II inlet ducts on 53-2419, in the foreground, are redily noticeable compared to the smaller Type I ducts of the original aircraft.
Photo Credit: National Museum of the United States Air Force via Mark Nankivil.
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