Heat stress in front and rear cockpits of F-4 aircraft

S. A. Nunneley, R. F. Stribley, J. R. Allan

Research output: Contribution to journalArticlepeer-review

13 Scopus citations

Abstract

Heat stress can be a serious problem in aircraft flown at low altitudes in warm-to-hot environments. Data are reported here on 36 flights by F-4 aircraft at Eglin AFB, FL. Ground dry-bulb temperatures (T(db,g)) were 19-33°C (mean 28°C) with psychrometric wet-bulb temperatures (T(wb)) 14-24°C (mean 20°C). Environmental and physiological data were recorded in both front and rear cockpits at 2-min intervals throughout each mission, which simulated low-level ground attack and lasted 94-126 min. Data were analyzed for four phases, A) preflight taxi, B) low-level flight, C) ordnance delivery, and D) postflight taxi. Cockpit dry-bulb temperature (T(db,c)) exceeded T(db,g) during ground operations; the front cockpit cooled in flight, while the rear remained hot. Linear relationships appeared for T(db,c) vs. T(db,g) in the four mission phases, and for globe temperature vs. T(db,c). Aircrew mean skin temperature was significantly related to T(db,c), and core (ear canal) temperature rose slightly with heat stress. Sweat rates reflected both T(db,c) and clothing worn. Discussion covers differences in air conditioning in the two cockpits and possible consequences of the observed heat stress and physiological strain.

Original languageEnglish (US)
Pages (from-to)287-290
Number of pages4
JournalAviation Space and Environmental Medicine
Volume52
Issue number5
StatePublished - Dec 1 1981
Externally publishedYes

ASJC Scopus subject areas

  • Public Health, Environmental and Occupational Health

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