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THE 456th FIGHTER INTERCEPTOR SQUADRON |
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THE PROTECTORS OF S. A. C. |
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Atmospheric Properties Calculator |
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Based on US Standard Atmosphere 1976
Version 2.1.4, released August 2005
The Atmospheric Properties Calculator computes conditions of the atmosphere, airspeed conversions, and aerodynamic quantities on a reference body. The calculator is based on methods documented in the official U.S. Standard Atmosphere 1976 ( See Below). This version includes the lower atmosphere below an altitude of 53.4 miles (86 km). The upper atmosphere extending to 621 miles (1,000 km) will be included as a future enhancement. A temperature increment can also be added or subtracted to model a non-standard atmosphere on a hot or cold day, and the user interface allows conversions between common units in the English and Metric systems.
The Atmospheric Properties Calculator is compatible with Javascript 1.5 available in Internet Explorer 5.5+ and Netscape 6+. The calculator currently must be allowed to open a pop-up window to work properly. Visitors using a pop-up blocking program, including the Google Toolbar or the Firefox and Safari browsers, need to allow pop-ups for the calculator to function!
United States Committee on Extension to the Standard Atmosphere (COESA)
U.S. Standard Atmosphere 1976
Parameter: Atmospheric density, temperature, and pressure
Brief Description:
The work of the U.S. Committee on Extension to the Standard Atmosphere (COESA), established in 1953, led to the 1958, 1962, 1966, and 1976 versions of the U.S. Standard Atmosphere. These models were published in book form jointly by the National Oceanic and Atmospheric Administration (NOAA), the National Aeronautics and Space Administration (NASA), and the U.S. Air Force. Altogether 30 U.S. organizations representing government, industry, research institutions, and universities participated in the COESA effort. Based on rocket and satellite data and perfect gas theory, the atmospheric densities and temperatures are represented from sea level to 1000 km. Below 32 km the U.S. Standard Atmosphere is identical with the Standard Atmosphere of the International Civil Aviation Organization (ICAO). The U.S. Standard Atmospheres 1958, 1962, and 1976 consist of single profiles representing the idealized, steady-state atmosphere for moderate solar activity. Parameters listed include temperature, pressure, density, acceleration caused by gravity, pressure scale height, number density, mean particle speed, mean collision frequency, mean free path, mean molecular weight, sound speed, dynamic viscosity, kinematics viscosity, thermal conductivity, and geo-potential altitude. The altitude resolution varies from 0.05 km at low altitudes to 5 km at high altitudes. All tables are given in English (foot) as well as metric (meter) units. The U.S. Standard Atmosphere Supplements, 1966 includes tables of temperature, pressure, density, sound speed, viscosity, and thermal conductivity for five northern latitudes (15, 30, 45, 60, 75), for summer and winter conditions.Availability: In hard copy from the National Technical Information Office, Springfield, Virginia (Product Number: ADA-035-6000).
References:
U.S. Extension to the ICAO Standard Atmosphere, U.S. Government Printing Office, Washington, D.C., 1958.U.S. Standard Atmosphere, 1962, U.S. Government Printing Office, Washington, D.C., 1962.
U.S. Standard Atmosphere Supplements, 1966, U.S. Government Printing Office, Washington, D.C., 1966.
U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976.
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