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DTIC-AD-A035728

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U.S. Standard Atmosphere, 1976

The U.S. Standard Atmosphere, 1976, which is a revision of the U.S. 
Standard Atmosphere, 1962, was generated under the impetus of increased 
knowledge of the upper atmosphere obtained over the past solar cycle. Above 
50 km, this Standard is based on extensive new rocket data and theory for 
the mesosphere and lower thermosphere, and on the vast resources of satel- 
lite data for the tYermosphere acquired over more than one complete solar 
Cycle. This Standard identical with the ICAO Standard (1964) up to 32 km 
and the ISO Standard (1973) to 50 km. Part 1 gives the basis for compu- 
tati01. of the main tables Of atmospheric properties, including values of 
physical constants, conversion factors, and definitions of derived properties. 
Part 2 describes the model and data used up to 85 km, in the first section; 
and the model and data used above 85 km, in the second section. The theoreti- 
cal basis of the high-altitude model is given in an appendix. Part 3 contains 
information on minor constituents in the troposphere, stratosphere, and 
mesosphere. The main tables Of atmospheric properties to 1000 km are given 
in Part 4. The international syse of metric units is used.
The US. Standard Atmosphere, 1976, with 
tables and graphs extending to 1000 km, was 
adopted by the United States Committee on Exten- 
sion to the Standard Atmosphere (COESA) in 
February 1975. This eAition is the Same as 
COESA's V.S. Standard Atmosphere, 1962" be- 
low 50 km, but replaces the 1962 Standard Atmo- 
sphere at higher altitudes. 
"hat. portion of the 1962 and 1976 U.S. Standard 
Ati„osphereg up to 32 km is identical with the In- 
ternational Civil Aviation Organization (ICAO) 
"Manual of the ICAO Standard Atmosphere," as 
revised in 1964 (International Civil Aviation Or- 
ganizution 1964). The definition of the lowest 
50 km was recommended as the standard for inter- 
national adoption by the International Standards 
Organization (ISO) cognizant committee, ISO/ TC 
20' SC 6, and appeared as • Draft International 
Standard ISO/ DIS 2533. It was approved by the 
ISO Member Bodies in September 1973 as the ISO 
Standard Atm08phere (ISO 1973). Addendum I to 
ISO/ DIS 2533, characteristics of the atmosphere 
from 50 to 80 km, has been included in the tables 
as the Interim Standard Atmosphere. The numer- 
iCal data in Addendum I also are identical with the 
data in this Standard. COESA has recommended 
that the ICAO also extend its standard atmosphere 
to 50 km, by accepting for its Own standard the 
definition of the 32- to 59-km region of the 1962 and 
1976 U.S. Standard Atmosp}wre in order to insure 
a single, accepted international standard to the 
altitude of 50 km. The ICAO has not acted on this 
recommendation at the time of this publication.

 

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DTIC-AD-A035728

  • Version
  • 223 Downloads
  • 20.40 MB File Size
  • 1 File Count
  • March 5, 2017 Create Date
  • March 5, 2017 Last Updated
Scroll for Details

U.S. Standard Atmosphere, 1976

The U.S. Standard Atmosphere, 1976, which is a revision of the U.S. 
Standard Atmosphere, 1962, was generated under the impetus of increased 
knowledge of the upper atmosphere obtained over the past solar cycle. Above 
50 km, this Standard is based on extensive new rocket data and theory for 
the mesosphere and lower thermosphere, and on the vast resources of satel- 
lite data for the tYermosphere acquired over more than one complete solar 
Cycle. This Standard identical with the ICAO Standard (1964) up to 32 km 
and the ISO Standard (1973) to 50 km. Part 1 gives the basis for compu- 
tati01. of the main tables Of atmospheric properties, including values of 
physical constants, conversion factors, and definitions of derived properties. 
Part 2 describes the model and data used up to 85 km, in the first section; 
and the model and data used above 85 km, in the second section. The theoreti- 
cal basis of the high-altitude model is given in an appendix. Part 3 contains 
information on minor constituents in the troposphere, stratosphere, and 
mesosphere. The main tables Of atmospheric properties to 1000 km are given 
in Part 4. The international syse of metric units is used.
The US. Standard Atmosphere, 1976, with 
tables and graphs extending to 1000 km, was 
adopted by the United States Committee on Exten- 
sion to the Standard Atmosphere (COESA) in 
February 1975. This eAition is the Same as 
COESA's V.S. Standard Atmosphere, 1962" be- 
low 50 km, but replaces the 1962 Standard Atmo- 
sphere at higher altitudes. 
"hat. portion of the 1962 and 1976 U.S. Standard 
Ati„osphereg up to 32 km is identical with the In- 
ternational Civil Aviation Organization (ICAO) 
"Manual of the ICAO Standard Atmosphere," as 
revised in 1964 (International Civil Aviation Or- 
ganizution 1964). The definition of the lowest 
50 km was recommended as the standard for inter- 
national adoption by the International Standards 
Organization (ISO) cognizant committee, ISO/ TC 
20' SC 6, and appeared as • Draft International 
Standard ISO/ DIS 2533. It was approved by the 
ISO Member Bodies in September 1973 as the ISO 
Standard Atm08phere (ISO 1973). Addendum I to 
ISO/ DIS 2533, characteristics of the atmosphere 
from 50 to 80 km, has been included in the tables 
as the Interim Standard Atmosphere. The numer- 
iCal data in Addendum I also are identical with the 
data in this Standard. COESA has recommended 
that the ICAO also extend its standard atmosphere 
to 50 km, by accepting for its Own standard the 
definition of the 32- to 59-km region of the 1962 and 
1976 U.S. Standard Atmosp}wre in order to insure 
a single, accepted international standard to the 
altitude of 50 km. The ICAO has not acted on this 
recommendation at the time of this publication.

 

FileAction
DTIC-AD-A035728 U.S. Standard Atmosphere, 1976.pdfDownload 
17,005 Documents in our Technical Library
2463120 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...