Extremes of Low Atmospheric Density near the Ground for Elevations up to 15,000 Feet for MIL-STD-210B

Abstract

Atmospheric density, especially low values thereof, is important to aircraft takeoff and landing operations. Such extremes must be considered in aircraft design and are therefore to be included in MIL-STD-210B. This document provides environmental design criteria to designers of military equipment, and requires for the most extreme area and month, values of low density that are equaled or surpassed during, 1, 5, 10, and 20 percent of the time for ground elevations up to 15,000 feet. Typical temperatures accompanying these values, needed for engine power calculations, are also required. This report provides these densities and temperatures. In addition, empirical equations, being used by the USAF Environmental Technical Applications Center, for estimating extremes of low density near the ground, are evaluated.

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Document Details

Document Type
Technical Report
Publication Date
Dec 06, 1972
Accession Number
AD0755791

Entities

People

  • Rene V. Cormier

Organizations

  • Air Force Cambridge Research Laboratories

Tags

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Design
  • Aircrafts
  • Altitude
  • Atmospheric Density
  • Design Criteria
  • Elevation
  • Fixed Wing Aircraft
  • High Temperature
  • Humidity
  • Lapse Rate
  • Low Density
  • Military Operations
  • Rotary Wing Aircraft
  • Sea Level
  • Standards
  • United States

Readers

  • Aerospace Engineering
  • Aerospace Test and Evaluation
  • Mathematics or Statistics