SAE ARP1702A PDF

SAE ARP1702A PDF

Name:
SAE ARP1702A PDF

Published Date:
09/01/1998

Status:
Active

Description:

Defining and Measuring Factors Affecting Helicopter Turbine Engine Power Available

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

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Choose Document Language:
$27
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This Aerospace Recommended Practice (ARP)identifies and defines a method of measuring those factors affecting installed power available for helicopter power plants. These factors are installation losses, accessory power extraction, and operational effects. Accurate determination of these factors is vital in the calculation of helicopter performance as described in the flight manual. It is intended that the methods herein prescribe and define each factor as well as an approach to measuring said factor. Only standard installations of turboshaft engines in helicopters are considered. Special arrangements leading to high installation losses, such as the fitting of an infrared suppressor may require individual techniques for the determination and definition of engine installation losses.
File Size : 1 file , 110 KB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 09/01/1998

History

SAE ARP1702B
Published Date: 10/01/2021
Defining and Measuring Factors Affecting Helicopter Turbine Engine Power Available
$29.4
SAE ARP1702A
Published Date: 09/01/1998
Defining and Measuring Factors Affecting Helicopter Turbine Engine Power Available
$27

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