Standard

SAE ARP1702A

Sep 1998 Withdrawn

Existing or new amendments and versions must be purchased separately.

Language English

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Abstract

This SAE 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 operation 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.

Products specifications

Standard from SAE International
Published: September 1 1998
Withdrawn: October 1 2021
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE ARP1702B
Refers: SAE ARP4056
Refers: SAE AIR1678
Refers: SAE AIR1419
Replaces: SAE ARP1702
Refers: SAE ARP1217
Refers: SAE ARP1420

Extended editions Extended editions (0)

Version history Related Corrigenda and Amendments (0)

Version history History (2)

SAE ARP1702A

SAE ARP1702

Abstract

Products specifications

Product Relations