SAE International Turbine Engine Starting System Design Requirements ARP949B

Description
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.
  • Turbine Engine Starting System Design Requirements - ARP949B - SAE International
    SAE International
Description
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.

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Turbine Engine Starting System Design Requirements - ARP949B - SAE International
SAE International
Warrendale, PA, United States
Turbine Engine Starting System Design Requirements
ARP949B
Turbine Engine Starting System Design Requirements ARP949B
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.

This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP949B
Product Name Turbine Engine Starting System Design Requirements
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