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SAE ARP704A

Helicopter Engine-Rotor System Compatibility

Standard by SAE International, 2026-07-02

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  • Language: English
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About This Item

This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expended during flight test and delivers a more effective system into service. The methodology presented herein is recommended for modern digital electronic propulsion control systems and also for traditional analog and hydromechanical systems. ARP704A has been reaffirmed to comply with the SAE Five-Year Review policy. A reaffirmed status is given to technical reports that have been reviewed by the technical committee and deemed to be current with no need for immediate revision. No changes have been made to this document as a result of this review.
SKU: 398672e329f2

  • Publication Date: 2026-07-02
  • Standard Status: latest
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Helicopters, , , , , , , ,
  • Official SAE: Doi link
  • This Version: ARP704A (2026-07-02)
  • Previous Version: ARP704 (1962-06-30)

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