Accession Number:

ADA034172

Title:

Integrated Propulsion Control System (IPCS) Volume III. FLight Test Report.

Descriptive Note:

Final technical rept. 1 Mar 73-30 Aug 76,

Corporate Author:

BOEING AEROSPACE CO SEATTLE WASH

Report Date:

1976-08-01

Pagination or Media Count:

328.0

Abstract:

The Integrated Propulsion Control System IPCS program was conducted to pursue and demonstrate the advantages of integrated propulsion controls. The program encompassed the design, build, flight qualification, and flight testing of control modes, software, and hardware. The flight test vehicle was an F-111E. The left inlet and TF30-P-9 engine were modified to operate under control of an HDC-601 computer. Two sets of hardware were built or modified and two sets of software were developed one implemented the bill-of-materials control laws and one implemented control laws developed under contract. Fifteen flights were conducted to evaluate the IPCS. The testing demonstrated that integrated digital propulsion control is effective. This document describes the flight test program and flight test results. Author

Subject Categories:

  • Attack and Fighter Aircraft
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE