Accession Number:

AD0893662

Title:

Test and Development of Flight Control Actuation System Components for Military Aircraft.

Descriptive Note:

Final rept. 17 Nov 69-25 Nov 70,

Corporate Author:

HYDRAULIC RESEARCH AND MFG CO VALENCIA CA

Personal Author(s):

Report Date:

1971-07-01

Pagination or Media Count:

224.0

Abstract:

Contents NAK Integrated Package Laboratory Tests B-47 FBW Pumping Module Evaluation Actuator Gunfire Vulnerability Evaluation Flow Difference Sensor Continued Evaluation Life Testing flow Difference Sensor Continued Evaluation Gunfire Testing Flow Difference Sensor Continued Evaluation Contamination Sensitivity Flow Difference Sensor Continued Evaluation Detection Level Improvement Active Load System Actuator Test Rig Evaluation of Simplex Integrated Actuator Package duplex Package Evaluation Hydraulic Fluid Contamination Research Input-Output Redundancy Investigation.

Subject Categories:

  • Flight Control and Instrumentation
  • Electrical and Electronic Equipment
  • Lubricants and Hydraulic Fluids
  • Hydraulic and Pneumatic Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE