Aerial Refueling

Abstract

Funds the system development and testing to support the incorporation of Aerial Refueling (AR) capability into the E-2D AHE aircraft. Emphasis during system development is on system redesign, air vehicle design, human systems integration and design, including interior/lighting modifications and seat replacement. Flight testing is required to evaluate fuel systems changes, aerial refueling capability, field of view, thermal and aerodynamic loads, kinematic performance, and handling qualities. Planned for DSSC-3AR

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2018
Source ID
5e028d73e8c7179d386ca22bc3965989

Tags

Fields of Study

  • Engineering

Readers

  • Aviation Science / Aeronautics.
  • Naval Mine Countermeasure Systems Development.

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