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 field of view, thermal and aerodynamic loads, kinematic performance, and handling qualities.

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2016
Source ID
36856812f8145554d0b44cc84e48a8e8

Tags

Fields of Study

  • Engineering

Readers

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

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