In-Flight Refueling

Abstract

Funds the system development and testing to support the incorporation of In-Flight Refueling 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, 2014
Source ID
73e3918906607526caa4627afbc6df13

Tags

Readers

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

Related Documents