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, 2013
Source ID
d5d8533e12fda19e0ded82f8402f0e1e

Tags

Readers

  • Aerospace Test and Evaluation
  • Naval Mine Countermeasure Systems Development.

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