In-Flight Refueling

Abstract

Funds the system development and testing to support the incorporation of IFR 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, 2012
Source ID
9f255d68aba540c281bdb8bada51ba40

Tags

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Naval Mine Countermeasure Systems Development.

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