In Flight Refueling (IFR)

Abstract

Funds the system development and testing to support the incorporation of In Flight Refueling (IFR) capability into the E-2 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, 2011
Source ID
b79670042a0b225c9f11eb5cee060cf8

Tags

Readers

  • Aerospace Engineering
  • Aviation Science / Aeronautics.
  • Robotics and Automation.

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