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 fuel systems changes, aerial refueling capability, field of view, thermal and aerodynamic loads, kinematic performance, and handling qualities. Planned for DSSC-3AR

Document Details

Document Type
Accomplishment
Publication Date
Oct 01, 2017
Source ID
765469f96db0489621cdb34a01aa624e

Tags

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering
  • Naval Mine Countermeasure Systems Development.

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