FINAL DESIGN WEIGHT REPORT

Abstract

The report contains weight and balance data in summary and in detail. The summary data are given for several fuel and flight test instrumentation combinations considered compatible with the Flight Test Program. Performance requirements were written for endurance missions of 20 to 45 minutes and therefore weights data are given for the aircraft with fuel to perform these missions with flight test instrumentation included. The design gross weight of the aircraft is 9200 lbs., and therefore data are given for this weight.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1965
Accession Number
AD0657990

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Control Surfaces
  • Exhaust Systems
  • Fuel Systems
  • Fuel Tanks
  • Horizontal Stabilizers
  • Inertia
  • Inverters
  • Landing Gear
  • Landing Gear Doors
  • Measurement
  • Moment Of Inertia
  • Nose Wheels
  • Spars
  • Trim Tabs
  • Vertical Stabilizers

Readers

  • Aerospace Engineering
  • Technical Research and Report Writing.