FINAL DESIGN WEIGHT REPORT
GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT
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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.
- Research and Experimental Aircraft