A tandem nose-to-tail configuration was selected, and a detailed study of the configuration was made to assess its feasibility and identify potential problem areas. A feasibile heavy-lift vehicle is postulated with a predicted payload capability up to 18.7 tons which is recommended to be carried forward to flight evaluation. (Author)
Multi-Helicopter Heavy Lift System Feasibility Study
1972
177 pages
Report
No indication
English
Heavy Lift Helicopter Main Engines
SAE Technical Papers | 1973
|Heavy-Lift Helicopter Power Systems
SAE Technical Papers | 1974
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