An Assessment of the Impact of Technology on VTOL Weight Prediction
VFS-F40-1161
5/16/1984
- Content
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The development of weight trending methods and the accurate prediction of the effects of technological advances on weight for the LHX family of vehicles will provide a challenge to the engineering community. The weight solution for the LHX will depend primarily on an accurate assessment of: 1) Technological Improvements in Rotors, Control Systems, Airframe, and Propulsion; 2) Weight impact of attribute enhancement in such areas as Nuclear, Biological and Chemical (NBC) protection, Low Observable Characteristics, Increased Reliability and Availability; and 3) Concept selection from among High Speed Compound Helicopters, ABC's or Tilt Rotors, none of which have a large statistical weight data base. To improve accuracy of the vehicle weight estimates and support associated tradeoff analyses, Sikorsky has undertaken a three-pronged approach: the update and improvement of existing statistical methods; development of interactive computer methods utilizing sizing criteria and statistical correlation coefficients; and thirdly, as a backup to these two methods, a detailed sub-system weight analysis to verify method development. The combination of these three approaches is expected to minimize the risk of predicting accurately the gross weight solution for the LHX vehicle.
- Citation
- Unsworth, D. and Sutton, J., "An Assessment of the Impact of Technology on VTOL Weight Prediction," Forum 40 - Arlington, VA 1984, Arlington, VA, May 16, 1984, https://doi.org/10.4050/VFS-F40-1161.