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HiMAT Systems Development Results and Projections
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English
Abstract
An overview of significant findings resulting from the development and ongoing flight test of the HiMAT RPRV system is presented, as well as potential future candidate concepts for flight research investigations. The impact and application of advanced technology features to future operational systems is treated with recommended areas of analysis, development, and testing for critical path maturity.
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Authors
Citation
Brown, L., Roe, M., and Quam, R., "HiMAT Systems Development Results and Projections," SAE Technical Paper 801175, 1980, https://doi.org/10.4271/801175.Also In
References
- Brown L.E. Roe M.H. Wiler C.D. “The HiMAT RPRV System,” AIAA Report 78-1457 August 1978
- Quam R.A. “HiMAT System Failure Detection and Redundancy Management Implementation,” Rockwell International Report NA-80-699 September 1980
- Gingrich P.B. Child R.D. Panageas G.N. “Aerodynamic Configuration Development of the Highly Maneuverable Aircraft Technology Remotely Piloted Research Vehicle,” NASA Report CR-143841 June 1977
- Price M.A. “HiMAT structural Development Design Methodology,” NASA Report CR-144886 October 1979