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The HiMAT RPRV Propulsion Control System
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1976 by SAE International in United States
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A multimode propulsion control system concept has been developed for the remotely piloted research vehicle of the NASA Highly Maneuverable Aircraft Technology program. The concept is based on the retention of most of the bill-of-materials control hardware, and will allow the implementation of flight/propulsion control coupling, high and normal flow stability margin operating modes, and rapid and normal thrust response modes. Description of the control system, the airborne control components, and the ground generated and displayed signals is given in this paper.
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CitationBayati, J., "The HiMAT RPRV Propulsion Control System," SAE Technical Paper 760887, 1976, https://doi.org/10.4271/760887.
- Lockenour Jerry L. Layton Garrison P. “RPRV Research Focus on HiMAT.” Astronautics and Aeronautics AIAA New York April 1976
- “Highly Maneuverable Aircraft Technology (HiMAT).” Volume V of a Final Report Prepared by Rockwell International Corporation to the NASA Under Contract NAS4-2166 25 November 1974
- Quam R. et al. “Advanced Fighter Technology Integration (Phase I).” Air Force Flight Dynamics Laboratory Report Number AFFDL-TR-75-88 VI Dayton, Ohio September 1975