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Commercial Application of Rocket Technology to WaterJet Propulsion
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English
Abstract
The technology of waterjet propulsion has reached a state of development where discussion of all technical aspects is beyond the scope and intent of this paper. The utilization and expansion of liquid rocket engine pump technologies derived from the U.S. military and space programs will be described, design of a single-stage axial flow pump for a new fast passenger hydrofoil will be discussed, and key benefits and features of waterjet systems will be discussed throughout the paper. The paper concludes with a forecast of possible uses for waterjet systems.
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Citation
Oquist, H. and Barham, H., "Commercial Application of Rocket Technology to WaterJet Propulsion," SAE Technical Paper 740876, 1974, https://doi.org/10.4271/740876.Also In
References
- Barr, R. A. Etter R. J. “Selection of Propulsion Systems for High Speed Advanced Marine Vehicles,” AIAA paper No. 74-344 AIAA/SNAME, Advanced Marine Vehicles Conference February 1974
- Wong, G. D. Barham H. L. “Some Aspects of Waterjet Optimization,” SAE paper No. 740282 SAE Automotive Engineering Congress February 1974
- Shultz, W. M. “Boeing Jetfoil Model 929-100,” AIAA paper No. 74-308 AIAA/SNAME, Advanced Marine Vehicles Conference February 1974