Results 121 to 130 of about 143,533 (301)
Effect of Varying Design Options on the Transient Behavior of a Hybrid Rocket Motor
Journal of Aerospace Technology and Management, 2014 Hybrid rockets provide compelling features for use in atmospheric and space rocket propulsion. One of the prominent applications of hybrid rockets which foster on its characteristics is the propulsion of micro air launch vehicles. In this paper, a set of
Raed Kafafy +2 more
doaj
Hybrid Propulsion Technology Program [PDF]
Future launch systems of the United States will require improvements in booster safety, reliability, and cost. In order to increase payload capabilities, performance improvements are also desirable.
Holzman, A. L., Jensen, G. E.
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Complex Metal Hydrides. High Energy Fuel Components for Solid Propellant Rocket Motors
, 1978 E. C. Ashby
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Overview of rocket engine control [PDF]
The issues of Chemical Rocket Engine Control are broadly covered. The basic feedback information and control variables used in expendable and reusable rocket engines, such as Space Shuttle Main Engine, are discussed.
Lorenzo, Carl F., Musgrave, Jeffrey L.
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Investigation of the starting transients of high performance solid-propellant motors [PDF]
The starting transients of solid propellant engines were investigated to develop design principles for predicting transients in high performance igniter and engine configurations.
Caveny, L. H., Summerfield, M.
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Method for continuous variation of propellant flow and thrust in propulsive devices Patent [PDF]
, 1962 Continuous variation of propellant flow and thrust by application of liquid foam flow theory to injection ...
Morrell, G.
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Fuel Regression Characteristics of Porous Solid Fuels for End-Burning Hybrid Rocket
, 2002 Satoshi Watanabe +4 more
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Experimental investigation of laboratory-scale rocket engine fed on solid polyethylene rod as fuel [PDF]
, 2007 В. В. Емец +6 more
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