Advantages of Rapid Prototyping for Hybrid Rocket Motor Fuel Grain Fabrication

Author:

Fuller Jerome,Ehrlich Daniel,Lu Paul,Jansen Ryan,Hoffman Justin

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. A comparison of rapid prototyping technologies

2. 2Hinkley, D. "A Novel Cold Gas Propulsion System for Nanosatellites and Picosatellites," AIAA/USU Conference on SmallSatellites, AIAA, UtahState University, Utah, 2008.

3. 3Altman, D., and Holzman, A. "Overview and History of Hybrid Rocket Propulsion," Fundamentals of Hybrid Rocket Combustion and Propulsion, edited by M. J. Chiaverini and K. K. Kuo, Progress in Astronautics and Aeronautics, AIAA, Reston, Virginia, 2007,pp.1-33.

4. 6Altman, D., and Humble, R. "Hybrid Rocket Propulsion Systems," Space Propulsion Analysis and Design, edited by R. W. Humble, G. N. Henry, and W. J. Larson, Space Technology Series, McGraw-Hill Companies, Inc, NewYork, 1995,pp.365-443

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