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Development of Materials for Solid Propellant Rocket Blast Defelectors
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English
Abstract
This paper demonstrates the approach to solving materials problems relevant to dry solid propellant rocket blast deflectors. The areas covered are the environments peculiar to these rockets; a qualitative evaluation of various materials exposed to subscale rocket motor test firings; and full-scale rocket blast deflectors performance.
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Citation
Locke, S., Chandler, H., Sayers, P., and Wheelehan, E., "Development of Materials for Solid Propellant Rocket Blast Defelectors," SAE Technical Paper 620367, 1962, https://doi.org/10.4271/620367.Also In
References
- Locke S. R. et al. “ Composite Structures for Hypersonic Flight,” SAMPE Conference, Los Angeles, California, March 23, 1961, Confidential
- Anderson A. Johns, F. “ Nondimensional Characteristics of Free and Deflected Supersonic Jets Exhausting With Quiescent Air.” NADC-ED-54-D1-25, March 1954
- “ Blast Deflector Study and Development Program,” Martin-Orlando, Oct. 30, 1961
- Locke S. R. et al. “ Composite Metal Ceramic Systems,” Astronautics, April 1961