NASA NTRS · 19770023227
Solid rocket motor internal insulation
Abstract
Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant. The primary purpose is to prevent the case from reaching temperatures that endanger its structural integrity. Secondary functions of the insulation are listed and guidelines for avoiding critical problems in the development of internal insulation for rocket motors are presented.
Keep this discovery
Explore connections, maps & timelines
Twichell, S. E., Keller, R. B., Jr.. 1976-12-01. Solid rocket motor internal insulation. https://ntrs.nasa.gov/citations/19770023227
Cite the original work for its findings. Save a collection to share your selection of sources.