NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Advanced solid propellant motor insulationAn advanced lightweight insulation system suitable for use in long duration, low pressure planetary orbiter-type motor applications was developed. Experiments included the screening of various filler and binder materials with optimization studies combining the best of each. Small scale test motor data were used to judge the degree of success.
Document ID
19730005232
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, P. L.
(Aerojet Solid Propulsion Co. Sacramento, CA, United States)
Russ, R. F.
(Aerojet Solid Propulsion Co. Sacramento, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-114513
Report Number: NASA-CR-114513
Accession Number
73N13959
Funding Number(s)
CONTRACT_GRANT: NAS2-6557
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available