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Prediction of nozzle material performance for NASA's 260 SL-3 motor.Nozzle erosion profile, char penetration and temperature response predicted for nozzle material for 260 SL-3 motor
Document ID
19690048795
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Moody, H. L.
Price, F. C.
Date Acquired
August 5, 2013
Publication Date
March 1, 1969
Subject Category
Materials, Nonmetallic
Report/Patent Number
AIAA PAPER 68-504
Report Number: AIAA PAPER 68-504
Meeting Information
Meeting: INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, SOLID PROPULSION CONFERENCE
Location: ATLANTIC CITY, NJ
Start Date: June 4, 1968
End Date: June 6, 1968
Sponsors: INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A26784
Funding Number(s)
CONTRACT_GRANT: NAS7-567
Distribution Limits
Public
Copyright
Other

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