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The 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
19680051444
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moody, H. L.
Price, F. C.
Date Acquired
August 4, 2013
Publication Date
June 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 68-504
Report Number: AIAA PAPER 68-504
Meeting Information
Meeting: SOLID PROPULSION CONFERENCE
Location: ATLANTIC CITY, NJ
Country: US
Start Date: June 4, 1968
End Date: June 6, 1968
Sponsors: INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP, AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A32416
Distribution Limits
Public
Copyright
Other

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